From c10bf43dd3fab0928027b1f34cb6498bfe01b9ac Mon Sep 17 00:00:00 2001
From: Duc Bui Tien <mail@duc-buitien.de>
Date: Fri, 13 Sep 2024 09:45:08 +0200
Subject: [PATCH] New UnicadoGUI Branch
---
README.md => UnicadoGUI/Backend/README.md | 0
UnicadoGUI/Backend/configWriter.py | 26 +
UnicadoGUI/Backend/main.py | 112 +
UnicadoGUI/Backend/requirements.txt | 3 +
UnicadoGUI/Backend/test_main.http | 41 +
UnicadoGUI/Backend/tmp/modules | 1 +
.../xml_configs/calculatePerformance_conf.xml | 139 +
.../calculatePerformance_conf_default.xml | 139 +
.../xml_configs/calculatePolar_conf.xml | 592 ++
.../calculatePolar_conf_default.xml | 592 ++
UnicadoGUI/Backend/xml_configs/config.ini | 3 +
.../xml_configs/convergenceLoop_conf.xml | 192 +
.../xml_configs/createMissionXML_conf.xml | 255 +
.../createMissionXML_conf_default.xml | 255 +
.../xml_configs/initialSizing_conf.xml | 167 +
.../initialSizing_conf_default.xml | 167 +
.../xml_configs/missionAnalysis_conf.xml | 286 +
.../missionAnalysis_conf_default.xml | 286 +
.../xml_configs/propulsionDesign_conf.xml | 129 +
.../propulsionDesign_conf_default.xml | 129 +
.../xml_configs/systemsDesign_conf.xml | 2437 ++++++++
.../systemsDesign_conf_default.xml | 2437 ++++++++
UnicadoGUI/Backend/xml_configs/template.xml | 5001 +++++++++++++++++
.../weightAndBalanceAnalysis_conf.xml | 96 +
.../weightAndBalanceAnalysis_conf_default.xml | 96 +
.../Backend/xml_configs/wingDesign_conf.xml | 731 +++
.../xml_configs/wingDesign_conf_default.xml | 732 +++
UnicadoGUI/Frontend/.npmrc | 1 +
UnicadoGUI/Frontend/README.md | 38 +
UnicadoGUI/Frontend/package-lock.json | 2244 ++++++++
UnicadoGUI/Frontend/package.json | 32 +
UnicadoGUI/Frontend/src/app.d.ts | 13 +
UnicadoGUI/Frontend/src/app.html | 12 +
UnicadoGUI/Frontend/src/global.d.ts | 3 +
UnicadoGUI/Frontend/src/lib/index.ts | 1 +
UnicadoGUI/Frontend/src/routes/+layout.svelte | 73 +
UnicadoGUI/Frontend/src/routes/+page.svelte | 8 +
.../Frontend/src/routes/graphs/+page.svelte | 48 +
.../Frontend/src/routes/logs/+page.svelte | 40 +
.../Frontend/src/routes/model/+page.svelte | 618 ++
.../src/routes/model/InPlaceEdit.svelte | 58 +
.../Frontend/src/routes/reports/+page.svelte | 37 +
.../Frontend/src/routes/settings/+page.svelte | 343 ++
UnicadoGUI/Frontend/static/favicon.png | Bin 0 -> 182528 bytes
UnicadoGUI/Frontend/svelte.config.js | 18 +
UnicadoGUI/Frontend/tsconfig.json | 18 +
UnicadoGUI/Frontend/vite.config.ts | 8 +
47 files changed, 18657 insertions(+)
rename README.md => UnicadoGUI/Backend/README.md (100%)
create mode 100644 UnicadoGUI/Backend/configWriter.py
create mode 100644 UnicadoGUI/Backend/main.py
create mode 100644 UnicadoGUI/Backend/requirements.txt
create mode 100644 UnicadoGUI/Backend/test_main.http
create mode 100644 UnicadoGUI/Backend/tmp/modules
create mode 100644 UnicadoGUI/Backend/xml_configs/calculatePerformance_conf.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/calculatePerformance_conf_default.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/calculatePolar_conf.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/calculatePolar_conf_default.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/config.ini
create mode 100644 UnicadoGUI/Backend/xml_configs/convergenceLoop_conf.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/createMissionXML_conf.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/createMissionXML_conf_default.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/initialSizing_conf.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/initialSizing_conf_default.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/missionAnalysis_conf.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/missionAnalysis_conf_default.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/propulsionDesign_conf.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/propulsionDesign_conf_default.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/systemsDesign_conf.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/systemsDesign_conf_default.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/template.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/weightAndBalanceAnalysis_conf.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/weightAndBalanceAnalysis_conf_default.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/wingDesign_conf.xml
create mode 100644 UnicadoGUI/Backend/xml_configs/wingDesign_conf_default.xml
create mode 100644 UnicadoGUI/Frontend/.npmrc
create mode 100644 UnicadoGUI/Frontend/README.md
create mode 100644 UnicadoGUI/Frontend/package-lock.json
create mode 100644 UnicadoGUI/Frontend/package.json
create mode 100644 UnicadoGUI/Frontend/src/app.d.ts
create mode 100644 UnicadoGUI/Frontend/src/app.html
create mode 100644 UnicadoGUI/Frontend/src/global.d.ts
create mode 100644 UnicadoGUI/Frontend/src/lib/index.ts
create mode 100644 UnicadoGUI/Frontend/src/routes/+layout.svelte
create mode 100644 UnicadoGUI/Frontend/src/routes/+page.svelte
create mode 100644 UnicadoGUI/Frontend/src/routes/graphs/+page.svelte
create mode 100644 UnicadoGUI/Frontend/src/routes/logs/+page.svelte
create mode 100644 UnicadoGUI/Frontend/src/routes/model/+page.svelte
create mode 100644 UnicadoGUI/Frontend/src/routes/model/InPlaceEdit.svelte
create mode 100644 UnicadoGUI/Frontend/src/routes/reports/+page.svelte
create mode 100644 UnicadoGUI/Frontend/src/routes/settings/+page.svelte
create mode 100644 UnicadoGUI/Frontend/static/favicon.png
create mode 100644 UnicadoGUI/Frontend/svelte.config.js
create mode 100644 UnicadoGUI/Frontend/tsconfig.json
create mode 100644 UnicadoGUI/Frontend/vite.config.ts
diff --git a/README.md b/UnicadoGUI/Backend/README.md
similarity index 100%
rename from README.md
rename to UnicadoGUI/Backend/README.md
diff --git a/UnicadoGUI/Backend/configWriter.py b/UnicadoGUI/Backend/configWriter.py
new file mode 100644
index 0000000..714e99b
--- /dev/null
+++ b/UnicadoGUI/Backend/configWriter.py
@@ -0,0 +1,26 @@
+import os
+import configparser
+
+#small script to write a config.ini with available modules
+
+def create_config():
+ config = configparser.ConfigParser()
+ directory = os.fsencode('xml_configs')
+ available_modules = []
+ for file in os.listdir(directory):
+ filename = os.fsdecode(file)
+ if filename.endswith("default.xml"):
+ available_modules.append(filename.split('_')[0])
+ config['available_Modules']={'modules':','.join(available_modules)}
+
+ with open('xml_configs/config.ini', 'w') as configfile:
+ config.write(configfile)
+
+if __name__ == '__main__':
+ create_config()
+ config = configparser.ConfigParser()
+ config.read('xml_configs/config.ini')
+ print(config['available_Modules']['modules'].split(','))
+
+
+
diff --git a/UnicadoGUI/Backend/main.py b/UnicadoGUI/Backend/main.py
new file mode 100644
index 0000000..0cd07cd
--- /dev/null
+++ b/UnicadoGUI/Backend/main.py
@@ -0,0 +1,112 @@
+import configparser
+import json
+from fastapi import FastAPI
+from fastapi.responses import FileResponse
+from fastapi.middleware.cors import CORSMiddleware
+from pydantic import BaseModel
+import xmltodict
+from fastapi.encoders import jsonable_encoder
+
+#FastAPI Backend for UNICADO Gui
+app = FastAPI()
+
+origins = [
+ "http://localhost",
+ "http://localhost:5173",
+]
+
+app.add_middleware(
+ CORSMiddleware,
+ allow_origins=origins,
+ allow_credentials=True,
+ allow_methods=["*"],
+ allow_headers=["*"],
+)
+
+#Models for requests
+class Modules(BaseModel):
+ groups: list = []
+
+class Conf(BaseModel):
+ module_configuration_file: dict = {}
+
+
+#Endpoints
+@app.get("/start/{module}")
+async def start_module(module: str):
+ #dummy-function
+ #waiting for working unicado
+ return {"message": f"running {module} without problems"}
+
+
+#endpoint which returns a list of available modules
+@app.get("/modules/selection")
+async def get_avail_modules():
+ dict = {}
+ config = configparser.ConfigParser()
+ config.read('xml_configs/config.ini')
+
+ dict['availableModules']=config['available_Modules']['modules'].split(',')
+ return dict
+
+
+#TO-DO: following endpoints are for the case of a single project, need to add solution for more projects
+#endpoint which returns the last saved project
+@app.get("/modules")
+async def get_modules():
+ with open("tmp/modules", "r") as fp:
+ modules = json.load(fp)
+
+ return modules
+
+#endpoint to save the current project on the server
+@app.put("/modules/update")
+async def update_modules(item:Modules):
+ print(jsonable_encoder(item))
+ with open("tmp/modules", "w") as fp:
+ json.dump(jsonable_encoder(item), fp)
+
+ return item
+
+#endpoint to get the settings of selected module
+@app.get("/modules/{module}/config")
+async def get_module_config(module: str):
+ with open("xml_configs/"+module+"_conf.xml", encoding='utf-8') as fd:
+ config = json.dumps(xmltodict.parse(fd.read()))
+ return config
+
+#endpoint to save the setting of selected module
+@app.put("/modules/config/update")
+async def update_module_config(config: Conf):
+ dict = {"module_configuration_file": config.module_configuration_file}
+ xml = xmltodict.unparse(dict, pretty=True)
+ with open("xml_configs/" + config.module_configuration_file["@name"], "w", encoding='utf-8') as fd:
+ fd.write(xml)
+ return
+
+#endpoint reset settings of selected module to default
+@app.get("/modules/{module}/config/reset")
+async def reset_module_config(module:str):
+ with open("xml_configs/"+module+"_conf_default.xml", encoding='utf-8') as fd:
+ dict = xmltodict.parse(fd.read())
+ xml = xmltodict.unparse(dict, pretty=True)
+ with open("xml_configs/"+module+"_conf.xml", "w", encoding='utf-8') as fd:
+ fd.write(xml)
+ return
+
+#dummy endpoints
+@app.get("/graph/")
+async def get_plotData():
+ #dummy-Function
+ #TO-DO: working Implemantion
+ plotData = {}
+ return plotData
+
+@app.get("/log/{file}")
+async def get_csv(file: str):
+ return FileResponse(f"output_files/logFiles/{file}")
+
+@app.get("/report/{file}")
+async def get_report(file: str):
+ return FileResponse(f"output_files/reportHTML/{file}")
+
diff --git a/UnicadoGUI/Backend/requirements.txt b/UnicadoGUI/Backend/requirements.txt
new file mode 100644
index 0000000..6fef470
--- /dev/null
+++ b/UnicadoGUI/Backend/requirements.txt
@@ -0,0 +1,3 @@
+xmltodict~=0.13.0
+fastapi~=0.109.2
+pydantic~=1.10.14
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/test_main.http b/UnicadoGUI/Backend/test_main.http
new file mode 100644
index 0000000..70bc248
--- /dev/null
+++ b/UnicadoGUI/Backend/test_main.http
@@ -0,0 +1,41 @@
+# Test your FastAPI endpoints
+
+GET http://127.0.0.1:8000/
+Accept: application/json
+
+###
+
+GET http://127.0.0.1:8000/start/convergenceLoop
+Accept: application/json
+
+###
+
+GET http://127.0.0.1:8000/modules
+Accept: application/json
+
+###
+
+GET http://127.0.0.1:8000/modules/initialSizing/config
+Accept: application/json
+
+###
+
+GET http://127.0.0.1:8000//graph/convergenceLoop_plot.csv
+Accept: application/json
+
+###
+
+GET http://127.0.0.1:8000//log/convergenceLoop.log
+Accept: application/json
+
+###
+
+GET http://127.0.0.1:8000//report/convergenceLoop_report.html
+Accept: application/json
+
+###
+
+GET http://127.0.0.1:8000//graph/
+Accept: application/json
+
+###
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/tmp/modules b/UnicadoGUI/Backend/tmp/modules
new file mode 100644
index 0000000..d0279f9
--- /dev/null
+++ b/UnicadoGUI/Backend/tmp/modules
@@ -0,0 +1 @@
+{"groups": [{"name": "models from modularization branches", "loop": "true", "loopsize": 1, "modules": ["initialSizing", "wingDesign", "createMissionXML", "systemsDesign", "calculatePolar", "calculatePerformance", "missionAnalysis", "weightAndBalanceAnalysis", "propulsionDesign"]}]}
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/xml_configs/calculatePerformance_conf.xml b/UnicadoGUI/Backend/xml_configs/calculatePerformance_conf.xml
new file mode 100644
index 0000000..de72592
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/calculatePerformance_conf.xml
@@ -0,0 +1,139 @@
+<?xml version="1.0" encoding="utf-8" ?>
+<ConfigFile Name="calculatePerformance_conf.xml">
+ <ControlSettings Desc="general control settings">
+ <IOFileName>CSR-02.xml</IOFileName>
+ <IODir>../projects/CSR/CSR-02/</IODir>
+ <OwnToolLevel>2</OwnToolLevel>
+ <ConsoleOutputOn Desc="0: Off, 1: only out/err/warn, 2: 1 + info, 3: 2 + debug">1</ConsoleOutputOn>
+ <LogfileOutputOn Desc="0: Off, 1: only out/err/warn, 2: 1 + info, 3: 2 + debug">1</LogfileOutputOn>
+ <PlotOutputOn CopyPlottingFiles="1" DeletePlottingFilesFromToolFolder="1">1</PlotOutputOn>
+ <ReportOutputOn>1</ReportOutputOn>
+ <TexReportOn>0</TexReportOn>
+ <WriteInfoFiles>1</WriteInfoFiles>
+ <GnuplotScript>calculatePerformance_plot.plt</GnuplotScript>
+ <LogFile>calculatePerformance.log</LogFile>
+ <InkscapePath>DEFAULT</InkscapePath>
+ <GnuplotPath>DEFAULT</GnuplotPath>
+ <ProgramSpecific Desc="program-specific control settings">
+ <SaveCSVFilesToProjectFolder Desc="CSV files will be stored in the folder csvFilesForPlots" Default="1">1</SaveCSVFilesToProjectFolder>
+ <DeleteFiles>0</DeleteFiles>
+ </ProgramSpecific>
+ </ControlSettings>
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>CSR-02.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>../projects/CSR/CSR-02/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>3</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>true</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>false</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>TOOLNAME_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>TOOLNAME.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </gnuplot_path>
+ </control_settings>
+ <ProgramSettings Desc="program settings">
+ <ModuleStrategy Desc="Select the strategy level option tool execution" Default="calculatePerformance" >calculatePerformance</ModuleStrategy>
+ <MuduleFidelityLevel>low</MuduleFidelityLevel>
+ <PerformanceChecks Desc="Settings that affect different functionalities!">
+ <PayloadRangeDiagram Desc="Payload Range Diagram Calculation">
+ <switch Desc="On-Off-Switch for this method: 1:On, 0:Off" Unit="-" Default="1">1</switch>
+ <fidelityLevel Desc="Fidelity level of calculation">low</fidelityLevel>
+ </PayloadRangeDiagram>
+ <EnginePerformance Desc="Engine power estimation">
+ <switch Desc="On-Off-Switch for this method: 1:On, 0:Off" Unit="-" Default="1">1</switch>
+ <fidelityLevel Desc="Fidelity level of calculation">low</fidelityLevel>
+ </EnginePerformance>
+ <FlightEnvelopePerformance Desc="Estimation of flight range limits" OverwriteInitialValues="0">
+ <switch Desc="On-Off-Switch for this method: 1:On, 0:Off" Unit="-" Default="1">1</switch>
+ <fidelityLevel Desc="Fidelity level of calculation">low</fidelityLevel>
+ </FlightEnvelopePerformance>
+ <ClimbPerformance Desc="Climb Performance (so far only for plots)" Default="1">
+ <switch Desc="On-Off-Switch for this method: 1:On, 0:Off" Default="1">1</switch>
+ <fidelityLevel Desc="Fidelity level of calculation">low</fidelityLevel>
+ </ClimbPerformance>
+ <TOPerformance Desc="Estimation of the starting distance" CalculateBLFLPerformance="1">
+ <switch Desc="On-Off-Switch for this method: 1:On, 0:Off" Unit="-" Default="1">1</switch>
+ <fidelityLevel Desc="Fidelity level of calculation">low</fidelityLevel>
+ </TOPerformance>
+ <LandingPerformance Desc="Landing distance estimation" >
+ <switch Desc="On-Off-Switch for this method: 1:On, 0:Off" Unit="-" Default="1">1</switch>
+ <fidelityLevel Desc="Fidelity level of calculation">low</fidelityLevel>
+ </LandingPerformance>
+ <VnDiagram Desc="Switch for calculation of V-n diagram 1: On, 0: Off">
+ <switch Desc="On-Off-Switch for this method: 1:On, 0:Off" Unit="-" Default="1">1</switch>
+ <fidelityLevel Desc="Fidelity level of calculation">low</fidelityLevel>
+ </VnDiagram>
+ </PerformanceChecks>
+ <ConstantsForPerformanceChecks>
+ <enginePerformance>
+ <Ratings>
+ <nrRatings>4</nrRatings>
+ <Rating ID="1">Cruise</Rating>
+ <Rating ID="2">Climb</Rating>
+ <Rating ID="3">MaxCont</Rating>
+ <Rating ID="4">TO</Rating>
+ </Ratings>
+ </enginePerformance>
+ <fieldPerformance>
+ <runwaySlope Desc="Slope / climb of the runway" Unit="deg" Default="0">0</runwaySlope>
+ <headWind Desc="headwind speed" Unit="m/s" Default="0">0.0</headWind>
+ </fieldPerformance>
+ <VnDiagram>
+ <maxNClean Desc="Maximum load factor in clean configuration (fixed for CS-25 2.5)" Unit="-" Default="2.5">2.5</maxNClean>
+ <minNClean Desc="Minimum load factor in clean configuration (fixed -1.0 for CS-25)" Unit="-" Default="-1.0">-1.0</minNClean>
+ <maxNFlaps Desc="Maximum load factor with flaps (fixed for CS-25 2.0)" Unit="-" Default="2.0">2.0</maxNFlaps>
+ <minNFlaps Desc="Minimum load factor with flaps (fixed at CS-25 0.0)" Unit="-" Default="0.0">0.0</minNFlaps>
+ </VnDiagram>
+ </ConstantsForPerformanceChecks>
+ <Modes Desc="other settings that influence different modes!">
+ <FuelPlanning Desc="Fuel estimation switch: 1:On, 0:Off" Unit="-" Default="0">0</FuelPlanning>
+ <UseStudyMissionForAnalysis Desc="1: use missionStudy.xml, 0: use missionDesign.xml" Default="0">0</UseStudyMissionForAnalysis>
+ <MTOM_Design Desc="Redetermination of the MTOM: 1:Yes (e.g. DesignLoop), 0:No (e.g. only analysis)" Default="0">0</MTOM_Design>
+ </Modes>
+ <Mission Desc="Specification of the mission">
+ <optimizeMissionProfile Desc="Switch to optimize the mission profile" Unit="-" Default="0">0</optimizeMissionProfile>
+ </Mission>
+ <fuelPlanning>
+ <Standard>
+ <ContingencyFuel Desc="Relative percentage of Contigency Fuel in total Trip Fuel" Unit="-" Default="0.05">0.03</ContingencyFuel>
+ </Standard>
+ </fuelPlanning>
+ </ProgramSettings>
+</ConfigFile>
diff --git a/UnicadoGUI/Backend/xml_configs/calculatePerformance_conf_default.xml b/UnicadoGUI/Backend/xml_configs/calculatePerformance_conf_default.xml
new file mode 100644
index 0000000..de72592
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/calculatePerformance_conf_default.xml
@@ -0,0 +1,139 @@
+<?xml version="1.0" encoding="utf-8" ?>
+<ConfigFile Name="calculatePerformance_conf.xml">
+ <ControlSettings Desc="general control settings">
+ <IOFileName>CSR-02.xml</IOFileName>
+ <IODir>../projects/CSR/CSR-02/</IODir>
+ <OwnToolLevel>2</OwnToolLevel>
+ <ConsoleOutputOn Desc="0: Off, 1: only out/err/warn, 2: 1 + info, 3: 2 + debug">1</ConsoleOutputOn>
+ <LogfileOutputOn Desc="0: Off, 1: only out/err/warn, 2: 1 + info, 3: 2 + debug">1</LogfileOutputOn>
+ <PlotOutputOn CopyPlottingFiles="1" DeletePlottingFilesFromToolFolder="1">1</PlotOutputOn>
+ <ReportOutputOn>1</ReportOutputOn>
+ <TexReportOn>0</TexReportOn>
+ <WriteInfoFiles>1</WriteInfoFiles>
+ <GnuplotScript>calculatePerformance_plot.plt</GnuplotScript>
+ <LogFile>calculatePerformance.log</LogFile>
+ <InkscapePath>DEFAULT</InkscapePath>
+ <GnuplotPath>DEFAULT</GnuplotPath>
+ <ProgramSpecific Desc="program-specific control settings">
+ <SaveCSVFilesToProjectFolder Desc="CSV files will be stored in the folder csvFilesForPlots" Default="1">1</SaveCSVFilesToProjectFolder>
+ <DeleteFiles>0</DeleteFiles>
+ </ProgramSpecific>
+ </ControlSettings>
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>CSR-02.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>../projects/CSR/CSR-02/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>3</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>true</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>false</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>TOOLNAME_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>TOOLNAME.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </gnuplot_path>
+ </control_settings>
+ <ProgramSettings Desc="program settings">
+ <ModuleStrategy Desc="Select the strategy level option tool execution" Default="calculatePerformance" >calculatePerformance</ModuleStrategy>
+ <MuduleFidelityLevel>low</MuduleFidelityLevel>
+ <PerformanceChecks Desc="Settings that affect different functionalities!">
+ <PayloadRangeDiagram Desc="Payload Range Diagram Calculation">
+ <switch Desc="On-Off-Switch for this method: 1:On, 0:Off" Unit="-" Default="1">1</switch>
+ <fidelityLevel Desc="Fidelity level of calculation">low</fidelityLevel>
+ </PayloadRangeDiagram>
+ <EnginePerformance Desc="Engine power estimation">
+ <switch Desc="On-Off-Switch for this method: 1:On, 0:Off" Unit="-" Default="1">1</switch>
+ <fidelityLevel Desc="Fidelity level of calculation">low</fidelityLevel>
+ </EnginePerformance>
+ <FlightEnvelopePerformance Desc="Estimation of flight range limits" OverwriteInitialValues="0">
+ <switch Desc="On-Off-Switch for this method: 1:On, 0:Off" Unit="-" Default="1">1</switch>
+ <fidelityLevel Desc="Fidelity level of calculation">low</fidelityLevel>
+ </FlightEnvelopePerformance>
+ <ClimbPerformance Desc="Climb Performance (so far only for plots)" Default="1">
+ <switch Desc="On-Off-Switch for this method: 1:On, 0:Off" Default="1">1</switch>
+ <fidelityLevel Desc="Fidelity level of calculation">low</fidelityLevel>
+ </ClimbPerformance>
+ <TOPerformance Desc="Estimation of the starting distance" CalculateBLFLPerformance="1">
+ <switch Desc="On-Off-Switch for this method: 1:On, 0:Off" Unit="-" Default="1">1</switch>
+ <fidelityLevel Desc="Fidelity level of calculation">low</fidelityLevel>
+ </TOPerformance>
+ <LandingPerformance Desc="Landing distance estimation" >
+ <switch Desc="On-Off-Switch for this method: 1:On, 0:Off" Unit="-" Default="1">1</switch>
+ <fidelityLevel Desc="Fidelity level of calculation">low</fidelityLevel>
+ </LandingPerformance>
+ <VnDiagram Desc="Switch for calculation of V-n diagram 1: On, 0: Off">
+ <switch Desc="On-Off-Switch for this method: 1:On, 0:Off" Unit="-" Default="1">1</switch>
+ <fidelityLevel Desc="Fidelity level of calculation">low</fidelityLevel>
+ </VnDiagram>
+ </PerformanceChecks>
+ <ConstantsForPerformanceChecks>
+ <enginePerformance>
+ <Ratings>
+ <nrRatings>4</nrRatings>
+ <Rating ID="1">Cruise</Rating>
+ <Rating ID="2">Climb</Rating>
+ <Rating ID="3">MaxCont</Rating>
+ <Rating ID="4">TO</Rating>
+ </Ratings>
+ </enginePerformance>
+ <fieldPerformance>
+ <runwaySlope Desc="Slope / climb of the runway" Unit="deg" Default="0">0</runwaySlope>
+ <headWind Desc="headwind speed" Unit="m/s" Default="0">0.0</headWind>
+ </fieldPerformance>
+ <VnDiagram>
+ <maxNClean Desc="Maximum load factor in clean configuration (fixed for CS-25 2.5)" Unit="-" Default="2.5">2.5</maxNClean>
+ <minNClean Desc="Minimum load factor in clean configuration (fixed -1.0 for CS-25)" Unit="-" Default="-1.0">-1.0</minNClean>
+ <maxNFlaps Desc="Maximum load factor with flaps (fixed for CS-25 2.0)" Unit="-" Default="2.0">2.0</maxNFlaps>
+ <minNFlaps Desc="Minimum load factor with flaps (fixed at CS-25 0.0)" Unit="-" Default="0.0">0.0</minNFlaps>
+ </VnDiagram>
+ </ConstantsForPerformanceChecks>
+ <Modes Desc="other settings that influence different modes!">
+ <FuelPlanning Desc="Fuel estimation switch: 1:On, 0:Off" Unit="-" Default="0">0</FuelPlanning>
+ <UseStudyMissionForAnalysis Desc="1: use missionStudy.xml, 0: use missionDesign.xml" Default="0">0</UseStudyMissionForAnalysis>
+ <MTOM_Design Desc="Redetermination of the MTOM: 1:Yes (e.g. DesignLoop), 0:No (e.g. only analysis)" Default="0">0</MTOM_Design>
+ </Modes>
+ <Mission Desc="Specification of the mission">
+ <optimizeMissionProfile Desc="Switch to optimize the mission profile" Unit="-" Default="0">0</optimizeMissionProfile>
+ </Mission>
+ <fuelPlanning>
+ <Standard>
+ <ContingencyFuel Desc="Relative percentage of Contigency Fuel in total Trip Fuel" Unit="-" Default="0.05">0.03</ContingencyFuel>
+ </Standard>
+ </fuelPlanning>
+ </ProgramSettings>
+</ConfigFile>
diff --git a/UnicadoGUI/Backend/xml_configs/calculatePolar_conf.xml b/UnicadoGUI/Backend/xml_configs/calculatePolar_conf.xml
new file mode 100644
index 0000000..b7fefec
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/calculatePolar_conf.xml
@@ -0,0 +1,592 @@
+<?xml version="1.0" encoding="utf-8" ?>
+<module_configuration_file name="wingDesign_conf.xml">
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>new_aircraft.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>../projects/CSR/CSR-02/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>3</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>false</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>false</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>false</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>calculatePolar_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>calculatePolar.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>../inkscape/</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>../gnuplot/</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings description="programSettings">
+ <CLModeAirfoilSelection description="aircraft CL for airfoil selection, 0: CL at ICA, 1: CL at TOC, 2: CL avg cr">
+ <value>mode_0</value>
+ <default>mode_0</default>
+ </CLModeAirfoilSelection>
+ <Trim>
+ <DoTrim description="Method for calculating trimmed aircraft polars with linear interpolation">
+ <value>false</value>
+ <default>true</default>
+ </DoTrim>
+ <TrimWithAdditionalCoGPositions description="Do trim method only for design CG or additional for forward and aft position">
+ <value>false</value>
+ <default>false</default>
+ </TrimWithAdditionalCoGPositions>
+ <TrimHighLift description="Additionally trim the high lift polars">
+ <value>false</value>
+ <default>false</default>
+ </TrimHighLift>
+ <StabAngleGrid description="stab angle gird relative to design angle; mode_0: coarse[-6;6] in 6 deg steps; mode_1: fine [-6;6] in 2 deg steps; mode_2: custom">
+ <value>mode_0</value>
+ <default>mode_0</default>
+ </StabAngleGrid>
+ <customStabAngleGrid description="custom stabilizer angles if StabAngleGrid is set to mode_2">
+ <value>-1;0;1</value>
+ <default>-1;0;1</default>
+ </customStabAngleGrid>
+ </Trim>
+ <LiftingLine description="liftingLine">
+ <FolderPath description="Path to LIFTING_LINE">
+ <value>LiftingLine/</value>
+ </FolderPath>
+ <DeleteLiftingLineFiles description="Deletes LL folder from project folder after program execution">
+ <value>false</value>
+ <default>true</default>
+ </DeleteLiftingLineFiles>
+ </LiftingLine>
+ <aeroStrategySelection description="selection of strategy to use">
+ <tawStrategies>
+ <default>tawDefaultStrategy</default>
+ <value>tawDefaultStrategy</value>
+ </tawStrategies>
+ <bwbStrategies>
+ <default>bwbDefaultStrategy</default>
+ <value>bwbDefaultStrategy</value>
+ </bwbStrategies>
+ </aeroStrategySelection>
+ <FlightConditions description="Flight State">
+ <AdaptMachNumbersToCruiseReq description="0: List below is used, 1: Mach numbers are distributed reasonably with respect to design Mach number.">
+ <value>mode_0</value>
+ </AdaptMachNumbersToCruiseReq>
+ <PolarAttributes description="If AdaptMachNumbersToCruiseReq is on, extrapolation and grid change are set for all polars. Otherwise list below is used.">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>true</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>true</value>
+ </AllowGridChange>
+ </PolarAttributes>
+ <DesignAltitude description="Design height for Mach numbers M geq 0.5" Unit="ft" UseAverageCruiseAltitude="0" Default="35000">
+ <value>35000</value>
+ <unit>ft</unit>
+ </DesignAltitude>
+ <numberFlightConditions description="Number of flight conditions to be examined">
+ <value>11</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000</upper_boundary>
+ </numberFlightConditions>
+ <FlightCondition ID="0" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.2</default>
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <value>0</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="1" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.5</default>
+ <value>0.5</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="2" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.6</default>
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="3" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.7</default>
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="4" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.75</default>
+ <value>0.73</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="5" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.78</default>
+ <value>0.76</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="6" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.80</default>
+ <value>0.77</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="7" Desc="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.81</default>
+ <value>0.78</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="8" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.82</default>
+ <value>0.79</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="9" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.83</default>
+ <value>0.80</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="10" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.84</default>
+ <value>0.83</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ </FlightConditions>
+ <LiftingLineForTAW>
+ <stepWidthCL description="CL steps in for the polars">
+ <value>0.001</value>
+ <default>0.001</default>
+ <unit>1</unit>
+ <lower_boundary>0.0001</lower_boundary>
+ <upper_boundary>0.1</upper_boundary>
+ </stepWidthCL>
+ <PitchingMoment description="Parameters for CM correction and calibration">
+ <CM_corr_fuselage description="Semi-emp. CMy-correction regarding fuselage influence (concerns CLalpha (TB), CM0 (TB), dCMdCL or CMalpha), 0: no correction, 1: Raymer, 2: Torenbeek">
+ <value>mode_1</value>
+ <default>mode_1</default>
+ </CM_corr_fuselage>
+ <CM_corr_nacelle description="Semi-emp. CMy correction for nacelle influence (concerns dCMdCL or CMalpha), 0: no correction, 1: Raymer, 2: Torenbeek" Default="1">
+ <value>mode_1</value>
+ <default>mode_1</default>
+ </CM_corr_nacelle>
+ <delta_CM0 description="Optional CM0-Summand (only for calibration!)">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <upper_boundary>inf</upper_boundary>
+ <lower_boundary>-inf</lower_boundary>
+ </delta_CM0>
+ <delta_dCMdCL description="Optional dCMdCL summand (only for calibration!)">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <upper_boundary>inf</upper_boundary>
+ <lower_boundary>-inf</lower_boundary>
+ </delta_dCMdCL>
+ </PitchingMoment>
+ <InducedDragCorrection>
+ <indDragCtCorrForCalibration description="indDragCtCorrForCalibration">
+ <value>1</value>
+ <default>0.99</default>
+ <unit>1</unit>
+ <upper_boundary>inf</upper_boundary>
+ <lower_boundary>-inf</lower_boundary>
+ </indDragCtCorrForCalibration>
+ <factorIndDragCleanPolar description="factorIndDragCleanPolar">
+ <value>1.0</value>
+ <default>1.0</default>
+ <unit>1</unit>
+ <upper_boundary>inf</upper_boundary>
+ <lower_boundary>-inf</lower_boundary>
+ </factorIndDragCleanPolar>
+ </InducedDragCorrection>
+ </LiftingLineForTAW>
+ <ViscDragRaymer>
+ <ManualTransition description="false: No manual transition; true: Manual transition relative to chord">
+ <value>false</value>
+ <default>false</default>
+ <unit>false</unit>
+ </ManualTransition>
+ <TransitionLocationWing description="Transition lines relative to local chord of components">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </TransitionLocationWing>
+ <TransitionLocationStabilizer description="Transition lines relative to local chord of components">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </TransitionLocationStabilizer>
+ <TransitionLocationFin description="Transition lines relative to local chord of components">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </TransitionLocationFin>
+ <UseCalibration description="switch for calibration">
+ <value>true</value>
+ <default>true</default>
+ </UseCalibration>
+ <CalibrationHighMa description="calibration values for Mach Numbers greater 0.5">
+ <CDSum description="description">
+ <value>0.0</value>
+ <default>0.0</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CDSum>
+ <CLFact description="description">
+ <value>0.01</value>
+ <default>0.01</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CLFact>
+ <CLExp description="description">
+ <value>4</value>
+ <default>4</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CLExp>
+ </CalibrationHighMa>
+ <CalibrationLowMa description="calibration values for Mach Numbers equal and lower 0.5">
+ <CDSum description="description">
+ <value>0.0</value>
+ <default>0.0</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CDSum>
+ <CLFact description="description">
+ <value>0.002</value>
+ <default>0.002</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CLFact>
+ <CLExp description="description">
+ <value>2</value>
+ <default>2</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CLExp>
+ </CalibrationLowMa>
+ </ViscDragRaymer>
+ <WaveDragMason>
+ <NumberWingStrips description="Number of wing strips used for the drag calculation">
+ <value>50</value>
+ <default>50</default>
+ <unit>1</unit>
+ <lower_boundary>1</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </NumberWingStrips>
+ <Ka description="Technology factor of the wing profiles for the mason method">
+ <value>0.935</value>
+ <default>0.94</default>
+ <unit>1</unit>
+ <lower_boundary>0.87</lower_boundary>
+ <upper_boundary>0.95</upper_boundary>
+ </Ka>
+ <MaximumSegmentSweep description="Maximum allowed sweep, befor wave drag calculate returns zero">
+ <value>50</value>
+ <default>50</default>
+ <unit>deg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>90</upper_boundary>
+ </MaximumSegmentSweep>
+ <UseCostomReferenceAngleForSweep description="Switch to enable custom position for the sweep line">
+ <value>false</value>
+ <default>fasle</default>
+ </UseCostomReferenceAngleForSweep>
+ <CustomSweepAngle description="Custom chord postition where to calculate the sweep line if enabled">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </CustomSweepAngle>
+ <UseCalibration description="Switch to enable calibration method">
+ <value>true</value>
+ <default>true</default>
+ </UseCalibration>
+ <CLFact description="CLFact">
+ <value>1</value>
+ <default>1</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CLFact>
+ <CLExp description="CLExp">
+ <value>8</value>
+ <default>8</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CLExp>
+ <DoDragCountCorrection description="Flat correction of wave wing drag in drag counts">
+ <value>false</value>
+ <default>false</default>
+ </DoDragCountCorrection>
+ <deltaWaveDragWing description="corrections in drag counts">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </deltaWaveDragWing>
+ </WaveDragMason>
+ <SemiEmpiricalHighLiftAdaptions>
+ <deltaTotalDrag description="Reduction of the total high lift drag in drag counts">
+ <value>0.0</value>
+ <default>0.0</default>
+ <unit>1</unit>
+ <lower_boundary>-1000</lower_boundary>
+ <upper_boundary>1000</upper_boundary>
+ </deltaTotalDrag>
+ <factorDrag description="Rel. factor for percentage change of total drag">
+ <value>1.0</value>
+ <default>1.0</default>
+ <unit>1</unit>
+ <lower_boundary>-1000</lower_boundary>
+ <upper_boundary>1000</upper_boundary>
+ </factorDrag>
+ </SemiEmpiricalHighLiftAdaptions>
+ <DragCorrection description="">
+ <factorDragCleanPolars description="">
+ <value>1</value>
+ <default>1</default>
+ <unit>1</unit>
+ <lower_boundary>0.5</lower_boundary>
+ <upper_boundary>1.5</upper_boundary>
+ </factorDragCleanPolars>
+ <factorDragHighliftPolar>
+ <value>1</value>
+ <default>1</default>
+ <unit>1</unit>
+ <lower_boundary>0.5</lower_boundary>
+ <upper_boundary>1.5</upper_boundary>
+ </factorDragHighliftPolar>
+ <deltaTotalDragHighLift description="Reduction of the total high lift drag in drag counts">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <lower_boundary>-60</lower_boundary>
+ <upper_boundary>60</upper_boundary>
+ </deltaTotalDragHighLift>
+ </DragCorrection>
+ </program_settings>
+</module_configuration_file>
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/xml_configs/calculatePolar_conf_default.xml b/UnicadoGUI/Backend/xml_configs/calculatePolar_conf_default.xml
new file mode 100644
index 0000000..b7fefec
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/calculatePolar_conf_default.xml
@@ -0,0 +1,592 @@
+<?xml version="1.0" encoding="utf-8" ?>
+<module_configuration_file name="wingDesign_conf.xml">
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>new_aircraft.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>../projects/CSR/CSR-02/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>3</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>false</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>false</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>false</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>calculatePolar_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>calculatePolar.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>../inkscape/</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>../gnuplot/</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings description="programSettings">
+ <CLModeAirfoilSelection description="aircraft CL for airfoil selection, 0: CL at ICA, 1: CL at TOC, 2: CL avg cr">
+ <value>mode_0</value>
+ <default>mode_0</default>
+ </CLModeAirfoilSelection>
+ <Trim>
+ <DoTrim description="Method for calculating trimmed aircraft polars with linear interpolation">
+ <value>false</value>
+ <default>true</default>
+ </DoTrim>
+ <TrimWithAdditionalCoGPositions description="Do trim method only for design CG or additional for forward and aft position">
+ <value>false</value>
+ <default>false</default>
+ </TrimWithAdditionalCoGPositions>
+ <TrimHighLift description="Additionally trim the high lift polars">
+ <value>false</value>
+ <default>false</default>
+ </TrimHighLift>
+ <StabAngleGrid description="stab angle gird relative to design angle; mode_0: coarse[-6;6] in 6 deg steps; mode_1: fine [-6;6] in 2 deg steps; mode_2: custom">
+ <value>mode_0</value>
+ <default>mode_0</default>
+ </StabAngleGrid>
+ <customStabAngleGrid description="custom stabilizer angles if StabAngleGrid is set to mode_2">
+ <value>-1;0;1</value>
+ <default>-1;0;1</default>
+ </customStabAngleGrid>
+ </Trim>
+ <LiftingLine description="liftingLine">
+ <FolderPath description="Path to LIFTING_LINE">
+ <value>LiftingLine/</value>
+ </FolderPath>
+ <DeleteLiftingLineFiles description="Deletes LL folder from project folder after program execution">
+ <value>false</value>
+ <default>true</default>
+ </DeleteLiftingLineFiles>
+ </LiftingLine>
+ <aeroStrategySelection description="selection of strategy to use">
+ <tawStrategies>
+ <default>tawDefaultStrategy</default>
+ <value>tawDefaultStrategy</value>
+ </tawStrategies>
+ <bwbStrategies>
+ <default>bwbDefaultStrategy</default>
+ <value>bwbDefaultStrategy</value>
+ </bwbStrategies>
+ </aeroStrategySelection>
+ <FlightConditions description="Flight State">
+ <AdaptMachNumbersToCruiseReq description="0: List below is used, 1: Mach numbers are distributed reasonably with respect to design Mach number.">
+ <value>mode_0</value>
+ </AdaptMachNumbersToCruiseReq>
+ <PolarAttributes description="If AdaptMachNumbersToCruiseReq is on, extrapolation and grid change are set for all polars. Otherwise list below is used.">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>true</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>true</value>
+ </AllowGridChange>
+ </PolarAttributes>
+ <DesignAltitude description="Design height for Mach numbers M geq 0.5" Unit="ft" UseAverageCruiseAltitude="0" Default="35000">
+ <value>35000</value>
+ <unit>ft</unit>
+ </DesignAltitude>
+ <numberFlightConditions description="Number of flight conditions to be examined">
+ <value>11</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000</upper_boundary>
+ </numberFlightConditions>
+ <FlightCondition ID="0" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.2</default>
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <value>0</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="1" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.5</default>
+ <value>0.5</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="2" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.6</default>
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="3" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.7</default>
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="4" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.75</default>
+ <value>0.73</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="5" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.78</default>
+ <value>0.76</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="6" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.80</default>
+ <value>0.77</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="7" Desc="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.81</default>
+ <value>0.78</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="8" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.82</default>
+ <value>0.79</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="9" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.83</default>
+ <value>0.80</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ <FlightCondition ID="10" description="Description of the flight condition">
+ <AllowExtrapolation description="AllowExtrapolation">
+ <value>mode_1</value>
+ </AllowExtrapolation>
+ <AllowGridChange description="AllowGridChange">
+ <value>mode_1</value>
+ </AllowGridChange>
+ <Mach description="Mach number">
+ <default>0.84</default>
+ <value>0.83</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </Mach>
+ <Altitude description="flight level">
+ <default>3500</default>
+ <value>35000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>42069</upper_boundary>
+ </Altitude>
+ </FlightCondition>
+ </FlightConditions>
+ <LiftingLineForTAW>
+ <stepWidthCL description="CL steps in for the polars">
+ <value>0.001</value>
+ <default>0.001</default>
+ <unit>1</unit>
+ <lower_boundary>0.0001</lower_boundary>
+ <upper_boundary>0.1</upper_boundary>
+ </stepWidthCL>
+ <PitchingMoment description="Parameters for CM correction and calibration">
+ <CM_corr_fuselage description="Semi-emp. CMy-correction regarding fuselage influence (concerns CLalpha (TB), CM0 (TB), dCMdCL or CMalpha), 0: no correction, 1: Raymer, 2: Torenbeek">
+ <value>mode_1</value>
+ <default>mode_1</default>
+ </CM_corr_fuselage>
+ <CM_corr_nacelle description="Semi-emp. CMy correction for nacelle influence (concerns dCMdCL or CMalpha), 0: no correction, 1: Raymer, 2: Torenbeek" Default="1">
+ <value>mode_1</value>
+ <default>mode_1</default>
+ </CM_corr_nacelle>
+ <delta_CM0 description="Optional CM0-Summand (only for calibration!)">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <upper_boundary>inf</upper_boundary>
+ <lower_boundary>-inf</lower_boundary>
+ </delta_CM0>
+ <delta_dCMdCL description="Optional dCMdCL summand (only for calibration!)">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <upper_boundary>inf</upper_boundary>
+ <lower_boundary>-inf</lower_boundary>
+ </delta_dCMdCL>
+ </PitchingMoment>
+ <InducedDragCorrection>
+ <indDragCtCorrForCalibration description="indDragCtCorrForCalibration">
+ <value>1</value>
+ <default>0.99</default>
+ <unit>1</unit>
+ <upper_boundary>inf</upper_boundary>
+ <lower_boundary>-inf</lower_boundary>
+ </indDragCtCorrForCalibration>
+ <factorIndDragCleanPolar description="factorIndDragCleanPolar">
+ <value>1.0</value>
+ <default>1.0</default>
+ <unit>1</unit>
+ <upper_boundary>inf</upper_boundary>
+ <lower_boundary>-inf</lower_boundary>
+ </factorIndDragCleanPolar>
+ </InducedDragCorrection>
+ </LiftingLineForTAW>
+ <ViscDragRaymer>
+ <ManualTransition description="false: No manual transition; true: Manual transition relative to chord">
+ <value>false</value>
+ <default>false</default>
+ <unit>false</unit>
+ </ManualTransition>
+ <TransitionLocationWing description="Transition lines relative to local chord of components">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </TransitionLocationWing>
+ <TransitionLocationStabilizer description="Transition lines relative to local chord of components">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </TransitionLocationStabilizer>
+ <TransitionLocationFin description="Transition lines relative to local chord of components">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </TransitionLocationFin>
+ <UseCalibration description="switch for calibration">
+ <value>true</value>
+ <default>true</default>
+ </UseCalibration>
+ <CalibrationHighMa description="calibration values for Mach Numbers greater 0.5">
+ <CDSum description="description">
+ <value>0.0</value>
+ <default>0.0</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CDSum>
+ <CLFact description="description">
+ <value>0.01</value>
+ <default>0.01</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CLFact>
+ <CLExp description="description">
+ <value>4</value>
+ <default>4</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CLExp>
+ </CalibrationHighMa>
+ <CalibrationLowMa description="calibration values for Mach Numbers equal and lower 0.5">
+ <CDSum description="description">
+ <value>0.0</value>
+ <default>0.0</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CDSum>
+ <CLFact description="description">
+ <value>0.002</value>
+ <default>0.002</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CLFact>
+ <CLExp description="description">
+ <value>2</value>
+ <default>2</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CLExp>
+ </CalibrationLowMa>
+ </ViscDragRaymer>
+ <WaveDragMason>
+ <NumberWingStrips description="Number of wing strips used for the drag calculation">
+ <value>50</value>
+ <default>50</default>
+ <unit>1</unit>
+ <lower_boundary>1</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </NumberWingStrips>
+ <Ka description="Technology factor of the wing profiles for the mason method">
+ <value>0.935</value>
+ <default>0.94</default>
+ <unit>1</unit>
+ <lower_boundary>0.87</lower_boundary>
+ <upper_boundary>0.95</upper_boundary>
+ </Ka>
+ <MaximumSegmentSweep description="Maximum allowed sweep, befor wave drag calculate returns zero">
+ <value>50</value>
+ <default>50</default>
+ <unit>deg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>90</upper_boundary>
+ </MaximumSegmentSweep>
+ <UseCostomReferenceAngleForSweep description="Switch to enable custom position for the sweep line">
+ <value>false</value>
+ <default>fasle</default>
+ </UseCostomReferenceAngleForSweep>
+ <CustomSweepAngle description="Custom chord postition where to calculate the sweep line if enabled">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </CustomSweepAngle>
+ <UseCalibration description="Switch to enable calibration method">
+ <value>true</value>
+ <default>true</default>
+ </UseCalibration>
+ <CLFact description="CLFact">
+ <value>1</value>
+ <default>1</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CLFact>
+ <CLExp description="CLExp">
+ <value>8</value>
+ <default>8</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </CLExp>
+ <DoDragCountCorrection description="Flat correction of wave wing drag in drag counts">
+ <value>false</value>
+ <default>false</default>
+ </DoDragCountCorrection>
+ <deltaWaveDragWing description="corrections in drag counts">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </deltaWaveDragWing>
+ </WaveDragMason>
+ <SemiEmpiricalHighLiftAdaptions>
+ <deltaTotalDrag description="Reduction of the total high lift drag in drag counts">
+ <value>0.0</value>
+ <default>0.0</default>
+ <unit>1</unit>
+ <lower_boundary>-1000</lower_boundary>
+ <upper_boundary>1000</upper_boundary>
+ </deltaTotalDrag>
+ <factorDrag description="Rel. factor for percentage change of total drag">
+ <value>1.0</value>
+ <default>1.0</default>
+ <unit>1</unit>
+ <lower_boundary>-1000</lower_boundary>
+ <upper_boundary>1000</upper_boundary>
+ </factorDrag>
+ </SemiEmpiricalHighLiftAdaptions>
+ <DragCorrection description="">
+ <factorDragCleanPolars description="">
+ <value>1</value>
+ <default>1</default>
+ <unit>1</unit>
+ <lower_boundary>0.5</lower_boundary>
+ <upper_boundary>1.5</upper_boundary>
+ </factorDragCleanPolars>
+ <factorDragHighliftPolar>
+ <value>1</value>
+ <default>1</default>
+ <unit>1</unit>
+ <lower_boundary>0.5</lower_boundary>
+ <upper_boundary>1.5</upper_boundary>
+ </factorDragHighliftPolar>
+ <deltaTotalDragHighLift description="Reduction of the total high lift drag in drag counts">
+ <value>0</value>
+ <default>0</default>
+ <unit>1</unit>
+ <lower_boundary>-60</lower_boundary>
+ <upper_boundary>60</upper_boundary>
+ </deltaTotalDragHighLift>
+ </DragCorrection>
+ </program_settings>
+</module_configuration_file>
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/xml_configs/config.ini b/UnicadoGUI/Backend/xml_configs/config.ini
new file mode 100644
index 0000000..a83da65
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/config.ini
@@ -0,0 +1,3 @@
+[available_Modules]
+modules = calculatePerformance,calculatePolar,createMissionXML,initialSizing,missionAnalysis,propulsionDesign,systemsDesign,weightAndBalanceAnalysis,wingDesign
+
diff --git a/UnicadoGUI/Backend/xml_configs/convergenceLoop_conf.xml b/UnicadoGUI/Backend/xml_configs/convergenceLoop_conf.xml
new file mode 100644
index 0000000..625cf7c
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/convergenceLoop_conf.xml
@@ -0,0 +1,192 @@
+<ConfigFile Name="convergenceLoop_conf.xml">
+ <ControlSettings Desc="general control settings">
+ <IOFileName>CSR-02.xml</IOFileName>
+ <IODir>../projects/CSR/CSR-02/</IODir>
+ <OwnToolLevel>1</OwnToolLevel>
+ <ConsoleOutputOn Desc="0: Off, 1: only out/err/warn, 2: 1 + info, 3: 2 + debug">1</ConsoleOutputOn>
+ <LogfileOutputOn Desc="0: Off, 1: only out/err/warn, 2: 1 + info, 3: 2 + debug">1</LogfileOutputOn>
+ <PlotOutputOn CopyPlottingFiles="1">1</PlotOutputOn>
+ <ReportOutputOn>1</ReportOutputOn>
+ <TexReportOn>1</TexReportOn>
+ <WriteInfoFiles>0</WriteInfoFiles>
+ <GnuplotScript>convergenceLoop_plot.plt</GnuplotScript>
+ <LogFile>convergenceLoop.log</LogFile>
+ <InkscapePath>DEFAULT</InkscapePath>
+ <GnuplotPath>DEFAULT</GnuplotPath>
+ <ProgramSpecific Desc="program-specific control settings">
+ <UseControlSettingsForSubPrograms Default="1" Desc="1: Using General Control Settings for All Subprograms">1</UseControlSettingsForSubPrograms>
+ <ResetConfigsAtExit Default="1" Desc="1: Resetting Config files at the End of the Program">1</ResetConfigsAtExit>
+ <SaveConfigsToProjectFolder Default="1" Desc="1: Configs of the subprograms are stored in the folder IODir/configFiles/">1</SaveConfigsToProjectFolder>
+ <SaveLogFilesToProjectFolder Default="1" Desc="1: Logfiles of the subprograms are stored in the folder IODir/configFiles/">1</SaveLogFilesToProjectFolder>
+ <UseConfigsFromProjectFolder Default="0" Desc="1: Configs are taken from project folders (see above)">0</UseConfigsFromProjectFolder>
+ <CheckSettingsForDesignLogic ChangeIfNotConsistent="1" Default="1" Desc="Settings of subprograms are checked">1</CheckSettingsForDesignLogic>
+ <DeletePlotsBeforeRun Default="0" Desc="1: Old plots and reports are deleted from folders (especially useful for studies)">0</DeletePlotsBeforeRun>
+ <ClearOldLogFilesAtStart Default="1" Desc="Clear all Subtool logfiles at start">1</ClearOldLogFilesAtStart>
+ <CreatePlotForCalculationHistory Default="0" Desc="0: no plot for calculation history created; 1: plot for calculation history created">0</CreatePlotForCalculationHistory>
+ <SwitchOffPlots Default="1" Desc="1: Switch Off Plots during Design Iteration">1</SwitchOffPlots>
+ <SaveAcftXmlAfterIteration Default="1" Desc="1: Acft-XML is buffered after each iteration">1</SaveAcftXmlAfterIteration>
+ <CheckoutProgramsFromRepository CheckoutDepth="1" Default="1" DeleteSrcDirs="0" Desc="1: If program folder does not exist, automatic checkout from Git server." ExitAfterCheckout="1" PrivateOpenSSHkey="DEFAULT" Timeout="30">1</CheckoutProgramsFromRepository>
+ <DesignCase>
+ <Mode Default="0" Desc="0: Standard (no checks in subprograms), 1: Clean Sheet Design, 2: Design with existing geometry">1</Mode>
+ <Calibration>
+ <CalibrateToTargetValues Default="0" Desc="1: use target values for MTOM and OME (see below)">0</CalibrateToTargetValues>
+ <TargetMTOM Desc="Given MTOM">77000</TargetMTOM>
+ <TargetOME Desc="Given OME (can be skipped, if already calibrated)" Skip="0">42100</TargetOME>
+ <FreeVariableOMECal Default="1" Desc="1: massEstimation (fuselage)" ResetAtStart="1">1</FreeVariableOMECal>
+ <FreeVariableMTOMCal Default="1" Desc="1: engineSizing (FuelFlow), 2:calculatePolar (DragReduction)" ResetBothVariablesAtStart="0" ResetUsedVariableAtStart="0">1</FreeVariableMTOMCal>
+ <NumberOfIterations Default="4" Desc="Number of iterations after which each MTOM calibration is performed">4</NumberOfIterations>
+ <MaxIterationsBeforeExitOMECal Default="20" Desc="Number of iterations before the OME calibration is canceled by exit(1)">20</MaxIterationsBeforeExitOMECal>
+ <TruncErrorFactor Default="125" Desc="Termination criterion: As factor regarding convergenceCriteria (see below)">125</TruncErrorFactor>
+ <Damp_MTOM_Calibration_Lever Default="0" Desc="Switch for damping MTOM calibration lever arm" x_rel_max="2">0</Damp_MTOM_Calibration_Lever>
+ <Damp_OME_Calibration_Lever Default="0" Desc="Switch for damping OME calibration lever arm" x_rel_max="2">0</Damp_OME_Calibration_Lever>
+ </Calibration>
+ <PayloadRangeAnalysis Desc="for determination of points on PL-Range diagram (not suitable for input of values)">
+ <ExitIfMTOMLimitReached AllowedRelOvershoot="0." Default="1" Desc="1: Program abort, if TOM ge MTOM (in Study Mode)">1</ExitIfMTOMLimitReached>
+ <ExitIfFuelLimitReached AllowedRelOvershoot="0." Default="1" Desc="1: Program abort, if fuel estimated ge MFM">1</ExitIfFuelLimitReached>
+ <DeltaTOMtoMTOM Desc="MTOM - TOM (study mission)" Unit="kg">15797.9102</DeltaTOMtoMTOM>
+ <DeltaFueltoMFM Desc="MFM - Mission Fuel (study mission)" Unit="kg">25016.84771</DeltaFueltoMFM>
+ <LeastSquareDelta Desc="sqrt(pow(deltaFuel,2)+pow(deltaTOM,2))" Unit="kg">29587.44051</LeastSquareDelta>
+ </PayloadRangeAnalysis>
+ <RangeTypeSpecificFactors Default="0" Des="Adapt aircraft specific factors in all used modules. Mode 0: No adaptation, Mode 1: based on design range, 2: short-range, 3: mid-range, 4: long-range">0</RangeTypeSpecificFactors>
+ </DesignCase>
+ <AutomaticTrim Default="1" Desc="Trim is automated">1</AutomaticTrim>
+ </ProgramSpecific>
+ <ATLASupportFiles>
+ <FileName type="OperatingCompany">operating_company.xml</FileName>
+ <FileName type="Scenario">scenario.xml</FileName>
+ </ATLASupportFiles>
+ </ControlSettings>
+ <ProgramSettings Desc="program settings">
+ <convergenceCriteria Default="0.0025" Desc="permitted relative change to achieve convergence" Unit="-">0.0001</convergenceCriteria>
+ <DampMTOMIteration Default="0" Desc="1: Mean value of the last 2 MTOM values is used to suppress vibrations if necessary.">1</DampMTOMIteration>
+ <DampOMEIteration Default="0" Desc="1: Mean value of the last 2 OME values is used to suppress vibrations if necessary.">0</DampOMEIteration>
+ <maxIterationsBeforeExitSizingLoop Default="30" Desc="Number of iterations before the loop is aborted by exit(1)">30</maxIterationsBeforeExitSizingLoop>
+ <SetupSteps Desc="Programs that are executed once in study mode">
+ <NumberPrograms Default="2" Desc="Number of programs before iteration">2</NumberPrograms>
+ <Program Desc="Path and program name" ID="1" maxRuntime_in_minutes="10">
+ <Name Default="initialSizing.exe" Desc="Name">initialSizing</Name>
+ <Directory Default="../01_initialSizing/" Desc="Path">../01_initialSizing/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="2" maxRuntime_in_minutes="10">
+ <Name Default="fuselageDesign.exe" Desc="Name">fuselageDesign</Name>
+ <Directory Default="../02_fuselageDesign/" Desc="Path">../02_fuselageDesign/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ </SetupSteps>
+ <SizingLoop Desc="Programs in the Convergence Loop" Iterate="1">
+ <NumberPrograms Default="10" Desc="Number of programs in the loop">10</NumberPrograms>
+ <Program Desc="Path and program name" ID="1" maxRuntime_in_minutes="10">
+ <Name Default="createMissionXML.exe" Desc="Name">createMissionXML</Name>
+ <Directory Default="../10_createMissionXML/" Desc="Pfad">../10_createMissionXML/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="7" maxRuntime_in_minutes="10">
+ <Name Default="wingDesign.exe" Desc="Name">wingDesign</Name>
+ <Directory Default="../11_wingDesign/" Desc="Pfad">../11_wingDesign/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="4" maxRuntime_in_minutes="10">
+ <Name Default="empenageSizing.exe" Desc="Name">empennageSizing</Name>
+ <Directory Default="../12_empennageSizing/" Desc="Path">../12_empennageSizing/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="3" maxRuntime_in_minutes="10">
+ <Name Default="engineSizing.exe" Desc="Name">engineSizing</Name>
+ <Directory Default="../13_engineSizing/" Desc="Path">../13_engineSizing/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="5" maxRuntime_in_minutes="10">
+ <Name Default="propulsionIntegration.exe" Desc="Name">propulsionIntegration</Name>
+ <Directory Default="../14_propulsionIntegration/" Desc="Path">../14_propulsionIntegration/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="2" maxRuntime_in_minutes="10">
+ <Name Default="landingGearDesign.exe" Desc="Name">landingGearDesign</Name>
+ <Directory Default="../15_landingGearDesign/" Desc="Path">../15_landingGearDesign/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="6" maxRuntime_in_minutes="10">
+ <Name Default="calculatePolar.exe" Desc="Name">calculatePolar</Name>
+ <Directory Default="../21_calculatePolar/" Desc="Path">../21_calculatePolar/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="8" maxRuntime_in_minutes="10">
+ <Name Default="massEstimation.exe" Desc="Name">massEstimation</Name>
+ <Directory Default="../22_massEstimation/" Desc="Path">../22_massEstimation/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="9" maxRuntime_in_minutes="10">
+ <Name Default="systemsDesign.exe" Desc="Name">systemsDesign</Name>
+ <Directory Default="../23_systemsDesign/" Desc="Path">../23_systemsDesign/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="10" maxRuntime_in_minutes="10">
+ <Name Default="missionAnalysis.exe" Desc="Name">missionAnalysis</Name>
+ <Directory Default="../31_missionAnalysis/" Desc="Path">../31_missionAnalysis/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ </SizingLoop>
+ <StudyMission Desc="Analyse for StudyMission" Iterate="1" TruncError="0.001">
+ <NumberPrograms Default="3" Desc="Number of programs for StudyMission">3</NumberPrograms>
+ <Program Desc="Path and program name" ID="1" maxRuntime_in_minutes="10">
+ <Name Default="createMissionXML.exe" Desc="Name">createMissionXML</Name>
+ <Directory Default="../10_createMissionXML/" Desc="Path">../10_createMissionXML/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="2" maxRuntime_in_minutes="10">
+ <Name Default="systemsDesign.exe" Desc="Name">systemsDesign</Name>
+ <Directory Default="../23_systemsDesign/" Desc="Path">../23_systemsDesign/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="3" maxRuntime_in_minutes="10">
+ <Name Default="missionAnalysis.exe" Desc="Name">missionAnalysis</Name>
+ <Directory Default="../31_missionAnalysis/" Desc="Path">../31_missionAnalysis/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ </StudyMission>
+ <PostprocessingSteps Desc="Programs that are executed once in study mode">
+ <NumberPrograms Default="2" Desc="Number of programs in postprocessing">8</NumberPrograms>
+ <Program Desc="Path and program name" ID="1" maxRuntime_in_minutes="10" type="std">
+ <Name Default="calculatePerformance.exe" Desc="Name">calculatePerformance</Name>
+ <Directory Default="../51_calculatePerformance/" Desc="Path">../51_calculatePerformance/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rAIRCRAFTDESIGN:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="2" maxRuntime_in_minutes="10" type="std">
+ <Name Default="calculateCosts.exe" Desc="Name">calculateCosts</Name>
+ <Directory Default="../52_calculateCosts/" Desc="Path">../52_calculateCosts/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rADDITIONALTOOLS:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="3" maxRuntime_in_minutes="10" type="std">
+ <Name Default="estimateDOC.exe" Desc="Name">estimateDOC</Name>
+ <Directory Default="../53_estimateDOC/" Desc="Path">../53_estimateDOC/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rADDITIONALTOOLS:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="4" maxRuntime_in_minutes="10" type="std">
+ <Name Default="calculateCosts.exe" Desc="Name">calculateCosts</Name>
+ <Directory Default="../52_calculateCosts/" Desc="Path">../52_calculateCosts/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rADDITIONALTOOLS:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="5" maxRuntime_in_minutes="10" type="std">
+ <Name Default="calculateEmissions.exe" Desc="Name">calculateEmissions</Name>
+ <Directory Default="../54_calculateEmissions/" Desc="Path">../54_calculateEmissions/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rADDITIONALTOOLS:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="6" maxRuntime_in_minutes="10" type="std">
+ <Name Default="reportGenerator.exe" Desc="Name">reportGenerator</Name>
+ <Directory Default="../91_reportGenerator/" Desc="Path">../91_reportGenerator/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rADDITIONALSOFTWARE:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="7" maxRuntime_in_minutes="10" type="std">
+ <Name Default="cpacsInterface.exe" Desc="Name">cpacsInterface</Name>
+ <Directory Default="../92_cpacsInterface/" Desc="Path">../92_cpacsInterface/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rADDITIONALSOFTWARE:master</Source>
+ </Program>
+ <Program Desc="Path and program name" ID="8" maxRuntime_in_minutes="10" type="std">
+ <Name Default="designEvaluator.exe" Desc="Name">designEvaluator</Name>
+ <Directory Default="../93_designEvaluator/" Desc="Path">../93_designEvaluator/</Directory>
+ <Source Desc="Source of tool. Repository: local - Set path to local tool directoryDefault; server - Set path to git repository:branch" Repository="server">rADDITIONALSOFTWARE:master</Source>
+ </Program>
+ </PostprocessingSteps>
+ </ProgramSettings>
+</ConfigFile>
diff --git a/UnicadoGUI/Backend/xml_configs/createMissionXML_conf.xml b/UnicadoGUI/Backend/xml_configs/createMissionXML_conf.xml
new file mode 100644
index 0000000..5723202
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/createMissionXML_conf.xml
@@ -0,0 +1,255 @@
+<?xml version="1.0" encoding="utf-8"?>
+<module_configuration_file name="createMissionXML_conf.xml">
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>CSR-02.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>../projects/CSR/CSR-02/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>3</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>false</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>true</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>false</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>create_mission_xml_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>create_mission_xml.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings description="Program Settings">
+ <mission_choice description="Pick a mission (by now only 1 implemented): standard">
+ <value>standard</value>
+ </mission_choice>
+ <maximum_operating_mach_number description="Specify the maximum operating Mach number by its delta to the initial cruise Mach number">
+ <enable description="Switch to enable the specification via initial cruise Mach number + delta ('true': On, 'false': Off-> read from aircraft exchange file)">
+ <value>false</value>
+ </enable>
+ <delta description="Difference between maximum operating Mach number (MMO) and initial cruise (IC) Mach number: delta = MMO - IC">
+ <value>0.04</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </delta>
+ </maximum_operating_mach_number>
+ <adapt_climb_speed_schedule description="Second calibrated airspeed (CAS) within climb adapted to crossover altitude">
+ <enable description="Switch to enable crossover altitude adaption ('true': On, 'false': Off)">
+ <value>false</value>
+ </enable>
+ <crossover_altitude description="Crossover altitude to which the second calibrated airspeed (CAS) shall be adapted">
+ <value>30000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>50000</upper_boundary>
+ </crossover_altitude>
+ </adapt_climb_speed_schedule>
+ <climb_thrust_setting description="Selector to set the thrust rating within climb/acceleration segments to 'mode_0': Takeoff, 'mode_1': Climb, 'mode_2': Maximum continuous, 'mode_3': Cruise">
+ <value>mode_1</value>
+ </climb_thrust_setting>
+ <maximum_rate_of_climb description="Limit the rate of climb (ROC) to a preset value during Climb segments; values less then 0: Use full thrust as limit">
+ <value>-1</value>
+ <unit>ft/min</unit>
+ <lower_boundary>-1</lower_boundary>
+ <upper_boundary>5000</upper_boundary>
+ </maximum_rate_of_climb>
+ <write_requirement_mission description="Switch if a mission file for requirement check mission shall be created ('true': On, 'false': Off)">
+ <value>true</value>
+ </write_requirement_mission>
+ <design_mission>
+ <write_mission_file description="Switch if a mission file for the design mission shall be created ('true': On, 'false': Off)">
+ <value>true</value>
+ </write_mission_file>
+ <output_file_name description="Specify the name of the created mission file">
+ <value>mission_design.xml</value>
+ </output_file_name>
+ <terminal_operation_time description="Specify the time at the terminal for stopovers">
+ <value>25</value>
+ <unit>min</unit>
+ <lower_boundary>5</lower_boundary>
+ <upper_boundary>10000</upper_boundary>
+ </terminal_operation_time>
+ <takeoff_procedure description="Selector for the takeoff procedure. 'mode_0': standard, 'mode_1': ICAO-A Take-Off Procedure (not implemented yet), 'mode_2': ICAO-A Take-Off Procedure (not implemented yet), 'mode_3': Standard 19 seat commuter">
+ <value>mode_0</value>
+ </takeoff_procedure>
+ <approach_procedure description="Selector for the approach procedure. 'mode_0': standard, 'mode_1': Continuous descent approach (not implemented yet), 'mode_2': steep Continuous descent approach (not implemented yet), 'mode_3': Standard 19 seat commuter">
+ <value>mode_0</value>
+ </approach_procedure>
+ <taxi_time_origin description="Time needed for taxiing at origin.">
+ <value>9</value>
+ <unit>min</unit>
+ <lower_boundary>0.1</lower_boundary>
+ <upper_boundary>30</upper_boundary>
+ </taxi_time_origin>
+ <taxi_time_destination description="Time needed for taxiing at destination.">
+ <value>5</value>
+ <unit>min</unit>
+ <lower_boundary>0.1</lower_boundary>
+ <upper_boundary>30</upper_boundary>
+ </taxi_time_destination>
+ <auto_select_initial_cruise_altitude description="Switch to activate automatic selection of the initial cruise altitude (ICA) ('true': On [ICA design: FL330, ICA study: FL350], 'false': Off)">
+ <value>false</value>
+ </auto_select_initial_cruise_altitude>
+ <auto_select_flight_level description="Specify if and how the flight level selection is automated">
+ <enable description="Switch to activate automatic selection of the flight level ('true': On, 'false': Off)">
+ <value>false</value>
+ </enable>
+ <no_steps description="Switch to never change from initial cruise altitude (ICA) -> ICA = altitude for whole cruise ('true': On, 'false': Off)">
+ <value>false</value>
+ </no_steps>
+ </auto_select_flight_level>
+ <round_to_regular_flight_level description="Switch to round to flight levels (FL) within 20 FL (= 2000 ft) intervals; e.g. FL 330 or 350 ('true': On, 'false': Off)">
+ <value>true</value>
+ </round_to_regular_flight_level>
+ <auto_climb_altitude_steps description="Altitude step distance in cruise flight with automatic altitude adjustment">
+ <value>2000</value>
+ <unit>ft</unit>
+ <lower_boundary>500</lower_boundary>
+ <upper_boundary>50000</upper_boundary>
+ </auto_climb_altitude_steps>
+ <auto_rate_of_climb_steps description="Rate of climb steps in cruise with automatic altitude adjustment">
+ <value>300</value>
+ <unit>ft/min</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5000</upper_boundary>
+ </auto_rate_of_climb_steps>
+ <alternate_distance description="Distance from destination to alternate aerodrome">
+ <value>370400.2</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>926000</upper_boundary>
+ </alternate_distance>
+ <engine_warmup_time description="Running time of the engines before take-off">
+ <value>0</value>
+ <unit>min</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>30</upper_boundary>
+ </engine_warmup_time>
+ <electric_taxiing_switch description="mode_0: Propulsion Taxiing; mode_1: Electric Taxiing">
+ <value>mode_0</value>
+ </electric_taxiing_switch>
+ <origin_airport description="ICAO code of origin - leave empty if no specific airport shall be selected">
+ <value></value>
+ </origin_airport>
+ <destination_airport description="ICAO code of destination - leave empty if no specific airport shall be selected">
+ <value></value>
+ </destination_airport>
+ </design_mission>
+ <study_mission>
+ <write_mission_file description="Switch if a mission file for the study mission shall be created ('true': On, 'false': Off)">
+ <value>true</value>
+ </write_mission_file>
+ <copy_mach_number description="Switch if the Mach number is copied from the design mission's requirements block ('true': On, 'false': Off; only for parameter studies with Mach number variation)">
+ <value>false</value>
+ </copy_mach_number>
+ <copy_initial_cruise_altitude description="Switch if the initial cruise altitude (ICA) is copied from the design mission's requirements block ('true': On, 'false': Off; only for parameter studies with ICA variation without altitude optimization)">
+ <value>false</value>
+ </copy_initial_cruise_altitude>
+ <output_file_name description="Specify the name of the created mission file">
+ <value>mission_study.xml</value>
+ </output_file_name>
+ <terminal_operation_time description="Specify the time at the terminal for stopovers">
+ <value>25</value>
+ <unit>min</unit>
+ <lower_boundary>5</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </terminal_operation_time>
+ <takeoff_procedure description="Selector for the takeoff procedure. 'mode_0': standard, 'mode_1': Standard 19 seat commuter">
+ <value>mode_0</value>
+ </takeoff_procedure>
+ <approach_procedure description="Selector for the approach procedure. 'mode_0': standard, 'mode_1': Standard 19 seat commuter">
+ <value>mode_0</value>
+ </approach_procedure>
+ <taxi_time_origin description="Time needed for taxiing at origin.">
+ <value>9</value>
+ <unit>min</unit>
+ <lower_boundary>0.1</lower_boundary>
+ <upper_boundary>30</upper_boundary>
+ </taxi_time_origin>
+ <taxi_time_destination description="Time needed for taxiing at destination.">
+ <value>5</value>
+ <unit>min</unit>
+ <lower_boundary>0.1</lower_boundary>
+ <upper_boundary>30</upper_boundary>
+ </taxi_time_destination>
+ <auto_select_initial_cruise_altitude description="Switch to activate automatic selection of the initial cruise altitude (ICA) ('true': On [ICA design: FL330, ICA study: FL350], 'false': Off)">
+ <value>false</value>
+ </auto_select_initial_cruise_altitude>
+ <auto_select_flight_level description="Specify if and how the flight level selection is automated">
+ <enable description="Switch to activate automatic selection of the flight level ('true': On, 'false': Off)">
+ <value>false</value>
+ </enable>
+ <no_steps description="Switch to never change from initial cruise altitude (ICA) -> ICA = altitude for whole cruise ('true': On, 'false': Off)">
+ <value>false</value>
+ </no_steps>
+ </auto_select_flight_level>
+ <round_to_regular_flight_level description="Switch to round to flight levels (FL) within 20 FL (= 2000 ft) intervals; e.g. FL 330 or 350 ('true': On, 'false': Off)">
+ <value>true</value>
+ </round_to_regular_flight_level>
+ <auto_climb_altitude_steps description="Altitude step distance in cruise flight with automatic altitude adjustment">
+ <value>2000</value>
+ <unit>ft</unit>
+ <lower_boundary>500</lower_boundary>
+ <upper_boundary>50000</upper_boundary>
+ </auto_climb_altitude_steps>
+ <auto_rate_of_climb_steps description="Rate of climb steps in cruise with automatic altitude adjustment">
+ <value>300</value>
+ <unit>ft/min</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5000</upper_boundary>
+ </auto_rate_of_climb_steps>
+ <alternate_distance description="Distance from destination to alternate aerodrome">
+ <value>370400.2</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>926000</upper_boundary>
+ </alternate_distance>
+ <engine_warmup_time description="Running time of the engines before take-off">
+ <value>0</value>
+ <unit>min</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>30</upper_boundary>
+ </engine_warmup_time>
+ <electric_taxiing_switch description="mode_0: Propulsion Taxiing; mode_1: Electric Taxiing">
+ <value>mode_0</value>
+ </electric_taxiing_switch>
+ <origin_airport description="ICAO code of origin - leave empty if no specific airport shall be selected">
+ <value></value>
+ </origin_airport>
+ <destination_airport description="ICAO code of destination - leave empty if no specific airport shall be selected">
+ <value></value>
+ </destination_airport>
+ </study_mission>
+ </program_settings>
+</module_configuration_file>
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/xml_configs/createMissionXML_conf_default.xml b/UnicadoGUI/Backend/xml_configs/createMissionXML_conf_default.xml
new file mode 100644
index 0000000..ef4019e
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/createMissionXML_conf_default.xml
@@ -0,0 +1,255 @@
+<?xml version="1.0" encoding="utf-8" ?>
+<module_configuration_file name="createMissionXML_conf.xml">
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>CSR-02.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>../projects/CSR/CSR-02/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>3</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>false</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>true</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>false</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>create_mission_xml_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>create_mission_xml.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings description="Program Settings">
+ <mission_choice description="Pick a mission (by now only 1 implemented): standard">
+ <value>standard</value>
+ </mission_choice>
+ <maximum_operating_mach_number description="Specify the maximum operating Mach number by its delta to the initial cruise Mach number">
+ <enable description="Switch to enable the specification via initial cruise Mach number + delta ('true': On, 'false': Off-> read from aircraft exchange file)">
+ <value>false</value>
+ </enable>
+ <delta description="Difference between maximum operating Mach number (MMO) and initial cruise (IC) Mach number: delta = MMO - IC">
+ <value>0.04</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </delta>
+ </maximum_operating_mach_number>
+ <adapt_climb_speed_schedule description="Second calibrated airspeed (CAS) within climb adapted to crossover altitude">
+ <enable description="Switch to enable crossover altitude adaption ('true': On, 'false': Off)">
+ <value>false</value>
+ </enable>
+ <crossover_altitude description="Crossover altitude to which the second calibrated airspeed (CAS) shall be adapted">
+ <value>30000</value>
+ <unit>ft</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>50000</upper_boundary>
+ </crossover_altitude>
+ </adapt_climb_speed_schedule>
+ <climb_thrust_setting description="Selector to set the thrust rating within climb/acceleration segments to 'mode_0': Takeoff, 'mode_1': Climb, 'mode_2': Maximum continuous, 'mode_3': Cruise">
+ <value>mode_1</value>
+ </climb_thrust_setting>
+ <maximum_rate_of_climb description="Limit the rate of climb (ROC) to a preset value during Climb segments; values less then 0: Use full thrust as limit">
+ <value>-1</value>
+ <unit>ft/min</unit>
+ <lower_boundary>-1</lower_boundary>
+ <upper_boundary>5000</upper_boundary>
+ </maximum_rate_of_climb>
+ <write_requirement_mission description="Switch if a mission file for requirement check mission shall be created ('true': On, 'false': Off)">
+ <value>true</value>
+ </write_requirement_mission>
+ <design_mission>
+ <write_mission_file description="Switch if a mission file for the design mission shall be created ('true': On, 'false': Off)">
+ <value>true</value>
+ </write_mission_file>
+ <output_file_name description="Specify the name of the created mission file">
+ <value>mission_design.xml</value>
+ </output_file_name>
+ <terminal_operation_time description="Specify the time at the terminal for stopovers">
+ <value>25</value>
+ <unit>min</unit>
+ <lower_boundary>5</lower_boundary>
+ <upper_boundary>10000</upper_boundary>
+ </terminal_operation_time>
+ <takeoff_procedure description="Selector for the takeoff procedure. 'mode_0': standard, 'mode_1': ICAO-A Take-Off Procedure (not implemented yet), 'mode_2': ICAO-A Take-Off Procedure (not implemented yet), 'mode_3': Standard 19 seat commuter">
+ <value>mode_0</value>
+ </takeoff_procedure>
+ <approach_procedure description="Selector for the approach procedure. 'mode_0': standard, 'mode_1': Continuous descent approach (not implemented yet), 'mode_2': steep Continuous descent approach (not implemented yet), 'mode_3': Standard 19 seat commuter">
+ <value>mode_0</value>
+ </approach_procedure>
+ <taxi_time_origin description="Time needed for taxiing at origin.">
+ <value>9</value>
+ <unit>min</unit>
+ <lower_boundary>0.1</lower_boundary>
+ <upper_boundary>30</upper_boundary>
+ </taxi_time_origin>
+ <taxi_time_destination description="Time needed for taxiing at destination.">
+ <value>5</value>
+ <unit>min</unit>
+ <lower_boundary>0.1</lower_boundary>
+ <upper_boundary>30</upper_boundary>
+ </taxi_time_destination>
+ <auto_select_initial_cruise_altitude description="Switch to activate automatic selection of the initial cruise altitude (ICA) ('true': On [ICA design: FL330, ICA study: FL350], 'false': Off)">
+ <value>false</value>
+ </auto_select_initial_cruise_altitude>
+ <auto_select_flight_level description="Specify if and how the flight level selection is automated">
+ <enable description="Switch to activate automatic selection of the flight level ('true': On, 'false': Off)">
+ <value>false</value>
+ </enable>
+ <no_steps description="Switch to never change from initial cruise altitude (ICA) -> ICA = altitude for whole cruise ('true': On, 'false': Off)">
+ <value>false</value>
+ </no_steps>
+ </auto_select_flight_level>
+ <round_to_regular_flight_level description="Switch to round to flight levels (FL) within 20 FL (= 2000 ft) intervals; e.g. FL 330 or 350 ('true': On, 'false': Off)">
+ <value>true</value>
+ </round_to_regular_flight_level>
+ <auto_climb_altitude_steps description="Altitude step distance in cruise flight with automatic altitude adjustment">
+ <value>2000</value>
+ <unit>ft</unit>
+ <lower_boundary>500</lower_boundary>
+ <upper_boundary>50000</upper_boundary>
+ </auto_climb_altitude_steps>
+ <auto_rate_of_climb_steps description="Rate of climb steps in cruise with automatic altitude adjustment">
+ <value>300</value>
+ <unit>ft/min</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5000</upper_boundary>
+ </auto_rate_of_climb_steps>
+ <alternate_distance description="Distance from destination to alternate aerodrome">
+ <value>370400.2</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>926000</upper_boundary>
+ </alternate_distance>
+ <engine_warmup_time description="Running time of the engines before take-off">
+ <value>0</value>
+ <unit>min</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>30</upper_boundary>
+ </engine_warmup_time>
+ <electric_taxiing_switch description="mode_0: Propulsion Taxiing; mode_1: Electric Taxiing">
+ <value>mode_0</value>
+ </electric_taxiing_switch>
+ <origin_airport description="ICAO code of origin - leave empty if no specific airport shall be selected">
+ <value></value>
+ </origin_airport>
+ <destination_airport description="ICAO code of destination - leave empty if no specific airport shall be selected">
+ <value></value>
+ </destination_airport>
+ </design_mission>
+ <study_mission>
+ <write_mission_file description="Switch if a mission file for the study mission shall be created ('true': On, 'false': Off)">
+ <value>true</value>
+ </write_mission_file>
+ <copy_mach_number description="Switch if the Mach number is copied from the design mission's requirements block ('true': On, 'false': Off; only for parameter studies with Mach number variation)">
+ <value>false</value>
+ </copy_mach_number>
+ <copy_initial_cruise_altitude description="Switch if the initial cruise altitude (ICA) is copied from the design mission's requirements block ('true': On, 'false': Off; only for parameter studies with ICA variation without altitude optimization)">
+ <value>false</value>
+ </copy_initial_cruise_altitude>
+ <output_file_name description="Specify the name of the created mission file">
+ <value>mission_study.xml</value>
+ </output_file_name>
+ <terminal_operation_time description="Specify the time at the terminal for stopovers">
+ <value>25</value>
+ <unit>min</unit>
+ <lower_boundary>5</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </terminal_operation_time>
+ <takeoff_procedure description="Selector for the takeoff procedure. 'mode_0': standard, 'mode_1': Standard 19 seat commuter">
+ <value>mode_0</value>
+ </takeoff_procedure>
+ <approach_procedure description="Selector for the approach procedure. 'mode_0': standard, 'mode_1': Standard 19 seat commuter">
+ <value>mode_0</value>
+ </approach_procedure>
+ <taxi_time_origin description="Time needed for taxiing at origin.">
+ <value>9</value>
+ <unit>min</unit>
+ <lower_boundary>0.1</lower_boundary>
+ <upper_boundary>30</upper_boundary>
+ </taxi_time_origin>
+ <taxi_time_destination description="Time needed for taxiing at destination.">
+ <value>5</value>
+ <unit>min</unit>
+ <lower_boundary>0.1</lower_boundary>
+ <upper_boundary>30</upper_boundary>
+ </taxi_time_destination>
+ <auto_select_initial_cruise_altitude description="Switch to activate automatic selection of the initial cruise altitude (ICA) ('true': On [ICA design: FL330, ICA study: FL350], 'false': Off)">
+ <value>false</value>
+ </auto_select_initial_cruise_altitude>
+ <auto_select_flight_level description="Specify if and how the flight level selection is automated">
+ <enable description="Switch to activate automatic selection of the flight level ('true': On, 'false': Off)">
+ <value>false</value>
+ </enable>
+ <no_steps description="Switch to never change from initial cruise altitude (ICA) -> ICA = altitude for whole cruise ('true': On, 'false': Off)">
+ <value>false</value>
+ </no_steps>
+ </auto_select_flight_level>
+ <round_to_regular_flight_level description="Switch to round to flight levels (FL) within 20 FL (= 2000 ft) intervals; e.g. FL 330 or 350 ('true': On, 'false': Off)">
+ <value>true</value>
+ </round_to_regular_flight_level>
+ <auto_climb_altitude_steps description="Altitude step distance in cruise flight with automatic altitude adjustment">
+ <value>2000</value>
+ <unit>ft</unit>
+ <lower_boundary>500</lower_boundary>
+ <upper_boundary>50000</upper_boundary>
+ </auto_climb_altitude_steps>
+ <auto_rate_of_climb_steps description="Rate of climb steps in cruise with automatic altitude adjustment">
+ <value>300</value>
+ <unit>ft/min</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5000</upper_boundary>
+ </auto_rate_of_climb_steps>
+ <alternate_distance description="Distance from destination to alternate aerodrome">
+ <value>370400.2</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>926000</upper_boundary>
+ </alternate_distance>
+ <engine_warmup_time description="Running time of the engines before take-off">
+ <value>0</value>
+ <unit>min</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>30</upper_boundary>
+ </engine_warmup_time>
+ <electric_taxiing_switch description="mode_0: Propulsion Taxiing; mode_1: Electric Taxiing">
+ <value>mode_0</value>
+ </electric_taxiing_switch>
+ <origin_airport description="ICAO code of origin - leave empty if no specific airport shall be selected">
+ <value></value>
+ </origin_airport>
+ <destination_airport description="ICAO code of destination - leave empty if no specific airport shall be selected">
+ <value></value>
+ </destination_airport>
+ </study_mission>
+ </program_settings>
+</module_configuration_file>
diff --git a/UnicadoGUI/Backend/xml_configs/initialSizing_conf.xml b/UnicadoGUI/Backend/xml_configs/initialSizing_conf.xml
new file mode 100644
index 0000000..3bf81bd
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/initialSizing_conf.xml
@@ -0,0 +1,167 @@
+<?xml version="1.0" encoding="utf-8"?>
+<module_configuration_file name="initialSizing_conf.xml">
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>template.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>X:/UNICADO/rUNICADO/aircraftReferences/CSR/CSR-02/cleanSheetDesign/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>1</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>true</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>false</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>TOOLNAME_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>TOOLNAME.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>C:/Programs/UNICADOworkflow/inkscape/</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>C:/Programs/UNICADOworkflow/gnuplot/</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings Desc="program settings">
+ <design_case description="Switch for system sizing. 1: Sizing, 0: ONLY determination of a load profile for a specific mission">
+ <value>1</value>
+ <default>1</default>
+ </design_case>
+ <tube_and_wing description="settings for tube and wing (TAW)">
+ <approach_selection description="selection of approach level">
+ <value>analytical</value>
+ </approach_selection>
+ <analytical_approach>
+ <General>
+ <OswaldFactor Desc="Oswald factor in clean configuration" Unit="-">
+ <value>0.85</value>
+ <default>0.85</default>
+ </OswaldFactor>
+ <AspectRatio Desc="aspect ratio" Unit="count">
+ <value>9.5</value>
+ <default>9.5</default>
+ </AspectRatio>
+ <n_pilots Desc="Number of Pilots" Unit="count">
+ <value>2</value>
+ <default>2</default>
+ </n_pilots>
+ <n_engines Desc="Number of engines" Unit="count">
+ <value>2</value>
+ <default>2</default>
+ </n_engines>
+ <Cf Desc="friction coefficient" Unit="count">
+ <value>0.002</value>
+ <default>0.002</default>
+ </Cf>
+ </General>
+ <Constants>
+ <SFC_kerosene Desc="Specific Fuel Consumption Factor for Kerosene">
+ <value>0.0001389</value>
+ <default>0.0001389</default>
+ </SFC_kerosene>
+ </Constants>
+ <TOFL Desc="takeoff distance requirement">
+ <CLmax_TO Desc="Maximum lift coefficient at takeoff" Unit="-">
+ <value>2.28</value>
+ <default>2.28</default>
+ </CLmax_TO>
+ </TOFL>
+ <LDN Desc="landing distance requirement">
+ <CLmax_L Desc="Maximum lift coefficient at landing" Unit="-">
+ <value>2.85</value>
+ <default>2.85</default>
+ </CLmax_L>
+ <mlmo Desc="ratio between maximum landing mass and takeoff mass" Unit="-">
+ <value>0.82</value>
+ <default>0.82</default>
+ </mlmo>
+ </LDN>
+ <Climb Desc="climb performance requirement">
+ <deltaCD_HL Desc="Delta CD0 with TO-Flaps" Unit="-">
+ <value>0.07</value>
+ <default>0.07</default>
+ </deltaCD_HL>
+ </Climb>
+ <Cruise Desc="maximum cruise speed requirement">
+ <mcr_mto Desc="ratio between cruise mass and takeoff mass - default for mid- and short-range: 0.956, default for long range: 0.924">
+ <value>0.956</value>
+ <default>0.956</default>
+ </mcr_mto>
+ <optimalCL Desc="maximum CL at initial cruise">
+ <value>0.57</value>
+ <default>0.57</default>
+ </optimalCL>
+ </Cruise>
+ <LiftToDragRatios Desc="initial cruise and loiter lift to drag ratios ">
+ <LD_initial_cruise Desc="cruise requirements">
+ <value>15</value>
+ <default>15</default>
+ </LD_initial_cruise>
+ <LD_initial_loiter Desc="loiter requirements">
+ <value>16</value>
+ <default>16</default>
+ </LD_initial_loiter>
+ </LiftToDragRatios>
+ <Masses Desc="mass estimation methodology">
+ <Fractions Desc="mass fractions">
+ <mf_warmup Desc="Warmup (according to Raymer: 0.97(A340)-0.99(A320))" Unit="-" Default="0.99">
+ <value>0.99</value>
+ <default>0.99</default>
+ </mf_warmup>
+ <mf_taxi Desc="Warmup (according to Raymer: 0.97(A340)-0.99(A320))" Unit="-" Default="0.99">
+ <value>0.99</value>
+ <default>0.99</default>
+ </mf_taxi>
+ <mf_to Desc="Taxi and Takeoff (according to Raymer: 0.97(A340)-0.99(A320))" Unit="-" Default="0.995">
+ <value>0.995</value>
+ <default>0.995</default>
+ </mf_to>
+ <mf_climb Desc="Climb (according to Raymer: 0.97(A340)-0.99(A320))" Unit="-" Default="0.98">
+ <value>0.98</value>
+ <default>0.98</default>
+ </mf_climb>
+ <mf_descent Desc="Descent (according to Raymer: 0.99(A340)-0.995(A320))" Unit="-" Default="0.99">
+ <value>0.99</value>
+ <default>0.99</default>
+ </mf_descent>
+ <mf_missedandclimb Desc="Landing and Taxi Back (according to Raymer: 0.992(A340)-0.997(A320))" Unit="-" Default="0.988">
+ <value>0.988</value>
+ <default>0.988</default>
+ </mf_missedandclimb>
+ <mf_land Desc="Landing and Taxi Back (according to Raymer: 0.992(A340)-0.997(A320))" Unit="-" Default="0.995">
+ <value>0.995</value>
+ <default>0.995</default>
+ </mf_land>
+ </Fractions>
+ </Masses>
+ </analytical_approach>
+ </tube_and_wing>
+ </program_settings>
+</module_configuration_file>
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/xml_configs/initialSizing_conf_default.xml b/UnicadoGUI/Backend/xml_configs/initialSizing_conf_default.xml
new file mode 100644
index 0000000..fbb78c8
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/initialSizing_conf_default.xml
@@ -0,0 +1,167 @@
+<?xml version="1.0" encoding="utf-8" ?>
+<module_configuration_file name="initialSizing_conf.xml">
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>template.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>X:/UNICADO/rUNICADO/aircraftReferences/CSR/CSR-02/cleanSheetDesign/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>1</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>true</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>false</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>TOOLNAME_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>TOOLNAME.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>C:/Programs/UNICADOworkflow/inkscape/</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>C:/Programs/UNICADOworkflow/gnuplot/</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings Desc="program settings">
+ <design_case description="Switch for system sizing. 1: Sizing, 0: ONLY determination of a load profile for a specific mission">
+ <value>1</value>
+ <default>1</default>
+ </design_case>
+ <tube_and_wing description="settings for tube and wing (TAW)">
+ <approach_selection description="selection of approach level">
+ <value>analytical</value>
+ </approach_selection>
+ <analytical_approach>
+ <General>
+ <OswaldFactor Desc="Oswald factor in clean configuration" Unit="-">
+ <value>0.85</value>
+ <default>0.85</default>
+ </OswaldFactor>
+ <AspectRatio Desc="aspect ratio" Unit="count">
+ <value>9.5</value>
+ <default>9.5</default>
+ </AspectRatio>
+ <n_pilots Desc="Number of Pilots" Unit="count">
+ <value>2</value>
+ <default>2</default>
+ </n_pilots>
+ <n_engines Desc="Number of engines" Unit="count">
+ <value>2</value>
+ <default>2</default>
+ </n_engines>
+ <Cf Desc="friction coefficient" Unit="count">
+ <value>0.002</value>
+ <default>0.002</default>
+ </Cf>
+ </General>
+ <Constants>
+ <SFC_kerosene Desc="Specific Fuel Consumption Factor for Kerosene">
+ <value>0.0001389</value>
+ <default>0.0001389</default>
+ </SFC_kerosene>
+ </Constants>
+ <TOFL Desc="takeoff distance requirement">
+ <CLmax_TO Desc="Maximum lift coefficient at takeoff" Unit="-">
+ <value>2.28</value>
+ <default>2.28</default>
+ </CLmax_TO>
+ </TOFL>
+ <LDN Desc="landing distance requirement">
+ <CLmax_L Desc="Maximum lift coefficient at landing" Unit="-">
+ <value>2.85</value>
+ <default>2.85</default>
+ </CLmax_L>
+ <mlmo Desc="ratio between maximum landing mass and takeoff mass" Unit="-">
+ <value>0.82</value>
+ <default>0.82</default>
+ </mlmo>
+ </LDN>
+ <Climb Desc="climb performance requirement">
+ <deltaCD_HL Desc="Delta CD0 with TO-Flaps" Unit="-">
+ <value>0.07</value>
+ <default>0.07</default>
+ </deltaCD_HL>
+ </Climb>
+ <Cruise Desc="maximum cruise speed requirement">
+ <mcr_mto Desc="ratio between cruise mass and takeoff mass - default for mid- and short-range: 0.956, default for long range: 0.924">
+ <value>0.956</value>
+ <default>0.956</default>
+ </mcr_mto>
+ <optimalCL Desc="maximum CL at initial cruise">
+ <value>0.57</value>
+ <default>0.57</default>
+ </optimalCL>
+ </Cruise>
+ <LiftToDragRatios Desc="initial cruise and loiter lift to drag ratios ">
+ <LD_initial_cruise Desc="cruise requirements">
+ <value>15</value>
+ <default>15</default>
+ </LD_initial_cruise>
+ <LD_initial_loiter Desc="loiter requirements">
+ <value>16</value>
+ <default>16</default>
+ </LD_initial_loiter>
+ </LiftToDragRatios>
+ <Masses Desc="mass estimation methodology">
+ <Fractions Desc="mass fractions">
+ <mf_warmup Desc="Warmup (according to Raymer: 0.97(A340)-0.99(A320))" Unit="-" Default="0.99">
+ <value>0.99</value>
+ <default>0.99</default>
+ </mf_warmup>
+ <mf_taxi Desc="Warmup (according to Raymer: 0.97(A340)-0.99(A320))" Unit="-" Default="0.99">
+ <value>0.99</value>
+ <default>0.99</default>
+ </mf_taxi>
+ <mf_to Desc="Taxi and Takeoff (according to Raymer: 0.97(A340)-0.99(A320))" Unit="-" Default="0.995">
+ <value>0.995</value>
+ <default>0.995</default>
+ </mf_to>
+ <mf_climb Desc="Climb (according to Raymer: 0.97(A340)-0.99(A320))" Unit="-" Default="0.98">
+ <value>0.98</value>
+ <default>0.98</default>
+ </mf_climb>
+ <mf_descent Desc="Descent (according to Raymer: 0.99(A340)-0.995(A320))" Unit="-" Default="0.99">
+ <value>0.99</value>
+ <default>0.99</default>
+ </mf_descent>
+ <mf_missedandclimb Desc="Landing and Taxi Back (according to Raymer: 0.992(A340)-0.997(A320))" Unit="-" Default="0.988">
+ <value>0.988</value>
+ <default>0.988</default>
+ </mf_missedandclimb>
+ <mf_land Desc="Landing and Taxi Back (according to Raymer: 0.992(A340)-0.997(A320))" Unit="-" Default="0.995">
+ <value>0.995</value>
+ <default>0.995</default>
+ </mf_land>
+ </Fractions>
+ </Masses>
+ </analytical_approach>
+ </tube_and_wing>
+ </program_settings>
+</module_configuration_file>
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/xml_configs/missionAnalysis_conf.xml b/UnicadoGUI/Backend/xml_configs/missionAnalysis_conf.xml
new file mode 100644
index 0000000..9d6114b
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/missionAnalysis_conf.xml
@@ -0,0 +1,286 @@
+<?xml version="1.0" encoding="utf-8"?>
+<module_configuration_file name="missionAnalysis_conf.xml">
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>template.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>../projects/CSR/CSR-02/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>3</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>true</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>true</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>mission_analysis_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>mission_analysis.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>../inkscape/</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>../gnuplot/</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings description="Program settings">
+ <program_specific description="Program specific control settings">
+ <specific_air_range_plot description="Switch to generate plots for the specific air range ('true': On, 'false': Off)">
+ <value>true</value>
+ </specific_air_range_plot>
+ <exit_if_fuel_limit_reached description="Switch to abort program if estimated fuel reaches maximum fuel mass ('true': On, 'false': Off)">
+ <enable description="'true': On, 'false': Off">
+ <value>false</value>
+ </enable>
+ <allowed_relative_overshoot description="Relative overshoot that shall be allowed">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </allowed_relative_overshoot>
+ </exit_if_fuel_limit_reached>
+ <exit_if_maximum_takeoff_mass_limit_reached description="Switch to abort program in study mode if takeoff mass (TOM) is greater than/equal to maximum takoff mass (MTOM) ('true': On, 'false': Off)">
+ <enable description="'true': On, 'false': Off">
+ <value>false</value>
+ </enable>
+ <allowed_relative_overshoot description="Relative overshoot that shall be allowed">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </allowed_relative_overshoot>
+ </exit_if_maximum_takeoff_mass_limit_reached>
+ </program_specific>
+ <general description="General parameters">
+ <fuel_planning description="Fuel planning according to the Joint Aviation Requirements (JAR) or the Federal Aviation Regulations (FAR)">
+ <fuel_estimation description="Setup of the fuel estimation">
+ <fuel_estimation_switch description="Switch if the fuel estimation method within the aircraft XML shall be used (to be found in the mission requirements' fuel_estimation_selector)">
+ <value>false</value>
+ </fuel_estimation_switch>
+ <joint_aviation_requirements_parameters description="Parameter for fuel planning according to the Joint Aviation Requirements (JAR)">
+ <contingency_fuel description="Relative share of contingency fuel in total trip fuel. Std: 0.05., if en-route allowance: 0.03 (check 'Getting to Grips With Aircraft Performance' p.173)">
+ <value>0.03</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </contingency_fuel>
+ <use_additional_fuel description="Switch if additional fuel shall be added e.g. for flag or supplemental operations ('true': On, 'false': Off)">
+ <value>false</value>
+ </use_additional_fuel>
+ <extra_fuel description="Extra fuel that shall be carried at the discretion of the captain">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </extra_fuel>
+ </joint_aviation_requirements_parameters>
+ <federal_aviation_regulations_parameter description="Parameter for fuel planning according to the Federal Aviation Regulations (FAR)">
+ <use_additional_fuel description="Switch if additional fuel shall be added e.g. for flag or supplemental operations ('true': On, 'false': Off)">
+ <value>false</value>
+ </use_additional_fuel>
+ </federal_aviation_regulations_parameter>
+ </fuel_estimation>
+ <fuel_flow_factor_taxiing description="Factor to adapt the (idle) fuel flow during taxiing">
+ <value>1.</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </fuel_flow_factor_taxiing>
+ <holding description="Behavior during holding">
+ <holding_mach_number description="Mach number flown during holding">
+ <value>0.4</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </holding_mach_number>
+ <holding_altitude description="Altitude during holding (30.48 m = 100 ft = 1 FL)">
+ <value>1500</value>
+ <unit>ft</unit>
+ <lower_boundary>500</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </holding_altitude>
+ <use_economical_speed description="Switch if the economic Mach number shall overwrite the holding Mach number within the value node ('true': On, 'false': Off)">
+ <value>true</value>
+ </use_economical_speed>
+ </holding>
+ </fuel_planning>
+ <landing_gear description="Design specifications for the landing gear">
+ <friction_coefficient description="Friction coefficient of tyres and pavement: Raymer p.486 - Table 17.1: 0.03 - 0.05">
+ <value>0.03</value>
+ <unit>1</unit>
+ <lower_boundary>0.02</lower_boundary>
+ <upper_boundary>0.08</upper_boundary>
+ </friction_coefficient>
+ <braking_coefficient description="Brake coefficient: Raymer p.486 - Table 17.1: 0.3 - 0.5; Torenbeek: jet 0.4-0.5; prop 0.35-0.45; Airbus: Medium Deceleration = 11 ft/s^2 = 0.34189">
+ <value>0.34189</value>
+ <unit>1</unit>
+ <lower_boundary>0.06</lower_boundary>
+ <upper_boundary>0.5</upper_boundary>
+ </braking_coefficient>
+ </landing_gear>
+ <increase_engine_rating_during_climb description="Switch to set engine rating to maximum continuous during climb if climb rating is not sufficient ('true': On, 'false': Off)">
+ <value>false</value>
+ </increase_engine_rating_during_climb>
+ <polar_switch_mission_point description="Definition where and how a polar switch shall take place">
+ <polar_switch_selector description="Selector to define the mission point where alternative polars takes place ('mode_0': Off, 'mode_1': Absolute range, 'mode_2': Relative range, 'mode_3'': Absolute remaining flight time, 'mode_4': Relative remaining flight time)">
+ <value>mode_0</value>
+ </polar_switch_selector>
+ <absolute_range_flown description="Absolute flown range">
+ <value>500</value>
+ <unit>nm</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </absolute_range_flown>
+ <relative_range_flown description="Range flown relative to total range">
+ <value>0.85</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </relative_range_flown>
+ <absolute_time_passed description="Absolute passed flight time">
+ <value>250</value>
+ <unit>min</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </absolute_time_passed>
+ <relative_time_passed description="Passed flight time relative to the total flight time">
+ <value>0.85</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </relative_time_passed>
+ </polar_switch_mission_point>
+ <glideslope_interception_distance description="Buffer distance to hit the glideslope exactly">
+ <value>1000.</value>
+ <unit>m</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </glideslope_interception_distance>
+ <use_breguet_estimation_in_cruise description="Switch to activate fuel estimation using Breguet equation ('true': On, 'false': Off -> fuel mass is calculated from fuel flow of current engine setting">
+ <value>false</value>
+ </use_breguet_estimation_in_cruise>
+ <iterate_top_of_descent_mass description="Switch for iteration of mass at top of descent ('true': On, 'false': Off)">
+ <value>true</value>
+ </iterate_top_of_descent_mass>
+ <landing description="Settings for landing calculation">
+ <rotation_time description="Time to rotate at touch down from main gear to nose gear">
+ <value>3</value>
+ <unit>s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </rotation_time>
+ <thrust_reverser description="Settings for thrust reverser">
+ <enable description="Switch to use thrust reverser for deceleration ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <deactivation_speed description="Calibrated airspeed when the thrust reverser is set from Maximum to Idle">
+ <value>80</value>
+ <unit>KCAS</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>650</upper_boundary>
+ </deactivation_speed>
+ <efficiency description="Efficiency of the reverse thrust">
+ <value>0.5</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </efficiency>
+ </thrust_reverser>
+ <runway_exit_speed description="Speed to slow down until runway can be exited (normal exit A320: max 15 kts = 7.72 m/s; high speed exit A320: max 25 kts = 12.86 m/s)">
+ <value>15</value>
+ <unit>kts</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>650</upper_boundary>
+ </runway_exit_speed>
+ </landing>
+ </general>
+ <mode description="Program mode">
+ <mission_methods>
+ <design_mission_switch description="Switch to set a study or design mission ('true': design mission, 'false': study mission)">
+ <value>true</value>
+ </design_mission_switch>
+ <center_of_gravity_method description="Selector to shift the center of gravity ('mode_0': Off, 'mode_1': half-sophisticated with howe for lifting surface tank, 'mode_2': sophisticated method for center of gravity (only payload and fuel) calculation)">
+ <value>mode_0</value>
+ </center_of_gravity_method>
+ </mission_methods>
+ <rate_of_climb_switch description="Switch THAT ONLY AFFECTS THE REQUIREMENTS MISSION: Calculate an optimum for the rate of climb ('true': calculate optimum, 'false': skip)">
+ <value>false</value>
+ </rate_of_climb_switch>
+ <requirement_check description="Settings for the requirement check">
+ <enable description="Switch to check the requirements 'time to climb' and 'flight levels' ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <force_requirement_check description="Switch to force this check ('true': On, 'false': Off)">
+ <value>true</value>
+ </force_requirement_check>
+ <auto_climb_ratings_for_time_to_climb description="Switch to use automated climb ratings for the time to climb (TTC) ('true': On, 'false': Off)">
+ <value>true</value>
+ </auto_climb_ratings_for_time_to_climb>
+ </requirement_check>
+ <calculate_emissions_parameters description="Switch if input for detailed emission calculation shall be generated ('true': On, 'false': Off)">
+ <value>true</value>
+ </calculate_emissions_parameters>
+ <calculate_noise_parameters description="Switch if input for noise calculation shall be generated ('true': On, 'false': Off)">
+ <value>true</value>
+ </calculate_noise_parameters>
+ </mode>
+ <precision description="Specify the calculation accuracy">
+ <acceleration_increment description="Step size regarding acceleration or deceleration">
+ <value>0.5</value>
+ <unit>m/s</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>340</upper_boundary>
+ </acceleration_increment>
+ <mach_acceleration_increment description="Step size regarding acceleration or deceleration as a Mach number">
+ <value>0.005</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </mach_acceleration_increment>
+ <altitude_increment description="Step distance for climb or descent">
+ <value>5.</value>
+ <unit>m</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </altitude_increment>
+ <way_increment description="Step distance in x-direction">
+ <value>1000.</value>
+ <unit>m</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </way_increment>
+ <specific_air_range_check_increment description="Relative step distance in x-direction for automatic Flight level change check">
+ <value>0.01</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </specific_air_range_check_increment>
+ </precision>
+ </program_settings>
+</module_configuration_file>
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/xml_configs/missionAnalysis_conf_default.xml b/UnicadoGUI/Backend/xml_configs/missionAnalysis_conf_default.xml
new file mode 100644
index 0000000..5955d49
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/missionAnalysis_conf_default.xml
@@ -0,0 +1,286 @@
+<?xml version="1.0" encoding="utf-8" ?>
+<module_configuration_file name="missionAnalysis_conf.xml">
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>template.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>../projects/CSR/CSR-02/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>3</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>true</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>true</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>mission_analysis_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>mission_analysis.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>../inkscape/</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>../gnuplot/</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings description="Program settings">
+ <program_specific description="Program specific control settings">
+ <specific_air_range_plot description="Switch to generate plots for the specific air range ('true': On, 'false': Off)">
+ <value>true</value>
+ </specific_air_range_plot>
+ <exit_if_fuel_limit_reached description="Switch to abort program if estimated fuel reaches maximum fuel mass ('true': On, 'false': Off)">
+ <enable description="'true': On, 'false': Off">
+ <value>false</value>
+ </enable>
+ <allowed_relative_overshoot description="Relative overshoot that shall be allowed">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </allowed_relative_overshoot>
+ </exit_if_fuel_limit_reached>
+ <exit_if_maximum_takeoff_mass_limit_reached description="Switch to abort program in study mode if takeoff mass (TOM) is greater than/equal to maximum takoff mass (MTOM) ('true': On, 'false': Off)">
+ <enable description="'true': On, 'false': Off">
+ <value>false</value>
+ </enable>
+ <allowed_relative_overshoot description="Relative overshoot that shall be allowed">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </allowed_relative_overshoot>
+ </exit_if_maximum_takeoff_mass_limit_reached>
+ </program_specific>
+ <general description="General parameters">
+ <fuel_planning description="Fuel planning according to the Joint Aviation Requirements (JAR) or the Federal Aviation Regulations (FAR)">
+ <fuel_estimation description="Setup of the fuel estimation">
+ <fuel_estimation_switch description="Switch if the fuel estimation method within the aircraft XML shall be used (to be found in the mission requirements' fuel_estimation_selector)">
+ <value>false</value>
+ </fuel_estimation_switch>
+ <joint_aviation_requirements_parameters description="Parameter for fuel planning according to the Joint Aviation Requirements (JAR)">
+ <contingency_fuel description="Relative share of contingency fuel in total trip fuel. Std: 0.05., if en-route allowance: 0.03 (check 'Getting to Grips With Aircraft Performance' p.173)">
+ <value>0.03</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </contingency_fuel>
+ <use_additional_fuel description="Switch if additional fuel shall be added e.g. for flag or supplemental operations ('true': On, 'false': Off)">
+ <value>false</value>
+ </use_additional_fuel>
+ <extra_fuel description="Extra fuel that shall be carried at the discretion of the captain">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </extra_fuel>
+ </joint_aviation_requirements_parameters>
+ <federal_aviation_regulations_parameter description="Parameter for fuel planning according to the Federal Aviation Regulations (FAR)">
+ <use_additional_fuel description="Switch if additional fuel shall be added e.g. for flag or supplemental operations ('true': On, 'false': Off)">
+ <value>false</value>
+ </use_additional_fuel>
+ </federal_aviation_regulations_parameter>
+ </fuel_estimation>
+ <fuel_flow_factor_taxiing description="Factor to adapt the (idle) fuel flow during taxiing">
+ <value>1.</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </fuel_flow_factor_taxiing>
+ <holding description="Behavior during holding">
+ <holding_mach_number description="Mach number flown during holding">
+ <value>0.4</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </holding_mach_number>
+ <holding_altitude description="Altitude during holding (30.48 m = 100 ft = 1 FL)">
+ <value>1500</value>
+ <unit>ft</unit>
+ <lower_boundary>500</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </holding_altitude>
+ <use_economical_speed description="Switch if the economic Mach number shall overwrite the holding Mach number within the value node ('true': On, 'false': Off)">
+ <value>true</value>
+ </use_economical_speed>
+ </holding>
+ </fuel_planning>
+ <landing_gear description="Design specifications for the landing gear">
+ <friction_coefficient description="Friction coefficient of tyres and pavement: Raymer p.486 - Table 17.1: 0.03 - 0.05">
+ <value>0.03</value>
+ <unit>1</unit>
+ <lower_boundary>0.02</lower_boundary>
+ <upper_boundary>0.08</upper_boundary>
+ </friction_coefficient>
+ <braking_coefficient description="Brake coefficient: Raymer p.486 - Table 17.1: 0.3 - 0.5; Torenbeek: jet 0.4-0.5; prop 0.35-0.45; Airbus: Medium Deceleration = 11 ft/s^2 = 0.34189">
+ <value>0.34189</value>
+ <unit>1</unit>
+ <lower_boundary>0.06</lower_boundary>
+ <upper_boundary>0.5</upper_boundary>
+ </braking_coefficient>
+ </landing_gear>
+ <increase_engine_rating_during_climb description="Switch to set engine rating to maximum continuous during climb if climb rating is not sufficient ('true': On, 'false': Off)">
+ <value>false</value>
+ </increase_engine_rating_during_climb>
+ <polar_switch_mission_point description="Definition where and how a polar switch shall take place">
+ <polar_switch_selector description="Selector to define the mission point where alternative polars takes place ('mode_0': Off, 'mode_1': Absolute range, 'mode_2': Relative range, 'mode_3'': Absolute remaining flight time, 'mode_4': Relative remaining flight time)">
+ <value>mode_0</value>
+ </polar_switch_selector>
+ <absolute_range_flown description="Absolute flown range">
+ <value>500</value>
+ <unit>nm</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </absolute_range_flown>
+ <relative_range_flown description="Range flown relative to total range">
+ <value>0.85</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </relative_range_flown>
+ <absolute_time_passed description="Absolute passed flight time">
+ <value>250</value>
+ <unit>min</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </absolute_time_passed>
+ <relative_time_passed description="Passed flight time relative to the total flight time">
+ <value>0.85</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </relative_time_passed>
+ </polar_switch_mission_point>
+ <glideslope_interception_distance description="Buffer distance to hit the glideslope exactly">
+ <value>1000.</value>
+ <unit>m</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </glideslope_interception_distance>
+ <use_breguet_estimation_in_cruise description="Switch to activate fuel estimation using Breguet equation ('true': On, 'false': Off -> fuel mass is calculated from fuel flow of current engine setting">
+ <value>false</value>
+ </use_breguet_estimation_in_cruise>
+ <iterate_top_of_descent_mass description="Switch for iteration of mass at top of descent ('true': On, 'false': Off)">
+ <value>true</value>
+ </iterate_top_of_descent_mass>
+ <landing description="Settings for landing calculation">
+ <rotation_time description="Time to rotate at touch down from main gear to nose gear">
+ <value>3</value>
+ <unit>s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </rotation_time>
+ <thrust_reverser description="Settings for thrust reverser">
+ <enable description="Switch to use thrust reverser for deceleration ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <deactivation_speed description="Calibrated airspeed when the thrust reverser is set from Maximum to Idle">
+ <value>80</value>
+ <unit>KCAS</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>650</upper_boundary>
+ </deactivation_speed>
+ <efficiency description="Efficiency of the reverse thrust">
+ <value>0.5</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </efficiency>
+ </thrust_reverser>
+ <runway_exit_speed description="Speed to slow down until runway can be exited (normal exit A320: max 15 kts = 7.72 m/s; high speed exit A320: max 25 kts = 12.86 m/s)">
+ <value>15</value>
+ <unit>kts</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>650</upper_boundary>
+ </runway_exit_speed>
+ </landing>
+ </general>
+ <mode description="Program mode">
+ <mission_methods>
+ <design_mission_switch description="Switch to set a study or design mission ('true': design mission, 'false': study mission)">
+ <value>true</value>
+ </design_mission_switch>
+ <center_of_gravity_method description="Selector to shift the center of gravity ('mode_0': Off, 'mode_1': half-sophisticated with howe for lifting surface tank, 'mode_2': sophisticated method for center of gravity (only payload and fuel) calculation)">
+ <value>mode_0</value>
+ </center_of_gravity_method>
+ </mission_methods>
+ <rate_of_climb_switch description="Switch THAT ONLY AFFECTS THE REQUIREMENTS MISSION: Calculate an optimum for the rate of climb ('true': calculate optimum, 'false': skip)">
+ <value>false</value>
+ </rate_of_climb_switch>
+ <requirement_check description="Settings for the requirement check">
+ <enable description="Switch to check the requirements 'time to climb' and 'flight levels' ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <force_requirement_check description="Switch to force this check ('true': On, 'false': Off)">
+ <value>true</value>
+ </force_requirement_check>
+ <auto_climb_ratings_for_time_to_climb description="Switch to use automated climb ratings for the time to climb (TTC) ('true': On, 'false': Off)">
+ <value>true</value>
+ </auto_climb_ratings_for_time_to_climb>
+ </requirement_check>
+ <calculate_emissions_parameters description="Switch if input for detailed emission calculation shall be generated ('true': On, 'false': Off)">
+ <value>true</value>
+ </calculate_emissions_parameters>
+ <calculate_noise_parameters description="Switch if input for noise calculation shall be generated ('true': On, 'false': Off)">
+ <value>true</value>
+ </calculate_noise_parameters>
+ </mode>
+ <precision description="Specify the calculation accuracy">
+ <acceleration_increment description="Step size regarding acceleration or deceleration">
+ <value>0.5</value>
+ <unit>m/s</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>340</upper_boundary>
+ </acceleration_increment>
+ <mach_acceleration_increment description="Step size regarding acceleration or deceleration as a Mach number">
+ <value>0.005</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </mach_acceleration_increment>
+ <altitude_increment description="Step distance for climb or descent">
+ <value>5.</value>
+ <unit>m</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </altitude_increment>
+ <way_increment description="Step distance in x-direction">
+ <value>1000.</value>
+ <unit>m</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </way_increment>
+ <specific_air_range_check_increment description="Relative step distance in x-direction for automatic Flight level change check">
+ <value>0.01</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </specific_air_range_check_increment>
+ </precision>
+ </program_settings>
+</module_configuration_file>
diff --git a/UnicadoGUI/Backend/xml_configs/propulsionDesign_conf.xml b/UnicadoGUI/Backend/xml_configs/propulsionDesign_conf.xml
new file mode 100644
index 0000000..0be5c3a
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/propulsionDesign_conf.xml
@@ -0,0 +1,129 @@
+<?xml version="1.0" encoding="utf-8" ?>
+<module_configuration_file name="propulsionDesign_conf.xml">
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>CSR02-converted.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>/home/obi/TUM_Work/60_UNICADO/Playground/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>3</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_3</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_0</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>true</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>false</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>propulsion_design_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>propulsion_design.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings description="Settings specific to engineSizing.">
+ <method description="Choose the implementation method of each design domain.">
+ <engine_designer description="Choose the engine designer: Empirical, Rubber, GasTurb">
+ <value>Rubber</value>
+ </engine_designer>
+ <nacelle_designer description="Choose the nacelle designer: Default">
+ <value>Default</value>
+ </nacelle_designer>
+ <pylon_designer description="Choose the pylon designer: Default">
+ <value>Default</value>
+ </pylon_designer>
+ <propulsion_integrator description="Choose the propulsion integrator: Default">
+ <value>Default</value>
+ </propulsion_integrator>
+ <mass_analyzer description="Choose the mass analyzer: Default">
+ <value>Default</value>
+ </mass_analyzer>
+ </method>
+ <path_engine_database description="The path to the database with existing engine decks.">
+ <value>/home/obi/TUM_Work/60_UNICADO/Repositories/rUNICADO/engines/</value>
+ </path_engine_database>
+ <technology_factors description="Improve or decrease the performance of every engine by this factor.">
+ <engine_mass>
+ <value>1.0</value>
+ <unit>1</unit>
+ <upper_boundary>+Inf</upper_boundary>
+ <lower_boundary>0.0</lower_boundary>
+ </engine_mass>
+ <nacelle_mass>
+ <value>1.0</value>
+ <unit>1</unit>
+ <upper_boundary>+Inf</upper_boundary>
+ <lower_boundary>0.0</lower_boundary>
+ </nacelle_mass>
+ <pylon_mass>
+ <value>1.0</value>
+ <unit>1</unit>
+ <upper_boundary>+Inf</upper_boundary>
+ <lower_boundary>0.0</lower_boundary>
+ </pylon_mass>
+ <engine_efficiency>
+ <value>1.0</value>
+ <unit>1</unit>
+ <upper_boundary>+Inf</upper_boundary>
+ <lower_boundary>0.0</lower_boundary>
+ </engine_efficiency>
+ </technology_factors>
+ <propulsion ID="Default" description="Define defaults for the clean sheet design. You can add other engines with different ID to override these setting for the propulsion with this ID.">
+ <engine description="Detailed information of engine design">
+ <Empirical description="Settings for empirical engine designer">
+ <BPR>
+ <value></value>
+ </BPR>
+ </Empirical>
+ <Rubber description="Settings for rubber engine designer">
+ <engine_model><value>V2527-A5</value></engine_model>
+ </Rubber>
+ <GasTurb description="Settings for gasTurb interface engine designer">
+ </GasTurb>
+ </engine>
+ <nacelle description="Detailed information of nacelle geometry">
+ <profile description="Section shape of the nacelle.">
+ <value>nacelle.dat</value>
+ </profile>
+ <duct_type description="Short or long ducted nacelle">
+ <value>short</value>
+ </duct_type>
+ </nacelle>
+ <pylon description="Detailed information of pylon geometry">
+ <profile description="Section shape of the pylon.">
+ <value>pylon.dat</value>
+ </profile>
+ </pylon>
+ <integration description="Detailed information of propulsion integraton">
+ </integration>
+ </propulsion>
+ </program_settings>
+</module_configuration_file>
diff --git a/UnicadoGUI/Backend/xml_configs/propulsionDesign_conf_default.xml b/UnicadoGUI/Backend/xml_configs/propulsionDesign_conf_default.xml
new file mode 100644
index 0000000..0be5c3a
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/propulsionDesign_conf_default.xml
@@ -0,0 +1,129 @@
+<?xml version="1.0" encoding="utf-8" ?>
+<module_configuration_file name="propulsionDesign_conf.xml">
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>CSR02-converted.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>/home/obi/TUM_Work/60_UNICADO/Playground/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>3</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_3</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_0</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>true</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>false</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>propulsion_design_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>propulsion_design.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings description="Settings specific to engineSizing.">
+ <method description="Choose the implementation method of each design domain.">
+ <engine_designer description="Choose the engine designer: Empirical, Rubber, GasTurb">
+ <value>Rubber</value>
+ </engine_designer>
+ <nacelle_designer description="Choose the nacelle designer: Default">
+ <value>Default</value>
+ </nacelle_designer>
+ <pylon_designer description="Choose the pylon designer: Default">
+ <value>Default</value>
+ </pylon_designer>
+ <propulsion_integrator description="Choose the propulsion integrator: Default">
+ <value>Default</value>
+ </propulsion_integrator>
+ <mass_analyzer description="Choose the mass analyzer: Default">
+ <value>Default</value>
+ </mass_analyzer>
+ </method>
+ <path_engine_database description="The path to the database with existing engine decks.">
+ <value>/home/obi/TUM_Work/60_UNICADO/Repositories/rUNICADO/engines/</value>
+ </path_engine_database>
+ <technology_factors description="Improve or decrease the performance of every engine by this factor.">
+ <engine_mass>
+ <value>1.0</value>
+ <unit>1</unit>
+ <upper_boundary>+Inf</upper_boundary>
+ <lower_boundary>0.0</lower_boundary>
+ </engine_mass>
+ <nacelle_mass>
+ <value>1.0</value>
+ <unit>1</unit>
+ <upper_boundary>+Inf</upper_boundary>
+ <lower_boundary>0.0</lower_boundary>
+ </nacelle_mass>
+ <pylon_mass>
+ <value>1.0</value>
+ <unit>1</unit>
+ <upper_boundary>+Inf</upper_boundary>
+ <lower_boundary>0.0</lower_boundary>
+ </pylon_mass>
+ <engine_efficiency>
+ <value>1.0</value>
+ <unit>1</unit>
+ <upper_boundary>+Inf</upper_boundary>
+ <lower_boundary>0.0</lower_boundary>
+ </engine_efficiency>
+ </technology_factors>
+ <propulsion ID="Default" description="Define defaults for the clean sheet design. You can add other engines with different ID to override these setting for the propulsion with this ID.">
+ <engine description="Detailed information of engine design">
+ <Empirical description="Settings for empirical engine designer">
+ <BPR>
+ <value></value>
+ </BPR>
+ </Empirical>
+ <Rubber description="Settings for rubber engine designer">
+ <engine_model><value>V2527-A5</value></engine_model>
+ </Rubber>
+ <GasTurb description="Settings for gasTurb interface engine designer">
+ </GasTurb>
+ </engine>
+ <nacelle description="Detailed information of nacelle geometry">
+ <profile description="Section shape of the nacelle.">
+ <value>nacelle.dat</value>
+ </profile>
+ <duct_type description="Short or long ducted nacelle">
+ <value>short</value>
+ </duct_type>
+ </nacelle>
+ <pylon description="Detailed information of pylon geometry">
+ <profile description="Section shape of the pylon.">
+ <value>pylon.dat</value>
+ </profile>
+ </pylon>
+ <integration description="Detailed information of propulsion integraton">
+ </integration>
+ </propulsion>
+ </program_settings>
+</module_configuration_file>
diff --git a/UnicadoGUI/Backend/xml_configs/systemsDesign_conf.xml b/UnicadoGUI/Backend/xml_configs/systemsDesign_conf.xml
new file mode 100644
index 0000000..8664a81
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/systemsDesign_conf.xml
@@ -0,0 +1,2437 @@
+<?xml version="1.0" encoding="utf-8"?>
+<module_configuration_file name="systemsDesign_conf.xml">
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>writing_test.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>X:/UNICADO/AircraftReferences/CSR/CSR-02/cleanSheetDesign/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>1</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_3</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_3</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>true</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>false</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>TOOLNAME_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>TOOLNAME.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>C:/Programs/UNICADOworkflow/inkscape/</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>C:/Programs/UNICADOworkflow/gnuplot/</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings>
+ <modes description="mode selection, only STANDARD available currently">
+ <value>STANDARD</value>
+ <default>STANDARD</default>
+ </modes>
+ <design_case description="Switch for system sizing. 1: Sizing, 0: ONLY determination of a load profile for a specific mission">
+ <value>1</value>
+ <default>1</default>
+ </design_case>
+ <offtakes_for_requirement_mission description="Determination of Offtakes for Requirement Mission">
+ <value>0</value>
+ <default>0</default>
+ </offtakes_for_requirement_mission>
+ <scaling_factors description="Variable scaling factors to change the calculated masses">
+ <systems description="Systems: 1 = full calculated weight">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>1</default>
+ </systems>
+ <furnishings description="Furnishings: 1 = on; 0 = off">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>1</default>
+ </furnishings>
+ <operator_items description="OperatorItems: 1 = full calculated weight">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>1</default>
+ </operator_items>
+ </scaling_factors>
+ <tex_report_without_masses description="1: TeX report only with approvals, since mass breakdown comes from massEstimation">
+ <value>1</value>
+ <default>1</default>
+ </tex_report_without_masses>
+ <control_device_warning description="Warning is issued if no suitable method is available for ControlDevice.">
+ <value>1</value>
+ <default>1</default>
+ </control_device_warning>
+ <aircraft_systems>
+ <energy_sinks>
+ <number_of_sinks description="Number of energy sinks">
+ <value>9</value>
+ <default>20</default>
+ </number_of_sinks>
+ <system ID="0">
+ <system_description description="Type of furnishing system">
+ <value>conventionalFurnishing</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="1">
+ <system_description description="Type of fuel system">
+ <value>conventionalFuel</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="2">
+ <system_description description="Type of system ice and rain protection system (conventional or electrical">
+ <value>conventionalIceRainProtection</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="3">
+ <system_description description="Type of lighting system">
+ <value>conventionalLighting</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="4">
+ <system_description description="Type of fire protection system">
+ <value>conventionalFireProtection</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="5">
+ <system_description description="Type of oxygen system">
+ <value>conventionalOxygenSystem</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="6">
+ <system_description description="Type of gear system">
+ <value>conventionalGear</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="7">
+ <system_description description="Type of flight control system">
+ <value>conventionalFlightControl</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="8">
+ <system_description description="remaining consumer system">
+ <value>remainingConsumers</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ </energy_sinks>
+ <environmental_control_system>
+ <system_description Unit="-" description="Type of environmental control system (ECS)">
+ <value>conventionalECS</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </environmental_control_system>
+ <energy_sources>
+ <number_of_sources description="Number of energy sources">
+ <value>2</value>
+ <default>1</default>
+ </number_of_sources>
+ <system ID="0">
+ <system_description description="Type of propulsion system">
+ <value>conventionalPropulsion</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ <uses_fuel description="Switch whether the energy source uses fuel. 1:yes, 0:no fuel">
+ <value>1</value>
+ <default>1</default>
+ </uses_fuel>
+ </system>
+ <system ID="1">
+ <system_description description="Type of auxiliary power unit (APU) system (conventionalAPU or fuelCellAPU)">
+ <value>conventionalAPU</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ <uses_fuel description="Switch whether the energy source uses fuel. 1:yes, 0:no fuel">
+ <value>1</value>
+ <default>1</default>
+ </uses_fuel>
+ </system>
+ <system ID="2">
+ <system_description description="Fuel cell">
+ <value>fuelCell</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ <uses_fuel description="Switch whether the energy source uses fuel. 1:yes, 0:no fuel">
+ <value>1</value>
+ <default>1</default>
+ </uses_fuel>
+ </system>
+ </energy_sources>
+ <energy_conductors>
+ <number_of_conductors description="Number of energy conductor systems">
+ <value>3</value>
+ <default>3</default>
+ </number_of_conductors>
+ <system ID="0">
+ <system_description description="Type of system">
+ <value>BleedAirSystem</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="1">
+ <system_description description="Type of system">
+ <value>HydraulicSystem</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="2">
+ <system_description description="Type of system">
+ <value>ElectricSystem</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ </energy_conductors>
+ <virtual_systems>
+ <number_of_virtual_systems description="Number of energy systems">
+ <value>0</value>
+ <default></default>
+ </number_of_virtual_systems>
+ <system ID="0">
+ <system_description description="Type of virtual system">
+ <value>virtualSystem</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ <mass description="mass of the system">
+ <value>5000.0</value>
+ <unit>kg</unit>
+ <default>0.0</default>
+ </mass>
+ <center_of_gravity description="position of mass item to global point of reference">
+ <x description="Position of reference in x-direction">
+ <value>0</value>
+ <unit>m</unit>
+ </x>
+ <y description="Position of reference in y-direction">
+ <value>0</value>
+ <unit>m</unit>
+ </y>
+ <z description="Position of reference in z-direction">
+ <value>0</value>
+ <unit>m</unit>
+ </z>
+ </center_of_gravity>
+ <power_demand>
+ <departure>
+ <bleed_air description="Bleed air requirement during departure">
+ <value>3.0</value>
+ <unit>kg/s</unit>
+ <default>0.0</default>
+ </bleed_air>
+ <hydraulic description="Hydraulic requirements during departure">
+ <value>10000.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </hydraulic>
+ <electric description="Electrical requirements during departure">
+ <value>15000.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </electric>
+ <heat_load description="Heat emission during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </heat_load>
+ </departure>
+ <cruise>
+ <bleed_air description="Bleed air requirement during departure">
+ <value>0.5</value>
+ <unit>kg/s</unit>
+ <default>0.0</default>
+ </bleed_air>
+ <hydraulic description="Hydraulic requirements during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </hydraulic>
+ <electric description="Electrical requirements during departure">
+ <value>20000.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </electric>
+ <heat_load description="Heat emission during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </heat_load>
+ </cruise>
+ <approach>
+ <bleed_air description="Bleed air requirement during departure">
+ <value>3.5</value>
+ <unit>kg/s</unit>
+ <default>0.0</default>
+ </bleed_air>
+ <hydraulic description="Hydraulic requirements during departure">
+ <value>7500.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </hydraulic>
+ <electric description="Electrical requirements during departure">
+ <value>18000.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </electric>
+ <heat_load description="Heat emission during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </heat_load>
+ </approach>
+ </power_demand>
+ </system>
+ <system ID="0">
+ <system_description description="Type of system">
+ <value>virtualSystem</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ <mass description="mass of the system">
+ <value>1000.0</value>
+ <unit>kg</unit>
+ <default>0.0</default>
+ </mass>
+ <center_of_gravity description="position of mass item to global point of reference">
+ <x description="Position of reference in x-direction">
+ <value>0</value>
+ <unit>m</unit>
+ </x>
+ <y description="Position of reference in y-direction">
+ <value>0</value>
+ <unit>m</unit>
+ </y>
+ <z description="Position of reference in z-direction">
+ <value>0</value>
+ <unit>m</unit>
+ </z>
+ </center_of_gravity>
+ <power_demand>
+ <departure>
+ <bleed_air description="Bleed air requirement during departure">
+ <value>0.0</value>
+ <unit>kg/s</unit>
+ <default>0.0</default>
+ </bleed_air>
+ <hydraulic description="Hydraulic requirements during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </hydraulic>
+ <electric description="Electrical requirements during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </electric>
+ <heat_load description="Heat emission during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </heat_load>
+ </departure>
+ <cruise>
+ <bleed_air description="Bleed air requirement during departure">
+ <value>0.0</value>
+ <unit>kg/s</unit>
+ <default>0.0</default>
+ </bleed_air>
+ <hydraulic description="Hydraulic requirements during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </hydraulic>
+ <electric description="Electrical requirements during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </electric>
+ <heat_load description="Heat emission during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </heat_load>
+ </cruise>
+ <approach>
+ <bleed_air description="Bleed air requirement during departure">
+ <value>0.0</value>
+ <unit>kg/s</unit>
+ <default>0.0</default>
+ </bleed_air>
+ <hydraulic description="Hydraulic requirements during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </hydraulic>
+ <electric description="Electrical requirements during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </electric>
+ <heat_load description="Heat emission during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </heat_load>
+ </approach>
+ </power_demand>
+ </system>
+ </virtual_systems>
+ </aircraft_systems>
+ <systems_constants>
+ <environmental_control_system>
+ <airflow_per_pax description="Constant air mass flow per passenger">
+ <value>0.00567</value>
+ <unit>kg/S</unit>
+ <default>0.00567</default>
+ </airflow_per_pax>
+ <recirculation description="Percentage of cabin air that is reused (0.0 - 1.0)">
+ <value>0.40</value>
+ <unit>-</unit>
+ <default>0.40</default>
+ </recirculation>
+ <heat_convection description="Heat convection over aircraft skin based on Airbus air conditioning system design">
+ <value>-0.56</value>
+ <unit>W/(m^2*K)</unit>
+ <default>-0.56</default>
+ </heat_convection>
+ <cabin_temperature description="Cabin temperature">
+ <value>24</value>
+ <unit>C</unit>
+ <default>24</default>
+ </cabin_temperature>
+ <heat_sun description="specific heat flow of the sun">
+ <value>1300</value>
+ <unit>W/m2</unit>
+ <default>1300</default>
+ </heat_sun>
+ <window_area description="Window area">
+ <value>0.07</value>
+ <unit>m2</unit>
+ <default>0.07</default>
+ </window_area>
+ <heat_per_pax description="Heat emission per passenger">
+ <value>75</value>
+ <unit>W</unit>
+ <default>75</default>
+ </heat_per_pax>
+ <heat_per_light_length description="Heat emission per light specific cabin length">
+ <value>40</value>
+ <unit>W/m</unit>
+ <default>40</default>
+ </heat_per_light_length>
+ <efficiency_factor description="Efficiency of the ACP">
+ <value>0.7</value>
+ <unit>-</unit>
+ <default>0.7</default>
+ </efficiency_factor>
+ <heat_capacity_air description="Heat capacity of air">
+ <value>1005.0</value>
+ <unit>J/(kg*K)</unit>
+ <default>1005.0</default>
+ </heat_capacity_air>
+ <off_on_take_off description="Switch: Switch off ACP during launch (Airbus Getting Grips on Fuel Savings)">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </off_on_take_off>
+ <eco_mode description="ECO Mode switch: 25% reduction in bleed air withdrawal (Airbus Getting Grips on Fuel Savings)">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </eco_mode>
+ <shaft_power_sources description="Sources for possible existing shaft power consumption">
+ <number_of_power_sources description="Number of power sources">
+ <value>1</value>
+ </number_of_power_sources>
+ <power_source ID="0" description="system description of the power source">
+ <operation_factor description="Percentage of performance provided by this source">
+ <value>1.0</value>
+ <unit>-</unit>
+ </operation_factor>
+ <type description="Type of power source (Hydraulic, Electric, Engine, APU)">
+ <value>Electric</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </shaft_power_sources>
+ </environmental_control_system>
+ <furnishing>
+ <galley_load_fraction_takeoff description="Workload relative to design Power consumption during Climb, see DA Buente p. 76">
+ <value>0.2</value>
+ <unit>-</unit>
+ <default>0.2</default>
+ </galley_load_fraction_takeoff>
+ <galley_load_fraction_cruise description="Workload relative to design Power consumption during cruise, see DA Buente p. 76">
+ <value>0.6</value>
+ <unit>-</unit>
+ <default>0.7</default>
+ </galley_load_fraction_cruise>
+ <galley_load_fraction_descent description="Workload relative to design Power consumption during Descent, see DA Buente p. 76">
+ <value>0.2</value>
+ <unit>-</unit>
+ <default>0.2</default>
+ </galley_load_fraction_descent>
+ <non_personal_ife_power description="Basic power consumption of non personnel IFE system per PAX">
+ <value>1.25</value>
+ <unit>W</unit>
+ <default>1.25</default>
+ </non_personal_ife_power>
+ <power_personal_ife description="Power consumption of the personnel IFE system per PAX">
+ <value>50</value>
+ <unit>W</unit>
+ <default>50</default>
+ </power_personal_ife>
+ <personal_ife_load_fraction_climb description="Workload relative to design Power consumption during Climb">
+ <value>0.58</value>
+ <unit>-</unit>
+ <default>0.58</default>
+ </personal_ife_load_fraction_climb>
+ <personal_ife_load_fraction_cruise description="Workload relative to design Power consumption during cruise">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>0.58</default>
+ </personal_ife_load_fraction_cruise>
+ <personal_ife_load_fraction_descent description="Workload relative to design Power consumption during Descent">
+ <value>0.50</value>
+ <unit>-</unit>
+ <default>0.58</default>
+ </personal_ife_load_fraction_descent>
+ <shaft_power_sources description="Sources for possible existing shaft power consumption">
+ <number_of_power_sources description="Number of power sources">
+ <value>1</value>
+ </number_of_power_sources>
+ <power_source ID="0" description="system description of the power source">
+ <operation_factor description="Percentage of performance provided by this source">
+ <value>1.0</value>
+ <unit>-</unit>
+ </operation_factor>
+ <type description="Type of power source (Hydraulic, Electric, Engine, APU)">
+ <value>Electric</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </shaft_power_sources>
+ <location_of_galley description="CoG-location of all galleys: 0: At wing_midCenterline, 1: Behind the cockpit">
+ <value>0</value>
+ <unit>-</unit>
+ <default>0</default>
+ </location_of_galley>
+ </furnishing>
+ <ice_rain_protection>
+ <switch_off_wing_anti_icing description="Switch for operation of wing anti icing">
+ <value>0</value>
+ <unit>-</unit>
+ <default>0</default>
+ </switch_off_wing_anti_icing>
+ <top_operating_altitude description="Flight altitude up to which the wings are de-iced">
+ <value>3658</value>
+ <unit>m</unit>
+ <default>3658</default>
+ </top_operating_altitude>
+ <engine_anti_ice description="Hot air anti-icing per engine nacelle">
+ <value>0.055</value>
+ <unit>kg/s</unit>
+ <default>0.055</default>
+ </engine_anti_ice>
+ <elec_power_departure description="Electric consumption during departure, see DA Buente p. 70">
+ <value>14026.9</value>
+ <unit>W</unit>
+ <default>14026.9</default>
+ </elec_power_departure>
+ <elec_power_cruise description="Electric consumption during cruise, see DA Buente p. 70">
+ <value>13070.9</value>
+ <unit>W</unit>
+ <default>13070.9</default>
+ </elec_power_cruise>
+ <elec_power_approach description="Electric consumption during approach, see DA Buente p. 70">
+ <value>14026.9</value>
+ <unit>W</unit>
+ <default>14026.9</default>
+ </elec_power_approach>
+ <elec_power_land description="Electric consumption during Landing, see DA Buente p. 70">
+ <value>7192.9</value>
+ <unit>W</unit>
+ <default>7192.9</default>
+ </elec_power_land>
+ <skin_thickness description="Thickness of the wing skin">
+ <value>0.01</value>
+ <unit>m</unit>
+ <default>0.01</default>
+ </skin_thickness>
+ <rel_span_anti_icing_start description="Relative half span width at the start of de-icing. If DEFAULT, rel. pos of first LE device after kink (with 5% safety margin) is used.">
+ <value>0.4</value>
+ <unit>-</unit>
+ </rel_span_anti_icing_start>
+ <heat_conductivity_wing description="Thermal conductivity of the wing skin, e.g. aluminum">
+ <value>235.0</value>
+ <unit>W/mK</unit>
+ <default>235.0</default>
+ </heat_conductivity_wing>
+ <drop_diameter description="Water drop diameter, relevant between 15 and 40, default 20 microns (CS-25 Book 1 Appendix C)">
+ <value>20</value>
+ <unit>micro meter</unit>
+ <default>20</default>
+ </drop_diameter>
+ <efficiency_factor_electro_thermic_anti_icing description="Efficiency for electro-thermal de-icing">
+ <value>0.8</value>
+ <unit>-</unit>
+ <default>0.8</default>
+ </efficiency_factor_electro_thermic_anti_icing>
+ <shaft_power_sources description="Sources for possible existing shaft power consumption">
+ <number_of_power_sources description="Number of power sources">
+ <value>1</value>
+ </number_of_power_sources>
+ <power_source ID="0" description="system description of the power source">
+ <operation_factor description="Percentage of performance provided by this source">
+ <value>1.0</value>
+ <unit>-</unit>
+ </operation_factor>
+ <type description="Type of power source (Hydraulic, Electric, Engine, APU)">
+ <value>Electric</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </shaft_power_sources>
+ <percentage_of_OME description="Mass of ATA30 is percentage of operating mass empty (OME)">
+ <value>0.001</value>
+ <unit>-</unit>
+ </percentage_of_OME>
+ </ice_rain_protection>
+ <lights>
+ <navigation_light_power description="Navigation Light (red, green, white tail = 6*50) power consumption, see LTH A320 (not LED)">
+ <value>300</value>
+ <unit>W</unit>
+ <default>300</default>
+ </navigation_light_power>
+ <rotating_beacon_light_power description="Rotating Beacon light power consumption, no ref">
+ <value>400</value>
+ <unit>W</unit>
+ <default>400</default>
+ </rotating_beacon_light_power>
+ <wing_light_power description="Wing light power consumption, DA Steinke">
+ <value>500</value>
+ <unit>W</unit>
+ <default>400</default>
+ </wing_light_power>
+ <rto_light_power description="Runway turn-off light power consumption, see LTH A320 (not LED)">
+ <value>150</value>
+ <unit>W</unit>
+ <default>150</default>
+ </rto_light_power>
+ <taxi_light_power description="Taxi light power consumption, DA Steinke">
+ <value>500</value>
+ <unit>W</unit>
+ <default>500</default>
+ </taxi_light_power>
+ <landing_light_power description="Landing Light power consumption, see Honeywell A320 (not LED)">
+ <value>1200</value>
+ <unit>W</unit>
+ <default>1200</default>
+ </landing_light_power>
+ <logo_light_power description="Landing Light power consumption, see Honeywell A320 (not LED)">
+ <value>200</value>
+ <unit>W</unit>
+ <default>200</default>
+ </logo_light_power>
+ <strobe_light_power description="Strobes Light power consumption, no ref">
+ <value>100</value>
+ <unit>W</unit>
+ <default>100</default>
+ </strobe_light_power>
+ <specific_emergency_light_power description="Emergency light power consumption specific to cabin volume, see DA Buente p. 73">
+ <value>1.46</value>
+ <unit>W/m³</unit>
+ <default>1.46</default>
+ </specific_emergency_light_power>
+ <specific_cabin_light_power description="Cabin light power consumption specific to cabin volume, see DA Buente p. 73">
+ <value>18.04</value>
+ <unit>W/m³</unit>
+ <default>18.04</default>
+ </specific_cabin_light_power>
+ <flight_deck_light_power description="Flight Deck light power consumption, see DA Buente p. 73">
+ <value>904.4</value>
+ <unit>W</unit>
+ <default>904.4</default>
+ </flight_deck_light_power>
+ <shaft_power_sources description="Sources for possible existing shaft power consumption">
+ <number_of_power_sources description="Number of power sources">
+ <value>1</value>
+ </number_of_power_sources>
+ <power_source ID="0" description="system description of the power source">
+ <operation_factor description="Percentage of performance provided by this source">
+ <value>1.0</value>
+ <unit>-</unit>
+ </operation_factor>
+ <type description="Type of power source (Hydraulic, Electric, Engine, APU)">
+ <value>Electric</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </shaft_power_sources>
+ </lights>
+ <gear>
+ <efficiency_factor description="Landing gear efficiency">
+ <value>0.95</value>
+ <unit>-</unit>
+ <default>0.95</default>
+ </efficiency_factor>
+ <retraction_time description="Time to retract the landing gear">
+ <value>10.0</value>
+ <unit>s</unit>
+ <default>10.0</default>
+ </retraction_time>
+ <extension_time description="Time to extend the landing gear">
+ <value>10.0</value>
+ <unit>s</unit>
+ <default>10.0</default>
+ </extension_time>
+ <shaft_power_sources description="Sources for possible existing shaft power consumption">
+ <number_of_power_sources description="Number of power sources">
+ <value>1</value>
+ </number_of_power_sources>
+ <power_source ID="0" description="system description of the power source">
+ <operation_factor description="Percentage of performance provided by this source">
+ <value>1.0</value>
+ <unit>-</unit>
+ </operation_factor>
+ <type description="Type of power source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </shaft_power_sources>
+ </gear>
+ <flight_controls>
+ <calculate_mission_loads description="Switch for the detailed calculation of the mission loads. Otherwise average values are calculated">
+ <value>1</value>
+ <default>1</default>
+ </calculate_mission_loads>
+ <electrical_fc_system description="Switch for electrical flight control system">
+ <value>1</value>
+ <default>1</default>
+ </electrical_fc_system>
+ <common_installation_weight_factor description="Percentage of flight control system for common installation weight">
+ <value>0.25</value>
+ <default>0.25</default>
+ </common_installation_weight_factor>
+ <default_actuator description="Actuator description for automatic flight control architecture">
+ <power_source description="energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ <default>Hydraulic</default>
+ </type>
+ <source_ID description="ID of the energy source" Default="1">
+ <value>1</value>
+ <default>1</default>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <default>0.85</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in active operation (due to rudder deflections)">
+ <value>0.</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </default_actuator>
+ <ailerons>
+ <electric_flight_control_system_weight_factor description="Weight factor for electrical Flight Control system">
+ <value>0.25</value>
+ <default>0.5</default>
+ </electric_flight_control_system_weight_factor>
+ <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </default_actuator_architecture_switch>
+ <default_actuator_architecture description="Definition of the default actuator architecture">
+ <number_of_actuators_per_control_surface description="Number of actuators per control surface">
+ <value>2</value>
+ <unit></unit>
+ <default>2</default>
+ </number_of_actuators_per_control_surface>
+ <default_deflection_speed description="Deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </default_deflection_speed>
+ </default_actuator_architecture>
+ <manual_actuator_architecture description="Definition of the manual actuator architecture">
+ <number_of_control_surfaces description="Number of control surfaces to be initialized">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_control_surfaces>
+ <ailerons ID="0" description="Control surface parameters">
+ <side>right</side>
+ <deflection_speed description="Deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for Ailerons 2 actuators per control surface) (active/damping mode)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>0.85</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="1" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ <default></default>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>damping</value>
+ <default>damping</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>0.85</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </ailerons>
+ </manual_actuator_architecture>
+ </ailerons>
+ <rudders>
+ <electric_flight_control_system_weight_factor description="Weight factor for electrical Flight Control system">
+ <value>0.25</value>
+ <default>0.5</default>
+ </electric_flight_control_system_weight_factor>
+ <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </default_actuator_architecture_switch>
+ <default_actuator_architecture description="Definition of the default actuator architecture">
+ <number_of_actuators_per_control_surface description="Number of actuators per control surface">
+ <value>3</value>
+ <unit></unit>
+ <default>3</default>
+ </number_of_actuators_per_control_surface>
+ <default_deflection_speed description="Deflection speed">
+ <value>60</value>
+ <unit>deg/s</unit>
+ <default>60</default>
+ </default_deflection_speed>
+ </default_actuator_architecture>
+ <manual_actuator_architecture description="Definition of the manual actuator architecture">
+ <number_of_control_surfaces description="Number of control surfaces to be initialized">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_control_surfaces>
+ <rudder ID="0" description="Control surface parameters">
+ <deflection_speed description="deflection speed">
+ <value>60</value>
+ <unit>deg/s</unit>
+ <default>60</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for Rudder 3 actuators per control surface (all active))">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>3</value>
+ <unit>-</unit>
+ <default>3</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="1" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="2" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="3" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>damping</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>1.</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="4" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>damping</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>1.</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </rudder>
+ </manual_actuator_architecture>
+ </rudders>
+ <elevators>
+ <electric_flight_control_system_weight_factor description="Weight factor for electrical Flight Control system">
+ <value>0.25</value>
+ <unit></unit>
+ <default>0.5</default>
+ </electric_flight_control_system_weight_factor>
+ <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </default_actuator_architecture_switch>
+ <default_actuator_architecture description="Definition of the default actuator architecture">
+ <number_of_actuators_per_control_surface description="Number of actuators per control surface">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_actuators_per_control_surface>
+ <default_deflection_speed description="Deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </default_deflection_speed>
+ </default_actuator_architecture>
+ <manual_actuator_architecture description="Definition of the manual actuator architecture">
+ <number_of_control_surfaces description="Number of control surfaces to be initialized">
+ <value>2</value>
+ <default>1</default>
+ </number_of_control_surfaces>
+ <elevator ID="0" description="Control surface parameters">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for elevator 2 actuators per control surface (one active, one damping))">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="1" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>damping</value>
+ <default>damping</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </elevator>
+ <elevator ID="1" description="Control surface parameters">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for elevator 2 actuators per control surface (one active, one damping))">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="1" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>damping</value>
+ <default>damping</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </elevator>
+ </manual_actuator_architecture>
+ </elevators>
+ <spoilers>
+ <electric_flight_control_system_weight_factor description="Weight factor for electrical Flight Control system">
+ <value>0.25</value>
+ <unit></unit>
+ <default>0.5</default>
+ </electric_flight_control_system_weight_factor>
+ <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </default_actuator_architecture_switch>
+ <default_actuator_architecture description="Definition of the default actuator architecture">
+ <number_of_actuators_per_control_surface description="Number of actuators per control surface">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators_per_control_surface>
+ <default_deflection_speed description="Deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </default_deflection_speed>
+ </default_actuator_architecture>
+ <manual_actuator_architecture description="Definition of the manual actuator architecture">
+ <number_of_control_surfaces description="Number of control surfaces to be initialized">
+ <value>10</value>
+ <default>1</default>
+ </number_of_control_surfaces>
+ <spoiler ID="0" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="1" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="2" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="3" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="4" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="5" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="6" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="7" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="8" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="9" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ </manual_actuator_architecture>
+ </spoilers>
+ <trimmable_horizontal_stabilizer>
+ <number_of_trimmable_horizontal_stabilizers description="Number of all trimmable horizontal stabilizers (thsa)">
+ <value>1</value>
+ <default>1</default>
+ </number_of_trimmable_horizontal_stabilizers>
+ <electric_flight_control_system_weight_factor description="Weight factor for electrical Flight Control system">
+ <value>0.5</value>
+ <unit></unit>
+ <default>0.5</default>
+ </electric_flight_control_system_weight_factor>
+ <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </default_actuator_architecture_switch>
+ <default_actuator_architecture description="Definition of the default actuator architecture">
+ <number_of_actuators_per_control_surface description="Number of actuators per control surface">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_actuators_per_control_surface>
+ <default_deflection_speed description="Deflection speed">
+ <value>0.5</value>
+ <unit>deg/s</unit>
+ <default>0.5</default>
+ </default_deflection_speed>
+ </default_actuator_architecture>
+ <manual_actuator_architecture description="Definition of the manual actuator architecture">
+ <number_of_control_surfaces description="Number of control surfaces to be initialized">
+ <value>2</value>
+ <default>1</default>
+ </number_of_control_surfaces>
+ <thsa ID="0" description="Control surface parameters">
+ <deflection_speed description="deflection speed">
+ <value>0.5</value>
+ <unit>deg/s</unit>
+ <default>0.5</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for THSA 2 actuators (both active))">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="1" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </thsa>
+ </manual_actuator_architecture>
+ </trimmable_horizontal_stabilizer>
+ <high_lift_system>
+ <trailing_edge>
+ <electric_flight_control_system_weight_factor description="Weight factor for electrical Flight Control system">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>2.0</default>
+ </electric_flight_control_system_weight_factor>
+ <number_of_devices description="Number of trailing edge systems">
+ <value>2</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_devices>
+ <trailing_edge_device ID="0">
+ <power_control_unit>
+ <number_of_power_control_unit_motors description="Number of PCU motors">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_power_control_unit_motors>
+ <power_control_unit_motor ID="0">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </active_power>
+ </power_control_unit_motor>
+ <power_control_unit_motor ID="1">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </active_power>
+ </power_control_unit_motor>
+ </power_control_unit>
+ </trailing_edge_device>
+ <trailing_edge_device ID="1">
+ <power_control_unit>
+ <number_of_power_control_unit_motors description="Number of PCU motors">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_power_control_unit_motors>
+ <power_control_unit_motor ID="0">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </active_power>
+ </power_control_unit_motor>
+ <power_control_unit_motor ID="1">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </active_power>
+ </power_control_unit_motor>
+ </power_control_unit>
+ </trailing_edge_device>
+ </trailing_edge>
+ <leading_edge>
+ <electric_flight_control_system_weight_factor description="Weight factor for electrical Flight Control system">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>1.0</default>
+ </electric_flight_control_system_weight_factor>
+ <number_of_devices description="Number of front edge systems">
+ <value>0</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_devices>
+ <leading_edge_device ID="0">
+ <power_control_unit>
+ <number_of_power_control_unit_motors description="Number of PCU motors">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_power_control_unit_motors>
+ <power_control_unit_motor ID="0">
+ <power_source description="Energy source" default="-">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)" default="-">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </power_control_unit_motor>
+ <power_control_unit_motor ID="1">
+ <power_source description="Energy source" default="-">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)" default="-">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <unit></unit>
+ <default>active</default>
+ </operation_mode>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </power_control_unit_motor>
+ </power_control_unit>
+ </leading_edge_device>
+ </leading_edge>
+ <duration_high_lift_deployment description="Extension time of the high-lift system">
+ <value>22.0</value>
+ <unit>s</unit>
+ <default>22.0</default>
+ </duration_high_lift_deployment>
+ </high_lift_system>
+ </flight_controls>
+ <bleed_air>
+ <temperature_bleed_air description="Temperature of Bleed Air during extraction">
+ <value>200</value>
+ <unit>C</unit>
+ <default>200</default>
+ </temperature_bleed_air>
+ <efficiency_factor_bleed_air_system description="Efficiency of the Bleed Air system, e.g. leakage losses">
+ <value>0.95</value>
+ <unit>-</unit>
+ <default>0.95</default>
+ </efficiency_factor_bleed_air_system>
+ <specific_ducting_mass description="Specific weight of Bleed Air pipes">
+ <value>4.5</value>
+ <unit>kg/m</unit>
+ <default>4.5</default>
+ </specific_ducting_mass>
+ </bleed_air>
+ <hydraulic_system>
+ <pressure description="Nominal pressure of the hydraulic system">
+ <value>20684000</value>
+ <unit>Pa</unit>
+ <default>20684000</default>
+ </pressure>
+ <efficiency_factor_hydraulic_system description="Efficiency of the hydraulic system, e.g. leakage losses">
+ <value>0.95</value>
+ <unit>-</unit>
+ <default>0.95</default>
+ </efficiency_factor_hydraulic_system>
+ <rel_max_power description="Ratio of maximum permanent power and maximum required power of all pumps">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>1.0</default>
+ </rel_max_power>
+ <specific_ducting_mass description="Specific weight of hydraulic lines">
+ <value>2.5</value>
+ <unit>kg/m</unit>
+ <default>2.5</default>
+ </specific_ducting_mass>
+ <specific_fluid_mass description="Specific weight of hydraulic fluid">
+ <value>0.75</value>
+ <unit>kg/m</unit>
+ <default>0.75</default>
+ </specific_fluid_mass>
+ <specific_pump_mass description="Specific weight of hydraulic pumps">
+ <value>1250</value>
+ <unit>kg/W</unit>
+ <default>1250</default>
+ </specific_pump_mass>
+ <hydraulic_circuits description="Detailed description of the hydraulic circuits">
+ <number_of_circuits description="Number of hydraulic circuits">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_circuits>
+ <hydraulic_circuit ID="0" description="Hydraulic circuit description">
+ <compartment_reference_point description="Reference point of the Hydraulic Compartment (distributor seat, reservoir, etc.)">
+ <x description="X-Distance to nose in relation to fuselage length">
+ <value>0.4</value>
+ <unit>-</unit>
+ <default>0.4</default>
+ </x>
+ <y description="Y-Distance to symmetry line in relation to half span">
+ <value>0.0</value>
+ <unit>-</unit>
+ <default>0.0</default>
+ </y>
+ <z description="Z-distance to symmetry line in relation to fuselage height">
+ <value>0.0</value>
+ <unit>-</unit>
+ <default>0.0</default>
+ </z>
+ </compartment_reference_point>
+ <components description="Components within the circuit">
+ <pumps description="Pumps">
+ <number_of_pumps description="Number of pumps">
+ <value>2</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_pumps>
+ <pump ID="0" description="Pump description">
+ <name description="Name of the pump">
+ <value>EDP</value>
+ </name>
+ <type description="Type of pump (Currently 3 types: Electric, EngineDriven, RAT)">
+ <value>EngineDriven</value>
+ <default>EngineDriven</default>
+ </type>
+ <efficiency description="Pump efficiency">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>0.85</default>
+ </efficiency>
+ <operation_factor description="Percentage of total pump power in normal operation (value must be between">
+ <value>0.8</value>
+ <unit></unit>
+ <default>1</default>
+ </operation_factor>
+ <power_source description="Energy source for the pump">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Engine</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </pump>
+ <pump ID="1" description="Pump description">
+ <name description="Name of the pump">
+ <value>EMP</value>
+ </name>
+ <type description="Type of pump (Currently 3 types: Electric, EngineDriven, RAT)">
+ <value>Electric</value>
+ <default>EngineDriven</default>
+ </type>
+ <efficiency description="Pump efficiency">
+ <value>0.7</value>
+ <unit>-</unit>
+ <default>0.95</default>
+ </efficiency>
+ <operation_factor description="Percentage of total pump power in normal operation (value must be between 0 and 1. 0=off, 1=total)">
+ <value>0.2</value>
+ <unit>-</unit>
+ <default>1</default>
+ </operation_factor>
+ <power_source description="Energy source for the pump">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Electric</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </pump>
+ </pumps>
+ <not_specified description="Description of the remaining components in the hydraulic circuit (without lines... are calculated internally!)">
+ <mass_factor description="Mass fraction of remaining components in the hydraulic circuit">
+ <value>0.</value>
+ <unit>-</unit>
+ <default>0.</default>
+ </mass_factor>
+ </not_specified>
+ </components>
+ </hydraulic_circuit>
+ </hydraulic_circuits>
+ <power_transfer_units description="System description of the Power Transfer Units">
+ <number_of_power_transfer_units description="Number of PTUs">
+ <value>0</value>
+ <unit>-</unit>
+ <default>0</default>
+ </number_of_power_transfer_units>
+ <power_transfer_unit ID="0" description="System description of the PTU">
+ <power_transfer_unit_connection ID="0" description="1. Circuit to which the PTU is connected">
+ <value>-</value>
+ </power_transfer_unit_connection>
+ <power_transfer_unit_connection ID="1" description="2. Circuit to which the PTU is connected">
+ <value>-</value>
+ </power_transfer_unit_connection>
+ </power_transfer_unit>
+ </power_transfer_units>
+ </hydraulic_system>
+ <electric_system>
+ <efficiency_factor_electric_system description="Efficiency of the electrical system, e.g. resistance of the cables">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>1.0</default>
+ </efficiency_factor_electric_system>
+ <rel_max_power description="Ratio of maximum permanent power and maximum required power of all generators">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>1.0</default>
+ </rel_max_power>
+ <specific_cable_mass description="Specific weight of electrical wiring">
+ <value>6.5</value>
+ <unit>kg/m</unit>
+ <default>6.5</default>
+ </specific_cable_mass>
+ <electric_circuits description="Detailed description of the electrical circuits">
+ <number_of_circuits description="Number of electric circuits">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_circuits>
+ <electric_circuit ID="0" description="System description electrical circuit">
+ <components description="Components within the cycle">
+ <generators description="Generators">
+ <number_of_generators description="Number of generators">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_generators>
+ <generator ID="0" description="System description of the generator">
+ <name description="Name of generator">
+ <value>IDG1</value>
+ </name>
+ <type description="Type of generators">
+ <value>IDG</value>
+ </type>
+ <generator_efficiency description="Efficiency of the generator including accessory gear box">
+ <value>0.665</value>
+ <unit>-</unit>
+ <default>0.665</default>
+ </generator_efficiency>
+ <operation_factor description="Share of total power in normal operation (value must be between 0 and 1. 0=off, 1=total)">
+ <value>1</value>
+ <default>1</default>
+ </operation_factor>
+ <power_source description="Energy source of generator">
+ <type description="Type of energy source (hydraulic, electric, engine, APU)">
+ <value>Engine</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </generator>
+ </generators>
+ <not_specified description="System description of the remaining components in the electrical circuit (without cable/plug... are calculated internally!)">
+ <mass_factor description="Mass fraction of the remaining components">
+ <value>0.</value>
+ <unit>-</unit>
+ <default>0.</default>
+ </mass_factor>
+ </not_specified>
+ </components>
+ </electric_circuit>
+ </electric_circuits>
+ </electric_system>
+ <propulsion_system>
+ <percentage_bleed_air description="Percentage of bleed air generated by the engine">
+ <value>1.00</value>
+ <unit>-</unit>
+ <default>1.00</default>
+ </percentage_bleed_air>
+ <percentage_electrical_power description="Percentage of electrical energy generated by the engine">
+ <value>1.00</value>
+ <unit>-</unit>
+ <default>1.00</default>
+ </percentage_electrical_power>
+ <percentage_hydraulic_power description="Percentage of hydraulic energy generated by the engine">
+ <value>1.00</value>
+ <unit>-</unit>
+ <default>1.00</default>
+ </percentage_hydraulic_power>
+ <efficiency_factor_bleed_air description="Efficiency of Bleed Air withdrawal">
+ <value>0.95</value>
+ <unit>-</unit>
+ <default>0.95</default>
+ </efficiency_factor_bleed_air>
+ </propulsion_system>
+ <auxiliary_power_unit>
+ <position_of_auxiliary_power_unit_in_fuselage_length description="Relative position of the APU in reference to the total fuselage length">
+ <value>0.95</value>
+ <unit>-</unit>
+ <default>0.95</default>
+ </position_of_auxiliary_power_unit_in_fuselage_length>
+ <percentage_bleed_air description="Percentage of Bleed Air generated by the APU">
+ <value>0.00</value>
+ <unit>-</unit>
+ <default>0.00</default>
+ </percentage_bleed_air>
+ <percentage_electrical_power description="Percentage of electrical energy generated by the APU">
+ <value>0.00</value>
+ <unit>-</unit>
+ <default>0.00</default>
+ </percentage_electrical_power>
+ <percentage_hydraulic_power description="Percentage of hydraulic energy generated by the APU">
+ <value>0.0</value>
+ <unit>-</unit>
+ <default>0.00</default>
+ </percentage_hydraulic_power>
+ <efficiency_factor_bleed_air description="Efficiency of Bleed Air withdrawal">
+ <value>0.90</value>
+ <unit>-</unit>
+ <default>0.90</default>
+ </efficiency_factor_bleed_air>
+ <installation_factor description="Installation factor for attached parts such as fire protection, noise protection, etc.">
+ <value>1.5</value>
+ <unit>-</unit>
+ <default>1.5</default>
+ </installation_factor>
+ <design_loads>
+ <percentage_bleed_air description="Percentage of Bleed Air for which the APU is designed">
+ <value>0.30</value>
+ <unit>-</unit>
+ <default>0.30</default>
+ </percentage_bleed_air>
+ <percentage_electrical_power description="Percentage of electrical energy for which the APU is designed">
+ <value>0.50</value>
+ <unit>-</unit>
+ <default>0.50</default>
+ </percentage_electrical_power>
+ <percentage_hydraulic_power description="Percentage of hydraulic energy for which the APU is designed">
+ <value>0.50</value>
+ <unit>-</unit>
+ <default>0.50</default>
+ </percentage_hydraulic_power>
+ </design_loads>
+ </auxiliary_power_unit>
+ <avionics description="Components grouped inside ATAXX">
+ <location_of_aviationics_bay description="0: Wing root, 1: Nose, 2: Behind cockpit">
+ <value>0</value>
+ <unit>-</unit>
+ <default>0</default>
+ </location_of_aviationics_bay>
+ </avionics>
+ <remaining_consumers>
+ <power description="Additional percentages of bleed, electric, and hydraulic power for ATA-XX">
+ <percentage_bleed_air description="Percentage of unrecorded performances">
+ <value>0.00</value>
+ <unit>-</unit>
+ <default>0.0</default>
+ </percentage_bleed_air>
+ <percentage_electric description="Percentage of unrecorded performances">
+ <value>0.104</value>
+ <unit>-</unit>
+ <default>0.104</default>
+ </percentage_electric>
+ <percentage_hydraulic description="Percentage of unrecorded performances">
+ <value>0.05</value>
+ <unit>-</unit>
+ <default>0.05</default>
+ </percentage_hydraulic>
+ </power>
+ <mass>
+ <scaling_factor description="Scaling of ATA-XX mass">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </scaling_factor>
+ <distribution description="Distribution of ATA-XX mass to single components">
+ <percentage_instrumentation_of_ATAXX description="Percentage of instrumentation in ATA-XX">
+ <value>0.08</value>
+ <unit>-</unit>
+ <default>0.08</default>
+ </percentage_instrumentation_of_ATAXX>
+ <percentage_auto_flight_of_ATAXX description="Percentage of AFS in ATA-XX">
+ <value>0.13</value>
+ <unit>-</unit>
+ <default>0.13</default>
+ </percentage_auto_flight_of_ATAXX>
+ <percentage_navigation_of_ATAXX description="Percentage of the navigation system in ATA-XX">
+ <value>0.53</value>
+ <unit>-</unit>
+ <default>0.53</default>
+ </percentage_navigation_of_ATAXX>
+ <percentage_communication_of_ATAXX description="Percentage of the communication system in ATA-XX">
+ <value>0.26</value>
+ <unit>-</unit>
+ <default>0.26</default>
+ </percentage_communication_of_ATAXX>
+ </distribution>
+ </mass>
+ </remaining_consumers>
+ </systems_constants>
+ </program_settings>
+</module_configuration_file>
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/xml_configs/systemsDesign_conf_default.xml b/UnicadoGUI/Backend/xml_configs/systemsDesign_conf_default.xml
new file mode 100644
index 0000000..fd1f7b1
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/systemsDesign_conf_default.xml
@@ -0,0 +1,2437 @@
+<?xml version="1.0" encoding="utf-8"?>
+<module_configuration_file name="systemsDesign_conf.xml">
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>writing_test.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>X:/UNICADO/AircraftReferences/CSR/CSR-02/cleanSheetDesign/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>1</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_3</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_3</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>true</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>false</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>TOOLNAME_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>TOOLNAME.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>C:/Programs/UNICADOworkflow/inkscape/</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>C:/Programs/UNICADOworkflow/gnuplot/</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings>
+ <modes description="mode selection, only STANDARD available currently">
+ <value>STANDARD</value>
+ <default>STANDARD</default>
+ </modes>
+ <design_case description="Switch for system sizing. 1: Sizing, 0: ONLY determination of a load profile for a specific mission">
+ <value>1</value>
+ <default>1</default>
+ </design_case>
+ <offtakes_for_requirement_mission description="Determination of Offtakes for Requirement Mission">
+ <value>0</value>
+ <default>0</default>
+ </offtakes_for_requirement_mission>
+ <scaling_factors description="Variable scaling factors to change the calculated masses">
+ <systems description="Systems: 1 = full calculated weight">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>1</default>
+ </systems>
+ <furnishings description="Furnishings: 1 = on; 0 = off">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>1</default>
+ </furnishings>
+ <operator_items description="OperatorItems: 1 = full calculated weight">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>1</default>
+ </operator_items>
+ </scaling_factors>
+ <tex_report_without_masses description="1: TeX report only with approvals, since mass breakdown comes from massEstimation">
+ <value>1</value>
+ <default>1</default>
+ </tex_report_without_masses>
+ <control_device_warning description="Warning is issued if no suitable method is available for ControlDevice.">
+ <value>1</value>
+ <default>1</default>
+ </control_device_warning>
+ <aircraft_systems>
+ <energy_sinks>
+ <number_of_sinks description="Number of energy sinks">
+ <value>9</value>
+ <default>20</default>
+ </number_of_sinks>
+ <system ID="0">
+ <system_description description="Type of furnishing system">
+ <value>conventionalFurnishing</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="1">
+ <system_description description="Type of fuel system">
+ <value>conventionalFuel</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="2">
+ <system_description description="Type of system ice and rain protection system (conventional or electrical">
+ <value>conventionalIceRainProtection</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="3">
+ <system_description description="Type of lighting system">
+ <value>conventionalLighting</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="4">
+ <system_description description="Type of fire protection system">
+ <value>conventionalFireProtection</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="5">
+ <system_description description="Type of oxygen system">
+ <value>conventionalOxygenSystem</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="6">
+ <system_description description="Type of gear system">
+ <value>conventionalGear</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="7">
+ <system_description description="Type of flight control system">
+ <value>conventionalFlightControl</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="8">
+ <system_description description="remaining consumer system">
+ <value>remainingConsumers</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ </energy_sinks>
+ <environmental_control_system>
+ <system_description Unit="-" description="Type of environmental control system (ECS)">
+ <value>conventionalECS</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </environmental_control_system>
+ <energy_sources>
+ <number_of_sources description="Number of energy sources">
+ <value>2</value>
+ <default>1</default>
+ </number_of_sources>
+ <system ID="0">
+ <system_description description="Type of propulsion system">
+ <value>conventionalPropulsion</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ <uses_fuel description="Switch whether the energy source uses fuel. 1:yes, 0:no fuel">
+ <value>1</value>
+ <default>1</default>
+ </uses_fuel>
+ </system>
+ <system ID="1">
+ <system_description description="Type of auxiliary power unit (APU) system (conventionalAPU or fuelCellAPU)">
+ <value>conventionalAPU</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ <uses_fuel description="Switch whether the energy source uses fuel. 1:yes, 0:no fuel">
+ <value>1</value>
+ <default>1</default>
+ </uses_fuel>
+ </system>
+ <system ID="2">
+ <system_description description="Fuel cell">
+ <value>fuelCell</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ <uses_fuel description="Switch whether the energy source uses fuel. 1:yes, 0:no fuel">
+ <value>1</value>
+ <default>1</default>
+ </uses_fuel>
+ </system>
+ </energy_sources>
+ <energy_conductors>
+ <number_of_conductors description="Number of energy conductor systems">
+ <value>3</value>
+ <default>3</default>
+ </number_of_conductors>
+ <system ID="0">
+ <system_description description="Type of system">
+ <value>BleedAirSystem</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="1">
+ <system_description description="Type of system">
+ <value>HydraulicSystem</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ <system ID="2">
+ <system_description description="Type of system">
+ <value>ElectricSystem</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ </system>
+ </energy_conductors>
+ <virtual_systems>
+ <number_of_virtual_systems description="Number of energy systems">
+ <value>0</value>
+ <default></default>
+ </number_of_virtual_systems>
+ <system ID="0">
+ <system_description description="Type of virtual system">
+ <value>virtualSystem</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ <mass description="mass of the system">
+ <value>5000.0</value>
+ <unit>kg</unit>
+ <default>0.0</default>
+ </mass>
+ <center_of_gravity description="position of mass item to global point of reference">
+ <x description="Position of reference in x-direction">
+ <value>0</value>
+ <unit>m</unit>
+ </x>
+ <y description="Position of reference in y-direction">
+ <value>0</value>
+ <unit>m</unit>
+ </y>
+ <z description="Position of reference in z-direction">
+ <value>0</value>
+ <unit>m</unit>
+ </z>
+ </center_of_gravity>
+ <power_demand>
+ <departure>
+ <bleed_air description="Bleed air requirement during departure">
+ <value>3.0</value>
+ <unit>kg/s</unit>
+ <default>0.0</default>
+ </bleed_air>
+ <hydraulic description="Hydraulic requirements during departure">
+ <value>10000.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </hydraulic>
+ <electric description="Electrical requirements during departure">
+ <value>15000.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </electric>
+ <heat_load description="Heat emission during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </heat_load>
+ </departure>
+ <cruise>
+ <bleed_air description="Bleed air requirement during departure">
+ <value>0.5</value>
+ <unit>kg/s</unit>
+ <default>0.0</default>
+ </bleed_air>
+ <hydraulic description="Hydraulic requirements during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </hydraulic>
+ <electric description="Electrical requirements during departure">
+ <value>20000.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </electric>
+ <heat_load description="Heat emission during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </heat_load>
+ </cruise>
+ <approach>
+ <bleed_air description="Bleed air requirement during departure">
+ <value>3.5</value>
+ <unit>kg/s</unit>
+ <default>0.0</default>
+ </bleed_air>
+ <hydraulic description="Hydraulic requirements during departure">
+ <value>7500.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </hydraulic>
+ <electric description="Electrical requirements during departure">
+ <value>18000.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </electric>
+ <heat_load description="Heat emission during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </heat_load>
+ </approach>
+ </power_demand>
+ </system>
+ <system ID="0">
+ <system_description description="Type of system">
+ <value>virtualSystem</value>
+ </system_description>
+ <operating_switch description="Switch whether the system is operated 1: on, 0: off (the mass is also determined for a switched off system!)">
+ <value>1</value>
+ <default>1</default>
+ </operating_switch>
+ <mass description="mass of the system">
+ <value>1000.0</value>
+ <unit>kg</unit>
+ <default>0.0</default>
+ </mass>
+ <center_of_gravity description="position of mass item to global point of reference">
+ <x description="Position of reference in x-direction">
+ <value>0</value>
+ <unit>m</unit>
+ </x>
+ <y description="Position of reference in y-direction">
+ <value>0</value>
+ <unit>m</unit>
+ </y>
+ <z description="Position of reference in z-direction">
+ <value>0</value>
+ <unit>m</unit>
+ </z>
+ </center_of_gravity>
+ <power_demand>
+ <departure>
+ <bleed_air description="Bleed air requirement during departure">
+ <value>0.0</value>
+ <unit>kg/s</unit>
+ <default>0.0</default>
+ </bleed_air>
+ <hydraulic description="Hydraulic requirements during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </hydraulic>
+ <electric description="Electrical requirements during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </electric>
+ <heat_load description="Heat emission during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </heat_load>
+ </departure>
+ <cruise>
+ <bleed_air description="Bleed air requirement during departure">
+ <value>0.0</value>
+ <unit>kg/s</unit>
+ <default>0.0</default>
+ </bleed_air>
+ <hydraulic description="Hydraulic requirements during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </hydraulic>
+ <electric description="Electrical requirements during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </electric>
+ <heat_load description="Heat emission during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </heat_load>
+ </cruise>
+ <approach>
+ <bleed_air description="Bleed air requirement during departure">
+ <value>0.0</value>
+ <unit>kg/s</unit>
+ <default>0.0</default>
+ </bleed_air>
+ <hydraulic description="Hydraulic requirements during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </hydraulic>
+ <electric description="Electrical requirements during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </electric>
+ <heat_load description="Heat emission during departure">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </heat_load>
+ </approach>
+ </power_demand>
+ </system>
+ </virtual_systems>
+ </aircraft_systems>
+ <systems_constants>
+ <environmental_control_system>
+ <airflow_per_pax description="Constant air mass flow per passenger">
+ <value>0.00567</value>
+ <unit>kg/S</unit>
+ <default>0.00567</default>
+ </airflow_per_pax>
+ <recirculation description="Percentage of cabin air that is reused (0.0 - 1.0)">
+ <value>0.40</value>
+ <unit>-</unit>
+ <default>0.40</default>
+ </recirculation>
+ <heat_convection description="Heat convection over aircraft skin based on Airbus air conditioning system design">
+ <value>-0.56</value>
+ <unit>W/(m^2*K)</unit>
+ <default>-0.56</default>
+ </heat_convection>
+ <cabin_temperature description="Cabin temperature">
+ <value>24</value>
+ <unit>C</unit>
+ <default>24</default>
+ </cabin_temperature>
+ <heat_sun description="specific heat flow of the sun">
+ <value>1300</value>
+ <unit>W/m2</unit>
+ <default>1300</default>
+ </heat_sun>
+ <window_area description="Window area">
+ <value>0.07</value>
+ <unit>m2</unit>
+ <default>0.07</default>
+ </window_area>
+ <heat_per_pax description="Heat emission per passenger">
+ <value>75</value>
+ <unit>W</unit>
+ <default>75</default>
+ </heat_per_pax>
+ <heat_per_light_length description="Heat emission per light specific cabin length">
+ <value>40</value>
+ <unit>W/m</unit>
+ <default>40</default>
+ </heat_per_light_length>
+ <efficiency_factor description="Efficiency of the ACP">
+ <value>0.7</value>
+ <unit>-</unit>
+ <default>0.7</default>
+ </efficiency_factor>
+ <heat_capacity_air description="Heat capacity of air">
+ <value>1005.0</value>
+ <unit>J/(kg*K)</unit>
+ <default>1005.0</default>
+ </heat_capacity_air>
+ <off_on_take_off description="Switch: Switch off ACP during launch (Airbus Getting Grips on Fuel Savings)">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </off_on_take_off>
+ <eco_mode description="ECO Mode switch: 25% reduction in bleed air withdrawal (Airbus Getting Grips on Fuel Savings)">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </eco_mode>
+ <shaft_power_sources description="Sources for possible existing shaft power consumption">
+ <number_of_power_sources description="Number of power sources">
+ <value>1</value>
+ </number_of_power_sources>
+ <power_source ID="0" description="system description of the power source">
+ <operation_factor description="Percentage of performance provided by this source">
+ <value>1.0</value>
+ <unit>-</unit>
+ </operation_factor>
+ <type description="Type of power source (Hydraulic, Electric, Engine, APU)">
+ <value>Electric</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </shaft_power_sources>
+ </environmental_control_system>
+ <furnishing>
+ <galley_load_fraction_takeoff description="Workload relative to design Power consumption during Climb, see DA Buente p. 76">
+ <value>0.2</value>
+ <unit>-</unit>
+ <default>0.2</default>
+ </galley_load_fraction_takeoff>
+ <galley_load_fraction_cruise description="Workload relative to design Power consumption during cruise, see DA Buente p. 76">
+ <value>0.6</value>
+ <unit>-</unit>
+ <default>0.7</default>
+ </galley_load_fraction_cruise>
+ <galley_load_fraction_descent description="Workload relative to design Power consumption during Descent, see DA Buente p. 76">
+ <value>0.2</value>
+ <unit>-</unit>
+ <default>0.2</default>
+ </galley_load_fraction_descent>
+ <non_personal_ife_power description="Basic power consumption of non personnel IFE system per PAX">
+ <value>1.25</value>
+ <unit>W</unit>
+ <default>1.25</default>
+ </non_personal_ife_power>
+ <power_personal_ife description="Power consumption of the personnel IFE system per PAX">
+ <value>50</value>
+ <unit>W</unit>
+ <default>50</default>
+ </power_personal_ife>
+ <personal_ife_load_fraction_climb description="Workload relative to design Power consumption during Climb">
+ <value>0.58</value>
+ <unit>-</unit>
+ <default>0.58</default>
+ </personal_ife_load_fraction_climb>
+ <personal_ife_load_fraction_cruise description="Workload relative to design Power consumption during cruise">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>0.58</default>
+ </personal_ife_load_fraction_cruise>
+ <personal_ife_load_fraction_descent description="Workload relative to design Power consumption during Descent">
+ <value>0.50</value>
+ <unit>-</unit>
+ <default>0.58</default>
+ </personal_ife_load_fraction_descent>
+ <shaft_power_sources description="Sources for possible existing shaft power consumption">
+ <number_of_power_sources description="Number of power sources">
+ <value>1</value>
+ </number_of_power_sources>
+ <power_source ID="0" description="system description of the power source">
+ <operation_factor description="Percentage of performance provided by this source">
+ <value>1.0</value>
+ <unit>-</unit>
+ </operation_factor>
+ <type description="Type of power source (Hydraulic, Electric, Engine, APU)">
+ <value>Electric</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </shaft_power_sources>
+ <location_of_galley description="CoG-location of all galleys: 0: At wing_midCenterline, 1: Behind the cockpit">
+ <value>0</value>
+ <unit>-</unit>
+ <default>0</default>
+ </location_of_galley>
+ </furnishing>
+ <ice_rain_protection>
+ <switch_off_wing_anti_icing description="Switch for operation of wing anti icing">
+ <value>0</value>
+ <unit>-</unit>
+ <default>0</default>
+ </switch_off_wing_anti_icing>
+ <top_operating_altitude description="Flight altitude up to which the wings are de-iced">
+ <value>3658</value>
+ <unit>m</unit>
+ <default>3658</default>
+ </top_operating_altitude>
+ <engine_anti_ice description="Hot air anti-icing per engine nacelle">
+ <value>0.055</value>
+ <unit>kg/s</unit>
+ <default>0.055</default>
+ </engine_anti_ice>
+ <elec_power_departure description="Electric consumption during departure, see DA Buente p. 70">
+ <value>14026.9</value>
+ <unit>W</unit>
+ <default>14026.9</default>
+ </elec_power_departure>
+ <elec_power_cruise description="Electric consumption during cruise, see DA Buente p. 70">
+ <value>13070.9</value>
+ <unit>W</unit>
+ <default>13070.9</default>
+ </elec_power_cruise>
+ <elec_power_approach description="Electric consumption during approach, see DA Buente p. 70">
+ <value>14026.9</value>
+ <unit>W</unit>
+ <default>14026.9</default>
+ </elec_power_approach>
+ <elec_power_land description="Electric consumption during Landing, see DA Buente p. 70">
+ <value>7192.9</value>
+ <unit>W</unit>
+ <default>7192.9</default>
+ </elec_power_land>
+ <skin_thickness description="Thickness of the wing skin">
+ <value>0.01</value>
+ <unit>m</unit>
+ <default>0.01</default>
+ </skin_thickness>
+ <rel_span_anti_icing_start description="Relative half span width at the start of de-icing. If DEFAULT, rel. pos of first LE device after kink (with 5% safety margin) is used.">
+ <value>0.4</value>
+ <unit>-</unit>
+ </rel_span_anti_icing_start>
+ <heat_conductivity_wing description="Thermal conductivity of the wing skin, e.g. aluminum">
+ <value>235.0</value>
+ <unit>W/mK</unit>
+ <default>235.0</default>
+ </heat_conductivity_wing>
+ <drop_diameter description="Water drop diameter, relevant between 15 and 40, default 20 microns (CS-25 Book 1 Appendix C)">
+ <value>20</value>
+ <unit>micro meter</unit>
+ <default>20</default>
+ </drop_diameter>
+ <efficiency_factor_electro_thermic_anti_icing description="Efficiency for electro-thermal de-icing">
+ <value>0.8</value>
+ <unit>-</unit>
+ <default>0.8</default>
+ </efficiency_factor_electro_thermic_anti_icing>
+ <shaft_power_sources description="Sources for possible existing shaft power consumption">
+ <number_of_power_sources description="Number of power sources">
+ <value>1</value>
+ </number_of_power_sources>
+ <power_source ID="0" description="system description of the power source">
+ <operation_factor description="Percentage of performance provided by this source">
+ <value>1.0</value>
+ <unit>-</unit>
+ </operation_factor>
+ <type description="Type of power source (Hydraulic, Electric, Engine, APU)">
+ <value>Electric</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </shaft_power_sources>
+ <percentage_of_OME description="Mass of ATA30 is percentage of operating mass empty (OME)">
+ <value>0.001</value>
+ <unit>-</unit>
+ </percentage_of_OME>
+ </ice_rain_protection>
+ <lights>
+ <navigation_light_power description="Navigation Light (red, green, white tail = 6*50) power consumption, see LTH A320 (not LED)">
+ <value>300</value>
+ <unit>W</unit>
+ <default>300</default>
+ </navigation_light_power>
+ <rotating_beacon_light_power description="Rotating Beacon light power consumption, no ref">
+ <value>400</value>
+ <unit>W</unit>
+ <default>400</default>
+ </rotating_beacon_light_power>
+ <wing_light_power description="Wing light power consumption, DA Steinke">
+ <value>500</value>
+ <unit>W</unit>
+ <default>400</default>
+ </wing_light_power>
+ <rto_light_power description="Runway turn-off light power consumption, see LTH A320 (not LED)">
+ <value>150</value>
+ <unit>W</unit>
+ <default>150</default>
+ </rto_light_power>
+ <taxi_light_power description="Taxi light power consumption, DA Steinke">
+ <value>500</value>
+ <unit>W</unit>
+ <default>500</default>
+ </taxi_light_power>
+ <landing_light_power description="Landing Light power consumption, see Honeywell A320 (not LED)">
+ <value>1200</value>
+ <unit>W</unit>
+ <default>1200</default>
+ </landing_light_power>
+ <logo_light_power description="Landing Light power consumption, see Honeywell A320 (not LED)">
+ <value>200</value>
+ <unit>W</unit>
+ <default>200</default>
+ </logo_light_power>
+ <strobe_light_power description="Strobes Light power consumption, no ref">
+ <value>100</value>
+ <unit>W</unit>
+ <default>100</default>
+ </strobe_light_power>
+ <specific_emergency_light_power description="Emergency light power consumption specific to cabin volume, see DA Buente p. 73">
+ <value>1.46</value>
+ <unit>W/m³</unit>
+ <default>1.46</default>
+ </specific_emergency_light_power>
+ <specific_cabin_light_power description="Cabin light power consumption specific to cabin volume, see DA Buente p. 73">
+ <value>18.04</value>
+ <unit>W/m³</unit>
+ <default>18.04</default>
+ </specific_cabin_light_power>
+ <flight_deck_light_power description="Flight Deck light power consumption, see DA Buente p. 73">
+ <value>904.4</value>
+ <unit>W</unit>
+ <default>904.4</default>
+ </flight_deck_light_power>
+ <shaft_power_sources description="Sources for possible existing shaft power consumption">
+ <number_of_power_sources description="Number of power sources">
+ <value>1</value>
+ </number_of_power_sources>
+ <power_source ID="0" description="system description of the power source">
+ <operation_factor description="Percentage of performance provided by this source">
+ <value>1.0</value>
+ <unit>-</unit>
+ </operation_factor>
+ <type description="Type of power source (Hydraulic, Electric, Engine, APU)">
+ <value>Electric</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </shaft_power_sources>
+ </lights>
+ <gear>
+ <efficiency_factor description="Landing gear efficiency">
+ <value>0.95</value>
+ <unit>-</unit>
+ <default>0.95</default>
+ </efficiency_factor>
+ <retraction_time description="Time to retract the landing gear">
+ <value>10.0</value>
+ <unit>s</unit>
+ <default>10.0</default>
+ </retraction_time>
+ <extension_time description="Time to extend the landing gear">
+ <value>10.0</value>
+ <unit>s</unit>
+ <default>10.0</default>
+ </extension_time>
+ <shaft_power_sources description="Sources for possible existing shaft power consumption">
+ <number_of_power_sources description="Number of power sources">
+ <value>1</value>
+ </number_of_power_sources>
+ <power_source ID="0" description="system description of the power source">
+ <operation_factor description="Percentage of performance provided by this source">
+ <value>1.0</value>
+ <unit>-</unit>
+ </operation_factor>
+ <type description="Type of power source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </shaft_power_sources>
+ </gear>
+ <flight_controls>
+ <calculate_mission_loads description="Switch for the detailed calculation of the mission loads. Otherwise average values are calculated">
+ <value>1</value>
+ <default>1</default>
+ </calculate_mission_loads>
+ <electrical_fc_system description="Switch for electrical flight control system">
+ <value>1</value>
+ <default>1</default>
+ </electrical_fc_system>
+ <common_installation_weight_factor description="Percentage of flight control system for common installation weight">
+ <value>0.25</value>
+ <default>0.25</default>
+ </common_installation_weight_factor>
+ <default_actuator description="Actuator description for automatic flight control architecture">
+ <power_source description="energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ <default>Hydraulic</default>
+ </type>
+ <source_ID description="ID of the energy source" Default="1">
+ <value>1</value>
+ <default>1</default>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <default>0.85</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in active operation (due to rudder deflections)">
+ <value>0.</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </default_actuator>
+ <ailerons>
+ <electric_flight_control_system_weight_factor description="Weight factor for electrical Flight Control system">
+ <value>0.25</value>
+ <default>0.5</default>
+ </electric_flight_control_system_weight_factor>
+ <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </default_actuator_architecture_switch>
+ <default_actuator_architecture description="Definition of the default actuator architecture">
+ <number_of_actuators_per_control_surface description="Number of actuators per control surface">
+ <value>2</value>
+ <unit></unit>
+ <default>2</default>
+ </number_of_actuators_per_control_surface>
+ <default_deflection_speed description="Deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </default_deflection_speed>
+ </default_actuator_architecture>
+ <manual_actuator_architecture description="Definition of the manual actuator architecture">
+ <number_of_control_surfaces description="Number of control surfaces to be initialized">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_control_surfaces>
+ <ailerons ID="0" description="Control surface parameters">
+ <side>right</side>
+ <deflection_speed description="Deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for Ailerons 2 actuators per control surface) (active/damping mode)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>0.85</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="1" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ <default></default>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>damping</value>
+ <default>damping</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>0.85</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </ailerons>
+ </manual_actuator_architecture>
+ </ailerons>
+ <rudders>
+ <electric_flight_control_system_weight_factor description="Weight factor for electrical Flight Control system">
+ <value>0.25</value>
+ <default>0.5</default>
+ </electric_flight_control_system_weight_factor>
+ <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </default_actuator_architecture_switch>
+ <default_actuator_architecture description="Definition of the default actuator architecture">
+ <number_of_actuators_per_control_surface description="Number of actuators per control surface">
+ <value>3</value>
+ <unit></unit>
+ <default>3</default>
+ </number_of_actuators_per_control_surface>
+ <default_deflection_speed description="Deflection speed">
+ <value>60</value>
+ <unit>deg/s</unit>
+ <default>60</default>
+ </default_deflection_speed>
+ </default_actuator_architecture>
+ <manual_actuator_architecture description="Definition of the manual actuator architecture">
+ <number_of_control_surfaces description="Number of control surfaces to be initialized">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_control_surfaces>
+ <rudder ID="0" description="Control surface parameters">
+ <deflection_speed description="deflection speed">
+ <value>60</value>
+ <unit>deg/s</unit>
+ <default>60</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for Rudder 3 actuators per control surface (all active))">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>3</value>
+ <unit>-</unit>
+ <default>3</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="1" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="2" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="3" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>damping</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>1.</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="4" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>damping</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>1.</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </rudder>
+ </manual_actuator_architecture>
+ </rudders>
+ <elevators>
+ <electric_flight_control_system_weight_factor description="Weight factor for electrical Flight Control system">
+ <value>0.25</value>
+ <unit></unit>
+ <default>0.5</default>
+ </electric_flight_control_system_weight_factor>
+ <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </default_actuator_architecture_switch>
+ <default_actuator_architecture description="Definition of the default actuator architecture">
+ <number_of_actuators_per_control_surface description="Number of actuators per control surface">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_actuators_per_control_surface>
+ <default_deflection_speed description="Deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </default_deflection_speed>
+ </default_actuator_architecture>
+ <manual_actuator_architecture description="Definition of the manual actuator architecture">
+ <number_of_control_surfaces description="Number of control surfaces to be initialized">
+ <value>2</value>
+ <default>1</default>
+ </number_of_control_surfaces>
+ <elevator ID="0" description="Control surface parameters">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for elevator 2 actuators per control surface (one active, one damping))">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="1" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>damping</value>
+ <default>damping</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </elevator>
+ <elevator ID="1" description="Control surface parameters">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for elevator 2 actuators per control surface (one active, one damping))">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="1" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>damping</value>
+ <default>damping</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </elevator>
+ </manual_actuator_architecture>
+ </elevators>
+ <spoilers>
+ <electric_flight_control_system_weight_factor description="Weight factor for electrical Flight Control system">
+ <value>0.25</value>
+ <unit></unit>
+ <default>0.5</default>
+ </electric_flight_control_system_weight_factor>
+ <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </default_actuator_architecture_switch>
+ <default_actuator_architecture description="Definition of the default actuator architecture">
+ <number_of_actuators_per_control_surface description="Number of actuators per control surface">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators_per_control_surface>
+ <default_deflection_speed description="Deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </default_deflection_speed>
+ </default_actuator_architecture>
+ <manual_actuator_architecture description="Definition of the manual actuator architecture">
+ <number_of_control_surfaces description="Number of control surfaces to be initialized">
+ <value>10</value>
+ <default>1</default>
+ </number_of_control_surfaces>
+ <spoiler ID="0" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="1" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="2" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="3" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="4" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="5" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="6" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="7" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="8" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ <spoiler ID="9" description="spoiler description">
+ <side>right</side>
+ <deflection_speed description="deflection speed">
+ <value>50</value>
+ <unit>deg/s</unit>
+ <default>50</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for spoiler 1 actuator per control surface)">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </spoiler>
+ </manual_actuator_architecture>
+ </spoilers>
+ <trimmable_horizontal_stabilizer>
+ <number_of_trimmable_horizontal_stabilizers description="Number of all trimmable horizontal stabilizers (thsa)">
+ <value>1</value>
+ <default>1</default>
+ </number_of_trimmable_horizontal_stabilizers>
+ <electric_flight_control_system_weight_factor description="Weight factor for electrical Flight Control system">
+ <value>0.5</value>
+ <unit></unit>
+ <default>0.5</default>
+ </electric_flight_control_system_weight_factor>
+ <default_actuator_architecture_switch description="Enables the default layout for the actuator architecture">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </default_actuator_architecture_switch>
+ <default_actuator_architecture description="Definition of the default actuator architecture">
+ <number_of_actuators_per_control_surface description="Number of actuators per control surface">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_actuators_per_control_surface>
+ <default_deflection_speed description="Deflection speed">
+ <value>0.5</value>
+ <unit>deg/s</unit>
+ <default>0.5</default>
+ </default_deflection_speed>
+ </default_actuator_architecture>
+ <manual_actuator_architecture description="Definition of the manual actuator architecture">
+ <number_of_control_surfaces description="Number of control surfaces to be initialized">
+ <value>2</value>
+ <default>1</default>
+ </number_of_control_surfaces>
+ <thsa ID="0" description="Control surface parameters">
+ <deflection_speed description="deflection speed">
+ <value>0.5</value>
+ <unit>deg/s</unit>
+ <default>0.5</default>
+ </deflection_speed>
+ <actuator_layout description="Actuator layouts (standard for THSA 2 actuators (both active))">
+ <number_of_actuators description="Number of actuator layouts">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_actuators>
+ <actuator ID="0" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ <actuator ID="1" description="Actuator description">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <efficiency description="Actuator efficiency in average operation">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>1.</default>
+ </efficiency>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </actuator>
+ </actuator_layout>
+ </thsa>
+ </manual_actuator_architecture>
+ </trimmable_horizontal_stabilizer>
+ <high_lift_system>
+ <trailing_edge>
+ <electric_flight_control_system_weight_factor description="Weight factor for electrical Flight Control system">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>2.0</default>
+ </electric_flight_control_system_weight_factor>
+ <number_of_devices description="Number of trailing edge systems">
+ <value>2</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_devices>
+ <trailing_edge_device ID="0">
+ <power_control_unit>
+ <number_of_power_control_unit_motors description="Number of PCU motors">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_power_control_unit_motors>
+ <power_control_unit_motor ID="0">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </active_power>
+ </power_control_unit_motor>
+ <power_control_unit_motor ID="1">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </active_power>
+ </power_control_unit_motor>
+ </power_control_unit>
+ </trailing_edge_device>
+ <trailing_edge_device ID="1">
+ <power_control_unit>
+ <number_of_power_control_unit_motors description="Number of PCU motors">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_power_control_unit_motors>
+ <power_control_unit_motor ID="0">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </active_power>
+ </power_control_unit_motor>
+ <power_control_unit_motor ID="1">
+ <power_source description="Energy source">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ </active_power>
+ </power_control_unit_motor>
+ </power_control_unit>
+ </trailing_edge_device>
+ </trailing_edge>
+ <leading_edge>
+ <electric_flight_control_system_weight_factor description="Weight factor for electrical Flight Control system">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>1.0</default>
+ </electric_flight_control_system_weight_factor>
+ <number_of_devices description="Number of front edge systems">
+ <value>0</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_devices>
+ <leading_edge_device ID="0">
+ <power_control_unit>
+ <number_of_power_control_unit_motors description="Number of PCU motors">
+ <value>2</value>
+ <unit>-</unit>
+ <default>2</default>
+ </number_of_power_control_unit_motors>
+ <power_control_unit_motor ID="0">
+ <power_source description="Energy source" default="-">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)" default="-">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <default>active</default>
+ </operation_mode>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </power_control_unit_motor>
+ <power_control_unit_motor ID="1">
+ <power_source description="Energy source" default="-">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)" default="-">
+ <value>Hydraulic</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ <operation_mode description="Activity of the actuator during normal operation (active, standby, damping)">
+ <value>active</value>
+ <unit></unit>
+ <default>active</default>
+ </operation_mode>
+ <standby_power description="Average basic power in standby operation (e.g. due to leakage)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </standby_power>
+ <active_power description="Average basic power in Active operation (due to rudder deflections)">
+ <value>0.0</value>
+ <unit>W</unit>
+ <default>0.0</default>
+ </active_power>
+ </power_control_unit_motor>
+ </power_control_unit>
+ </leading_edge_device>
+ </leading_edge>
+ <duration_high_lift_deployment description="Extension time of the high-lift system">
+ <value>22.0</value>
+ <unit>s</unit>
+ <default>22.0</default>
+ </duration_high_lift_deployment>
+ </high_lift_system>
+ </flight_controls>
+ <bleed_air>
+ <temperature_bleed_air description="Temperature of Bleed Air during extraction">
+ <value>200</value>
+ <unit>C</unit>
+ <default>200</default>
+ </temperature_bleed_air>
+ <efficiency_factor_bleed_air_system description="Efficiency of the Bleed Air system, e.g. leakage losses">
+ <value>0.95</value>
+ <unit>-</unit>
+ <default>0.95</default>
+ </efficiency_factor_bleed_air_system>
+ <specific_ducting_mass description="Specific weight of Bleed Air pipes">
+ <value>4.5</value>
+ <unit>kg/m</unit>
+ <default>4.5</default>
+ </specific_ducting_mass>
+ </bleed_air>
+ <hydraulic_system>
+ <pressure description="Nominal pressure of the hydraulic system">
+ <value>20684000</value>
+ <unit>Pa</unit>
+ <default>20684000</default>
+ </pressure>
+ <efficiency_factor_hydraulic_system description="Efficiency of the hydraulic system, e.g. leakage losses">
+ <value>0.95</value>
+ <unit>-</unit>
+ <default>0.95</default>
+ </efficiency_factor_hydraulic_system>
+ <rel_max_power description="Ratio of maximum permanent power and maximum required power of all pumps">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>1.0</default>
+ </rel_max_power>
+ <specific_ducting_mass description="Specific weight of hydraulic lines">
+ <value>2.5</value>
+ <unit>kg/m</unit>
+ <default>2.5</default>
+ </specific_ducting_mass>
+ <specific_fluid_mass description="Specific weight of hydraulic fluid">
+ <value>0.75</value>
+ <unit>kg/m</unit>
+ <default>0.75</default>
+ </specific_fluid_mass>
+ <specific_pump_mass description="Specific weight of hydraulic pumps">
+ <value>1250</value>
+ <unit>kg/W</unit>
+ <default>1250</default>
+ </specific_pump_mass>
+ <hydraulic_circuits description="Detailed description of the hydraulic circuits">
+ <number_of_circuits description="Number of hydraulic circuits">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_circuits>
+ <hydraulic_circuit ID="0" description="Hydraulic circuit description">
+ <compartment_reference_point description="Reference point of the Hydraulic Compartment (distributor seat, reservoir, etc.)">
+ <x description="X-Distance to nose in relation to fuselage length">
+ <value>0.4</value>
+ <unit>-</unit>
+ <default>0.4</default>
+ </x>
+ <y description="Y-Distance to symmetry line in relation to half span">
+ <value>0.0</value>
+ <unit>-</unit>
+ <default>0.0</default>
+ </y>
+ <z description="Z-distance to symmetry line in relation to fuselage height">
+ <value>0.0</value>
+ <unit>-</unit>
+ <default>0.0</default>
+ </z>
+ </compartment_reference_point>
+ <components description="Components within the circuit">
+ <pumps description="Pumps">
+ <number_of_pumps description="Number of pumps">
+ <value>2</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_pumps>
+ <pump ID="0" description="Pump description">
+ <name description="Name of the pump">
+ <value>EDP</value>
+ </name>
+ <type description="Type of pump (Currently 3 types: Electric, EngineDriven, RAT)">
+ <value>EngineDriven</value>
+ <default>EngineDriven</default>
+ </type>
+ <efficiency description="Pump efficiency">
+ <value>0.85</value>
+ <unit>-</unit>
+ <default>0.85</default>
+ </efficiency>
+ <operation_factor description="Percentage of total pump power in normal operation (value must be between">
+ <value>0.8</value>
+ <unit></unit>
+ <default>1</default>
+ </operation_factor>
+ <power_source description="Energy source for the pump">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Engine</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </pump>
+ <pump ID="1" description="Pump description">
+ <name description="Name of the pump">
+ <value>EMP</value>
+ </name>
+ <type description="Type of pump (Currently 3 types: Electric, EngineDriven, RAT)">
+ <value>Electric</value>
+ <default>EngineDriven</default>
+ </type>
+ <efficiency description="Pump efficiency">
+ <value>0.7</value>
+ <unit>-</unit>
+ <default>0.95</default>
+ </efficiency>
+ <operation_factor description="Percentage of total pump power in normal operation (value must be between 0 and 1. 0=off, 1=total)">
+ <value>0.2</value>
+ <unit>-</unit>
+ <default>1</default>
+ </operation_factor>
+ <power_source description="Energy source for the pump">
+ <type description="Type of energy source (Hydraulic, Electric, Engine, APU)">
+ <value>Electric</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </pump>
+ </pumps>
+ <not_specified description="Description of the remaining components in the hydraulic circuit (without lines... are calculated internally!)">
+ <mass_factor description="Mass fraction of remaining components in the hydraulic circuit">
+ <value>0.</value>
+ <unit>-</unit>
+ <default>0.</default>
+ </mass_factor>
+ </not_specified>
+ </components>
+ </hydraulic_circuit>
+ </hydraulic_circuits>
+ <power_transfer_units description="System description of the Power Transfer Units">
+ <number_of_power_transfer_units description="Number of PTUs">
+ <value>0</value>
+ <unit>-</unit>
+ <default>0</default>
+ </number_of_power_transfer_units>
+ <power_transfer_unit ID="0" description="System description of the PTU">
+ <power_transfer_unit_connection ID="0" description="1. Circuit to which the PTU is connected">
+ <value>-</value>
+ </power_transfer_unit_connection>
+ <power_transfer_unit_connection ID="1" description="2. Circuit to which the PTU is connected">
+ <value>-</value>
+ </power_transfer_unit_connection>
+ </power_transfer_unit>
+ </power_transfer_units>
+ </hydraulic_system>
+ <electric_system>
+ <efficiency_factor_electric_system description="Efficiency of the electrical system, e.g. resistance of the cables">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>1.0</default>
+ </efficiency_factor_electric_system>
+ <rel_max_power description="Ratio of maximum permanent power and maximum required power of all generators">
+ <value>1.0</value>
+ <unit>-</unit>
+ <default>1.0</default>
+ </rel_max_power>
+ <specific_cable_mass description="Specific weight of electrical wiring">
+ <value>6.5</value>
+ <unit>kg/m</unit>
+ <default>6.5</default>
+ </specific_cable_mass>
+ <electric_circuits description="Detailed description of the electrical circuits">
+ <number_of_circuits description="Number of electric circuits">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_circuits>
+ <electric_circuit ID="0" description="System description electrical circuit">
+ <components description="Components within the cycle">
+ <generators description="Generators">
+ <number_of_generators description="Number of generators">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </number_of_generators>
+ <generator ID="0" description="System description of the generator">
+ <name description="Name of generator">
+ <value>IDG1</value>
+ </name>
+ <type description="Type of generators">
+ <value>IDG</value>
+ </type>
+ <generator_efficiency description="Efficiency of the generator including accessory gear box">
+ <value>0.665</value>
+ <unit>-</unit>
+ <default>0.665</default>
+ </generator_efficiency>
+ <operation_factor description="Share of total power in normal operation (value must be between 0 and 1. 0=off, 1=total)">
+ <value>1</value>
+ <default>1</default>
+ </operation_factor>
+ <power_source description="Energy source of generator">
+ <type description="Type of energy source (hydraulic, electric, engine, APU)">
+ <value>Engine</value>
+ </type>
+ <source_ID description="ID of the energy source">
+ <value>1</value>
+ </source_ID>
+ </power_source>
+ </generator>
+ </generators>
+ <not_specified description="System description of the remaining components in the electrical circuit (without cable/plug... are calculated internally!)">
+ <mass_factor description="Mass fraction of the remaining components">
+ <value>0.</value>
+ <unit>-</unit>
+ <default>0.</default>
+ </mass_factor>
+ </not_specified>
+ </components>
+ </electric_circuit>
+ </electric_circuits>
+ </electric_system>
+ <propulsion_system>
+ <percentage_bleed_air description="Percentage of bleed air generated by the engine">
+ <value>1.00</value>
+ <unit>-</unit>
+ <default>1.00</default>
+ </percentage_bleed_air>
+ <percentage_electrical_power description="Percentage of electrical energy generated by the engine">
+ <value>1.00</value>
+ <unit>-</unit>
+ <default>1.00</default>
+ </percentage_electrical_power>
+ <percentage_hydraulic_power description="Percentage of hydraulic energy generated by the engine">
+ <value>1.00</value>
+ <unit>-</unit>
+ <default>1.00</default>
+ </percentage_hydraulic_power>
+ <efficiency_factor_bleed_air description="Efficiency of Bleed Air withdrawal">
+ <value>0.95</value>
+ <unit>-</unit>
+ <default>0.95</default>
+ </efficiency_factor_bleed_air>
+ </propulsion_system>
+ <auxiliary_power_unit>
+ <position_of_auxiliary_power_unit_in_fuselage_length description="Relative position of the APU in reference to the total fuselage length">
+ <value>0.95</value>
+ <unit>-</unit>
+ <default>0.95</default>
+ </position_of_auxiliary_power_unit_in_fuselage_length>
+ <percentage_bleed_air description="Percentage of Bleed Air generated by the APU">
+ <value>0.00</value>
+ <unit>-</unit>
+ <default>0.00</default>
+ </percentage_bleed_air>
+ <percentage_electrical_power description="Percentage of electrical energy generated by the APU">
+ <value>0.00</value>
+ <unit>-</unit>
+ <default>0.00</default>
+ </percentage_electrical_power>
+ <percentage_hydraulic_power description="Percentage of hydraulic energy generated by the APU">
+ <value>0.0</value>
+ <unit>-</unit>
+ <default>0.00</default>
+ </percentage_hydraulic_power>
+ <efficiency_factor_bleed_air description="Efficiency of Bleed Air withdrawal">
+ <value>0.90</value>
+ <unit>-</unit>
+ <default>0.90</default>
+ </efficiency_factor_bleed_air>
+ <installation_factor description="Installation factor for attached parts such as fire protection, noise protection, etc.">
+ <value>1.5</value>
+ <unit>-</unit>
+ <default>1.5</default>
+ </installation_factor>
+ <design_loads>
+ <percentage_bleed_air description="Percentage of Bleed Air for which the APU is designed">
+ <value>0.30</value>
+ <unit>-</unit>
+ <default>0.30</default>
+ </percentage_bleed_air>
+ <percentage_electrical_power description="Percentage of electrical energy for which the APU is designed">
+ <value>0.50</value>
+ <unit>-</unit>
+ <default>0.50</default>
+ </percentage_electrical_power>
+ <percentage_hydraulic_power description="Percentage of hydraulic energy for which the APU is designed">
+ <value>0.50</value>
+ <unit>-</unit>
+ <default>0.50</default>
+ </percentage_hydraulic_power>
+ </design_loads>
+ </auxiliary_power_unit>
+ <avionics description="Components grouped inside ATAXX">
+ <location_of_aviationics_bay description="0: Wing root, 1: Nose, 2: Behind cockpit">
+ <value>0</value>
+ <unit>-</unit>
+ <default>0</default>
+ </location_of_aviationics_bay>
+ </avionics>
+ <remaining_consumers>
+ <power description="Additional percentages of bleed, electric, and hydraulic power for ATA-XX">
+ <percentage_bleed_air description="Percentage of unrecorded performances">
+ <value>0.00</value>
+ <unit>-</unit>
+ <default>0.0</default>
+ </percentage_bleed_air>
+ <percentage_electric description="Percentage of unrecorded performances">
+ <value>0.104</value>
+ <unit>-</unit>
+ <default>0.104</default>
+ </percentage_electric>
+ <percentage_hydraulic description="Percentage of unrecorded performances">
+ <value>0.05</value>
+ <unit>-</unit>
+ <default>0.05</default>
+ </percentage_hydraulic>
+ </power>
+ <mass>
+ <scaling_factor description="Scaling of ATA-XX mass">
+ <value>1</value>
+ <unit>-</unit>
+ <default>1</default>
+ </scaling_factor>
+ <distribution description="Distribution of ATA-XX mass to single components">
+ <percentage_instrumentation_of_ATAXX description="Percentage of instrumentation in ATA-XX">
+ <value>0.08</value>
+ <unit>-</unit>
+ <default>0.08</default>
+ </percentage_instrumentation_of_ATAXX>
+ <percentage_auto_flight_of_ATAXX description="Percentage of AFS in ATA-XX">
+ <value>0.13</value>
+ <unit>-</unit>
+ <default>0.13</default>
+ </percentage_auto_flight_of_ATAXX>
+ <percentage_navigation_of_ATAXX description="Percentage of the navigation system in ATA-XX">
+ <value>0.53</value>
+ <unit>-</unit>
+ <default>0.53</default>
+ </percentage_navigation_of_ATAXX>
+ <percentage_communication_of_ATAXX description="Percentage of the communication system in ATA-XX">
+ <value>0.26</value>
+ <unit>-</unit>
+ <default>0.26</default>
+ </percentage_communication_of_ATAXX>
+ </distribution>
+ </mass>
+ </remaining_consumers>
+ </systems_constants>
+ </program_settings>
+</module_configuration_file>
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/xml_configs/template.xml b/UnicadoGUI/Backend/xml_configs/template.xml
new file mode 100644
index 0000000..6111745
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/template.xml
@@ -0,0 +1,5001 @@
+<aircraft_exchange_file>
+ <requirements_and_specifications description="Requirements and specifications">
+ <general description="General aircraft information">
+ <type description="Aircraft type">
+ <value>CeRAS</value>
+ </type>
+ <model description="Model - Version">
+ <value>SMR-2020</value>
+ </model>
+ </general>
+ <mission_files description="Name of xml files which are located in the missionData directory and contain the flight phase data" tool_level="0">
+ <design_mission_file description="Name of the design mission xml">
+ <value>design_mission.xml</value>
+ </design_mission_file>
+ <study_mission_file description="Name of the study mission xml">
+ <value>study_mission.xml</value>
+ </study_mission_file>
+ <requirements_mission_file description="Name of the requirements mission xml">
+ <value>requirements_mission.xml</value>
+ </requirements_mission_file>
+ </mission_files>
+ <design_specification description="Design specification">
+ <configuration description="Configuration information">
+ <configuration_type description="aircraft configuration: tube_and_wing / blended_wing_body">
+ <value>tube_and_wing</value>
+ </configuration_type>
+ <fuselage_definition description="Design description of the fuselage.">
+ <fuselage_type description="Fuselage type: single_aisle / weight_body">
+ <value>single_aisle</value>
+ </fuselage_type>
+ </fuselage_definition>
+ <wing_defintion description="Definitions for wing design">
+ <mounting description="wing mounting for tube_and_wing configuration (ignored at blended_wing_body) - low / mid / high">
+ <value>low</value>
+ </mounting>
+ </wing_defintion>
+ <empennage_definition description="Definitions for empennage design">
+ <empennage_type description="tube_and_wing configuration: conventional - blended_wing_body: vertical_tails">
+ <value>conventional</value>
+ </empennage_type>
+ </empennage_definition>
+ <undercarriage_definition description="Design description of the undercarriage.">
+ <main_gear_mounting description="Mounting position of the main landing gear: wing_mounted / fuselage_mounted.">
+ <value>wing_mounted</value>
+ </main_gear_mounting>
+ <undercarriage_retractability description="Switch to set retractability of landing gear: retractable / non_retractable.">
+ <value>retractable</value>
+ </undercarriage_retractability>
+ </undercarriage_definition>
+ <loads description="Loads information">
+ <design_load_factor description="design load factor n">
+ <maximum description="maximum design load factor n">
+ <value>2.5</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>4</upper_boundary>
+ </maximum>
+ <minimum description="maximum design load factor n">
+ <value>-1.0</value>
+ <unit>1</unit>
+ <lower_boundary>-2.0</lower_boundary>
+ <upper_boundary>0.0</upper_boundary>
+ </minimum>
+ <maneuver description="standard maneuver load factor for e.g. flare">
+ <value>1.1</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>2.0</upper_boundary>
+ </maneuver>
+ </design_load_factor>
+ </loads>
+ </configuration>
+ <transport_task>
+ <passenger_definition description="Define the masses of the passengers">
+ <total_number_passengers description="Design number of passengers">
+ <value>150</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </total_number_passengers>
+ <mass_per_passenger description="Design mass of a single passenger WITHOUT luggage">
+ <value>80</value>
+ <unit>kg</unit>
+ <lower_boundary>50</lower_boundary>
+ <upper_boundary>200</upper_boundary>
+ </mass_per_passenger>
+ <luggage_mass_per_passenger description="Design mass of a the luggage for a single passenger">
+ <value>17</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </luggage_mass_per_passenger>
+ </passenger_definition>
+ <passenger_class_definition>
+ <class_distribution description="Relative passenger distribution for the classes: President Class/First Class/Business Class/Premium Economy/Economy. Sum must be equal to 1!">
+ <value>0/0/0/0.1/0.9</value>
+ </class_distribution>
+ </passenger_class_definition>
+ <cargo_definition description="Definition of cargo which does not belong to passengers">
+ <additional_cargo_mass description="Mass of cargo which does not belong to passengers">
+ <value>500</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000</upper_boundary>
+ </additional_cargo_mass>
+ <cargo_density description="Density of cargo which does not belong to passengers">
+ <value>165</value>
+ <unit>kg/m^3</unit>
+ <lower_boundary>150</lower_boundary>
+ <upper_boundary>200</upper_boundary>
+ </cargo_density>
+ </cargo_definition>
+ </transport_task>
+ <energy_carriers description="Energy carriers information">
+ <energy_carrier ID="0" description="Energy type: kerosene / liquid_hydrogen / battery / saf (for multifuel engine create new ID)">
+ <value>0</value>
+ </energy_carrier>
+ </energy_carriers>
+ <propulsion description="Propulsion information">
+ <propulsor ID="0" description="Information for specific propulsor">
+ <powertrain description="Way the power is generated from the source: turbo, electric, fuel_cell">
+ <value>turbo</value>
+ </powertrain>
+ <type description="Type of main thrust generator: fan or prop">
+ <value>fan</value>
+ </type>
+ <position description="propulsor position (arrangement order acc to ID order)">
+ <parent_component description="position on component: wing, fuselage, empennage">
+ <value>wing</value>
+ </parent_component>
+ <x description="x-position (aircraft coordinate system): front or back">
+ <value>front</value>
+ </x>
+ <y description="y position (aircraft coordinate system): left or right">
+ <value>left</value>
+ </y>
+ <z description="z position (aircraft coordinate system): over, mid, under, in">
+ <value>in</value>
+ </z>
+ </position>
+ <energy_carrier_ID description="see energy carrier specification node">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </energy_carrier_ID>
+ <thrust_share description="Share of this thrust in relation to required aircraft thrust">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </thrust_share>
+ </propulsor>
+ </propulsion>
+ <systems description="Systems information">
+ <energy_provider description="source where energy is coming from per segment">
+ <ground description="source where energy is coming from in the ground mission segment">
+ <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <value>propulsor</value>
+ </powertrain>
+ <energy_carrier_ID description="see energy carrier specification node">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </energy_carrier_ID>
+ </ground>
+ <taxi description="source where energy is coming from in the taxi mission segment">
+ <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <value>propulsor</value>
+ </powertrain>
+ <energy_carrier_ID description="see energy carrier specification node">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </energy_carrier_ID>
+ </taxi>
+ <takeoff description="source where energy is coming from in the takeoff mission segment">
+ <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <value>propulsor</value>
+ </powertrain>
+ <energy_carrier_ID description="see energy carrier specification node">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </energy_carrier_ID>
+ </takeoff>
+ <climb description="source where energy is coming from in the climb mission segment">
+ <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <value>propulsor</value>
+ </powertrain>
+ <energy_carrier_ID description="see energy carrier specification node">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </energy_carrier_ID>
+ </climb>
+ <cruise description="source where energy is coming from in the cruise mission segment">
+ <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <value>propulsor</value>
+ </powertrain>
+ <energy_carrier_ID description="see energy carrier specification node">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </energy_carrier_ID>
+ </cruise>
+ <descent description="source where energy is coming from in the descent mission segment">
+ <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <value>propulsor</value>
+ </powertrain>
+ <energy_carrier_ID description="see energy carrier specification node">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </energy_carrier_ID>
+ </descent>
+ <landing description="source where energy is coming from in the landing mission segment">
+ <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+ <value>propulsor</value>
+ </powertrain>
+ <energy_carrier_ID description="see energy carrier specification node">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </energy_carrier_ID>
+ </landing>
+ </energy_provider>
+ </systems>
+ <skinning description="Skinning Information">
+ <material description="Material of skinning">
+ <value>aluminium2024</value>
+ </material>
+ <thickness description="Thickness of skinning">
+ <value>0.003</value>
+ <unit>m</unit>
+ <lower_boundary>0.0001</lower_boundary>
+ <upper_boundary>0.1</upper_boundary>
+ </thickness>
+ </skinning>
+ <technology>
+ <variable_camber description="Switch if variable camber is used">
+ <value>false</value>
+ </variable_camber>
+ </technology>
+ <tank_configuration description="Energy tanks information">
+ <tank ID="0" description="One Tank">
+ <energy_carrier_ID description="see energy carrier specification node">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </energy_carrier_ID>
+ <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
+ <value>0</value>
+ </location>
+ <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total">
+ <value>0</value>
+ </position>
+ </tank>
+ </tank_configuration>
+ </design_specification>
+ <requirements description="Aircraft design requirements">
+ <top_level_aircraft_requirements description="Top level aircraft requirements (TLAR)">
+ <maximum_structrual_payload_mass description="Maximum structual payload mass which can be carried by the aircraft (e.g. for short trips)">
+ <value>30000</value>
+ <unit>kg</unit>
+ <lower_boundary>100</lower_boundary>
+ <upper_boundary>150000</upper_boundary>
+ </maximum_structrual_payload_mass>
+ <takeoff_distance description="Design takeoff distance (Balanced Field Length) at Sea Level with maximum takeoff mass (MTOM) and (ISA + deltaISA)-Conditions">
+ <value>2122</value>
+ <unit>m</unit>
+ <lower_boundary>600</lower_boundary>
+ <upper_boundary>5000</upper_boundary>
+ </takeoff_distance>
+ <landing_field_length description="Needed runway length at Sea Level with maximum landiung mass (MLM) and (ISA + deltaISA)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6)">
+ <value>2387</value>
+ <unit>m</unit>
+ <lower_boundary>600</lower_boundary>
+ <upper_boundary>5000</upper_boundary>
+ </landing_field_length>
+ <icao_aerodrome_reference_code description="ICAO reference code - code_number 1-4 (field length) + code_letter A-F (wing span limits) + faa ADG code number I-VI (wing span limits + tail height limits) + Aircraft Approach Category letter A-D">
+ <value>3CIIIB</value>
+ </icao_aerodrome_reference_code>
+ <flight_envelope description="Maxima of design flight envelope">
+ <maximum_operating_mach_number description="Maximum operating mach number">
+ <value>0.85</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </maximum_operating_mach_number>
+ <maximum_operating_velocity description="Maximum operating speed (maximum dynamic pressure)">
+ <value>180</value>
+ <unit>m/s</unit>
+ <lower_boundary>50</lower_boundary>
+ <upper_boundary>250</upper_boundary>
+ </maximum_operating_velocity>
+ <maximum_approach_speed description="Maximum allowed approach speed.">
+ <value>71</value>
+ <unit>m/s</unit>
+ <lower_boundary>50</lower_boundary>
+ <upper_boundary>90</upper_boundary>
+ </maximum_approach_speed>
+ <maximum_operating_altitude description="Maximum operating altitude">
+ <value>12500</value>
+ <unit>m</unit>
+ <lower_boundary>4500</lower_boundary>
+ <upper_boundary>20000</upper_boundary>
+ </maximum_operating_altitude>
+ <maximum_one_engine_operating_altitude description="Maximum operating altitude with one engine inoperative">
+ <value>4500</value>
+ <unit>m</unit>
+ <lower_boundary>1500</lower_boundary>
+ <upper_boundary>12000</upper_boundary>
+ </maximum_one_engine_operating_altitude>
+ </flight_envelope>
+ <pavement_classification_number description="Runway pavment classification number (PCN) - limits the maximum allowed aircraft classification number of undercarriage.">
+ <value>55</value>
+ <unit>1</unit>
+ <lower_boundary>5</lower_boundary>
+ <upper_boundary>120</upper_boundary>
+ </pavement_classification_number>
+ <design_mission description="Requirements regarding the design mission">
+ <delta_ISA description="Temperature offset to the International Standard Atmosphere (ISA)">
+ <value>0</value>
+ <unit>K</unit>
+ <lower_boundary>100</lower_boundary>
+ <upper_boundary>-288.15</upper_boundary>
+ </delta_ISA>
+ <range description="Target range for the specified mission">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>20000000</upper_boundary>
+ </range>
+ <initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise.">
+ <value>0.78</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </initial_cruise_mach_number>
+ <initial_cruise_altitude description="Initial cruise altitude (ICA) at top of descent. May be altered during cruise.">
+ <value>11000</value>
+ <unit>m</unit>
+ <lower_boundary>1000</lower_boundary>
+ <upper_boundary>20000</upper_boundary>
+ </initial_cruise_altitude>
+ <climb_speed_schedule description="Climb speed for different altitudes">
+ <climb_speed_below_FL100 description="Calibrated airspeed in climb below FL100 (FL100 = 3048 m)">
+ <value>50</value>
+ <unit>m/s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>250</upper_boundary>
+ </climb_speed_below_FL100>
+ <climb_speed_above_FL100 description="Calibrated airspeed in climb above FL100 (FL100 = 3048 m)">
+ <value>100</value>
+ <unit>m/s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>250</upper_boundary>
+ </climb_speed_above_FL100>
+ <delta_mach_climb_cruise description="Difference between crossover altitude Mach number and cruise Mach number">
+ <value>-0.02</value>
+ <unit>1</unit>
+ <lower_boundary>-0.3</lower_boundary>
+ <upper_boundary>0.01</upper_boundary>
+ </delta_mach_climb_cruise>
+ </climb_speed_schedule>
+ <descent_speed_schedule description="Descent speed for different altitudes">
+ <descent_speed_below_FL100 description="Calibrated airspeed in descent below FL100 (FL100 = 3048 m)">
+ <value>50</value>
+ <unit>m/s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>250</upper_boundary>
+ </descent_speed_below_FL100>
+ <descent_speed_above_FL100 description="Calibrated airspeed in descent above FL100 (FL100 = 3048 m)">
+ <value>100</value>
+ <unit>m/s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>250</upper_boundary>
+ </descent_speed_above_FL100>
+ </descent_speed_schedule>
+ <time_to_climb description="Time the aircraft takes to climb to cruise altitude">
+ <value>2100</value>
+ <unit>s</unit>
+ <lower_boundary>600</lower_boundary>
+ <upper_boundary>3600</upper_boundary>
+ </time_to_climb>
+ <fuel_planning description="Fuel planning according to the Joint Aviation Requirements (JAR) or the Federal Aviation Regulations (FAR)">
+ <fuel_estimation_selector description="'mode_0': Fuel planning according to JAR, 'mode_1': Domestic fuel planning according to FAR, 'mode_2': Flag or supplemental fuel planning according to FAR">
+ <value>mode_0</value>
+ </fuel_estimation_selector>
+ </fuel_planning>
+ </design_mission>
+ <study_mission description="Requirements regarding the study mission">
+ <delta_ISA description="Temperature offset to the International Standard Atmosphere (ISA)">
+ <value>0</value>
+ <unit>K</unit>
+ <lower_boundary>100</lower_boundary>
+ <upper_boundary>-288.15</upper_boundary>
+ </delta_ISA>
+ <range description="Target range for the specified mission">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>20000000</upper_boundary>
+ </range>
+ <initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise.">
+ <value>0.78</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </initial_cruise_mach_number>
+ <initial_cruise_altitude description="Initial cruise altitude at top of descent. May be altered during cruise.">
+ <value>11000</value>
+ <unit>m</unit>
+ <lower_boundary>1000</lower_boundary>
+ <upper_boundary>20000</upper_boundary>
+ </initial_cruise_altitude>
+ <climb_speed_schedule description="Climb speed for different altitudes">
+ <climb_speed_below_FL100 description="Calibrated airspeed in climb below FL100 (FL100 = 3048 m)">
+ <value>50</value>
+ <unit>m/s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>250</upper_boundary>
+ </climb_speed_below_FL100>
+ <climb_speed_above_FL100 description="Calibrated airspeed in climb above FL100 (FL100 = 3048 m)">
+ <value>100</value>
+ <unit>m/s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>250</upper_boundary>
+ </climb_speed_above_FL100>
+ <delta_mach_climb_cruise description="Difference between crossover altitude Mach number and cruise Mach number">
+ <value>-0.02</value>
+ <unit>1</unit>
+ <lower_boundary>-0.3</lower_boundary>
+ <upper_boundary>0.01</upper_boundary>
+ </delta_mach_climb_cruise>
+ </climb_speed_schedule>
+ <descent_speed_schedule description="Descent speed for different altitudes">
+ <descent_speed_below_FL100 description="Calibrated airspeed in descent below FL100 (FL100 = 3048 m)">
+ <value>50</value>
+ <unit>m/s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>250</upper_boundary>
+ </descent_speed_below_FL100>
+ <descent_speed_above_FL100 description="Calibrated airspeed in descent above FL100 (FL100 = 3048 m)">
+ <value>100</value>
+ <unit>m/s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>250</upper_boundary>
+ </descent_speed_above_FL100>
+ </descent_speed_schedule>
+ <fuel_planning description="Fuel planning according to the Joint Aviation Requirements (JAR) or the Federal Aviation Regulations (FAR)">
+ <fuel_estimation_selector description="'mode_0': Fuel planning according to JAR, 'mode_1': Domestic fuel planning according to FAR, 'mode_2': Flag or supplemental fuel planning according to FAR">
+ <value>mode_0</value>
+ </fuel_estimation_selector>
+ </fuel_planning>
+ <payload_fractions description="Set the fraction of different design payload values for the study mission">
+ <cargo_fraction description="Fraction of the design cargo mass which is used for the study mission">
+ <value>0.75</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </cargo_fraction>
+ <passenger_mass_fraction description="Fraction of the design passenger mass which is used for the study mission">
+ <value>0.75</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </passenger_mass_fraction>
+ </payload_fractions>
+ </study_mission>
+ </top_level_aircraft_requirements>
+ <additional_requirements description="Additional requirements"></additional_requirements>
+ </requirements>
+ <assessment_scenario description="Scenario for ecological and economical assessment">
+ <flights_per_year description="Number of flights per year">
+ <value>2227</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>4000</upper_boundary>
+ </flights_per_year>
+ </assessment_scenario>
+ </requirements_and_specifications>
+ <sizing_point>
+ <wing_loading description="Maximum takeoff mass (MTOM) divided by wing area (Sref)" tool_level="1">
+ <value>0</value>
+ <unit>kg/m^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </wing_loading>
+ <thrust_to_weight description="Total thrust (kN) divided by maximum aircraft weight (kN)" tool_level="1">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </thrust_to_weight>
+ </sizing_point>
+ <component_design>
+ <global_reference_point>
+ <reference_component description="Gobal reference point of aircraft geometry">
+ <value></value>
+ </reference_component>
+ <x description="X coordinate of the global reference point">
+ <value></value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="Y coordinate of the global reference point">
+ <value></value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="Z coordinate of the global reference point">
+ <value></value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </global_reference_point>
+ <wing description="wing component" tool_level="0">
+ <position description="position of wing (most forward position of part composition at y = 0)">
+ <x description="x position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </position>
+ <mass_properties description="mass_properties of component wing">
+ <mass description="component mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="component inertia refered to center of gravity">
+ <j_xx description="inertia component in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia component in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia component in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia component in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia component in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia component in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia component in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia component in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia component in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="component center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>17.1682343</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <specific>
+ <geometry>
+ <aerodynamic_surface ID="0" description="aerodynamic surface">
+ <name description="name of aerodynamic surface">
+ <value>main_wing</value>
+ </name>
+ <position description="reference position in global coordinates">
+ <x description="x position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </position>
+ <parameters description="aerodynamic surface parameters">
+ <direction description="unit vector according to global coordinate system for direction applied at position">
+ <x description="x direction of unit vector">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </x>
+ <y description="y direction of unit vector">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </y>
+ <z description="z direction of unit vector">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </z>
+ </direction>
+ <symmetric description="symmetric to x-z plane (global) aerodynamic surface">
+ <value>true</value>
+ </symmetric>
+ <sections description="sections">
+ <section ID="0" description="section">
+ <chord_origin description="origin of chord (local)">
+ <x description="x position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </chord_origin>
+ <chord_length description="length of chord">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </chord_length>
+ <geometric_twist description="geometric twist at leading edge">
+ <value>0.0</value>
+ <unit>rad</unit>
+ <lower_boundary>-180</lower_boundary>
+ <upper_boundary>180</upper_boundary>
+ </geometric_twist>
+ <scale_thickness description="scale the thickness defined by the profile with this factor">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </scale_thickness>
+ <profile description="profile (data normalized on chord)">
+ <name>
+ <value>naca0012</value>
+ </name>
+ </profile>
+ </section>
+ </sections>
+ <spars description="spars">
+ <spar ID="0" description="front spar">
+ <position description="chord relative position of control device">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </spar>
+ <spar ID="1" description="rear spar">
+ <position description="chord relative position of control device">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </spar>
+ </spars>
+ <control_devices description="control devices">
+ <control_device ID="0" description="control device">
+ <type>
+ <value>aileron</value>
+ </type>
+ <deflection description="maximum positive and negative deflection of control device">
+ <full_negative_deflection description="full negative deflection">
+ <value>-25.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>25.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ <position description="chord relative position of control device">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </control_device>
+ </control_devices>
+ </parameters>
+ <mass_properties description="mass_properties of aerodynamic surface">
+ <mass description="component mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="component inertia refered to center of gravity">
+ <j_xx description="inertia component in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia component in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia component in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia component in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia component in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia component in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia component in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia component in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia component in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="component center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </aerodynamic_surface>
+ </geometry>
+ </specific>
+ </wing>
+ <fuselage description="Geometric description of the aircraft fuselages" tool_level="0">
+ <position description="Position of the fuselages with regard to the global reference point.">
+ <x description="Distance in x direction with regard to the global reference point. (fuselage nose point)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the global reference point. (fuselage nose point)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>0</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the global reference point. (distance to fuselage center line)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </position>
+ <mass_properties description="Mass properties of the fuselages.">
+ <mass description="Mass of the total fuselages.">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia of the total fuselages with regard to the total center of gravity.">
+ <j_xx description="Inertia of the total fuselages in x.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia of the total fuselages in y.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia of the total fuselages in z.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="Inertia of the total fuselages in xy.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="Inertia of the total fuselages in xz.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="Inertia of the total fuselages in yx.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="Inertia of the total fuselages in yz.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="Inertia of the total fuselages in zx.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="Inertia of the total fuselages in zy.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Center of gravity of the total fuselages.">
+ <x description="Center of gravity in x-direction with regard to the global reference point. (total fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point. (total fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point. (total fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <specific>
+ <geometry>
+ <fuselage ID="0" description="Geometrical description of one entire fuselage.">
+ <name description="Name of the fuselage.">
+ <value>center_fuselage</value>
+ </name>
+ <position description="Position of one entire fuselage with regard to the global reference point.">
+ <x description="Distance in x direction with regard to the global reference point. (fuselage nose point)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the global reference point. (fuselage nose point)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the global reference point. (distance to fuselage center line)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </position>
+ <direction description="unit vector according to global coordinate system for direction applied at position">
+ <x description="Distance in x direction with regard to the global reference point. (fuselage nose point)">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the global reference point. (fuselage nose point)">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the global reference point. (distance to fuselage center line)">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </z>
+ </direction>
+ <mass_properties description="Mass properties of one entire fuselage.">
+ <mass description="Mass of one entire fuslege.">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ <inertia description="Inertia of one entire fuselage with regard to his center of gravity.">
+ <j_xx description="Inertia of one entire fuselage in x.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia of one entire fuselage in y.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia of one entire fuselage in z.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="Inertia of one entire fuselage in xy.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="Inertia of one entire fuselage in xz.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="Inertia of one entire fuselage in yx.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="Inertia of one entire fuselage in yz.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="Inertia of one entire fuselage in zx.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="Inertia of one entire fuselage in zy.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Center of gravity of one entire fuselage.">
+ <x description="Center of gravity in x-direction with regard to the global reference point. (entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point. (entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point. (entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <sections description="Geometrical description of the fuselage sections of one entire fuselage">
+ <section ID="0" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_1</value>
+ </name>
+ <section_shape dedication="Contains a String with path to *.dat file or the key word 'elipse'">
+ <value>geometryData/fuselage/section_0.dat</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <x description="Distance in x direction with regard to the global reference point. (cgal convention local: x ist die breite/2 in y!)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the global reference point. (cgal convention local: y ist die höhe/2 in z!)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the global reference point. (cgal convention local: z ist die position in x!)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </upper_height>
+ <lower_height description="Height of the lower half of the fuselage section.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ </sections>
+ <fuselage_accommodation>
+ <position description="Position of the payload tubes with regard to the global reference point.">
+ <x description="Distance in x direction with regard to the global reference point. (center payload tube starting point)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the global reference point. (center payload tube starting point)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>0</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the global reference point. (distance to fuselage center line)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </position>
+ <mass_properties description="Mass properties of the payload tubes of one entire fuselage.">
+ <mass description="Mass of the payload tubes of one entire fuslege.">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ <center_of_gravity description="Center of gravity of the payload tubes of one entire fuselage.">
+ <x description="Center of gravity in x-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <payload_tube ID="0" description="Geometrical description of one payload tube of the fuselage.">
+ <mass_properties>
+ <mass description="Mass of the payload tubes of one entire fuslege.">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ <center_of_gravity description="Center of gravity of the payload tubes of one entire fuselage.">
+ <x description="Center of gravity in x-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <operator_items>
+ <mass_properties>
+ <mass description="Mass of the payload tubes of one entire fuslege.">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ <center_of_gravity description="Center of gravity of the payload tubes of one entire fuselage.">
+ <x description="Center of gravity in x-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </operator_items>
+ <furnishing_and_equipment>
+ <mass_properties>
+ <mass description="Mass of the payload tubes of one entire fuslege.">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ <center_of_gravity description="Center of gravity of the payload tubes of one entire fuselage.">
+ <x description="Center of gravity in x-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </furnishing_and_equipment>
+ <name description="Name of the payload tube.">
+ <value>center_payload_tube</value>
+ </name>
+ <payload_tube_reference_points description="Payload tube center reference points in x, y and z-direction refered to fuselage nose point.">
+ <front_reference_points description="Reference points in the front of payload tube.">
+ <x description="Payload tube reference point in x-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="Payload tube reference point in y-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="Payload tube reference point in z-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ <upper_z description="Upper payload tube reference point in z-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </upper_z>
+ <lower_z description="Lower payload tube reference point in z-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </lower_z>
+ </front_reference_points>
+ <aft_reference_points description="Reference points in the aft of payload tube.">
+ <x description="Payload tube reference point in x-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="Payload tube reference point in y-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="Payload tube reference point in z-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ <upper_z description="Upper payload tube reference point in z-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </upper_z>
+ <lower_z description="Lower payload tube reference point in z-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </lower_z>
+ </aft_reference_points>
+ </payload_tube_reference_points>
+ <payload_tube_wall_reference_points description="Payload tube wall reference points in x, y and z-direction refered to fuselage nose point.">
+ <front_reference_points description="Wall reference points in the front of payload tube.">
+ <x description="Wall reference point in x-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <left_y description="Left wall reference point in y-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </left_y>
+ <right_y description="Right wall reference point in y-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </right_y>
+ <z description="Wall reference point in z-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </front_reference_points>
+ <aft_reference_points description="Wall reference points in the aft of payload tube.">
+ <x description="Wall reference point in x-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <left_y description="Left wall reference point in y-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </left_y>
+ <right_y description="Right wall reference point in y-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </right_y>
+ <z description="Wall reference point in z-direction">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </aft_reference_points>
+ </payload_tube_wall_reference_points>
+ <payload_tube_structural_wall_thickness description="Structural wall thickness of the paylaod tube.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </payload_tube_structural_wall_thickness>
+ <payload_tube_water_volume description="Total water volume of one entire paylaod tube.">
+ <value>0</value>
+ <unit>m^3</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>infr</upper_boundary>
+ </payload_tube_water_volume>
+ <payload_deck ID="0" description="Geometrical description of the payload decks in one payload tube.">
+ <name description="Name of the payload deck.">
+ <value>passenger_deck</value>
+ </name>
+ <position description="Position of the payload deck with regard to the global reference point.">
+ <x description="Distance in x direction with regard to the global reference point. (payload deck starting point)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the global reference point. (payload deck starting point)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>0</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the global reference point. (distance to fuselage center line)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </position>
+ <mass_properties description="Mass properties of the payload deck of one entire payload tube.">
+ <mass description="Mass of the payload deck of one entire paylaod tube.">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ <center_of_gravity description="Center of gravity of the payload tubes of one entire fuselage.">
+ <x description="Center of gravity in x-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point. (all payload tubes of one entire fuselage)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <payload_tube_structural_floor_thickness description="Structural floor thickness of current paylaod deck.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </payload_tube_structural_floor_thickness>
+ <payload_deck_area description="Total floor area of the paylaod deck.">
+ <value>0</value>
+ <unit>m^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000</upper_boundary>
+ </payload_deck_area>
+ <payload_deck_water_volume description="Total water volume of the paylaod deck.">
+ <value>0</value>
+ <unit>m^3</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000</upper_boundary>
+ </payload_deck_water_volume>
+ <payload_deck_length description="Total length of the paylaod deck.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </payload_deck_length>
+ <payload_deck_height description="Maximum standing height of the paylaod deck.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>3</upper_boundary>
+ </payload_deck_height>
+ <payload_deck_top_width description="Width on the top of the paylaod deck.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </payload_deck_top_width>
+ <payload_deck_bottom_width description="Width on the bottom of the paylaod deck.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </payload_deck_bottom_width>
+ <payload_deck_required_galley_power description="Required power of the payload deck.">
+ <value>0</value>
+ <unit>W</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </payload_deck_required_galley_power>
+ <payload_compartment ID="0" description="Geometrical description of the payload compartment of one payload deck.">
+ <name description="Name of the payload compartment of the payload deck.">
+ <value>front_compartment</value>
+ </name>
+ <position description="Position of the payload compartment with regard to the global reference point.">
+ <x description="Distance in x direction with regard to the global reference point. (payload compartment starting point)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the global reference point. (payload compartment starting point)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the global reference point. (distance compartment fuselage center line)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </position>
+ <payload_compartment_area description="Total floor area of the payload compartment.">
+ <value>0</value>
+ <unit>m^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000</upper_boundary>
+ </payload_compartment_area>
+ <payload_compartment_water_volume description="Total water volume of the paylaod compartment.">
+ <value>0</value>
+ <unit>m^3</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000</upper_boundary>
+ </payload_compartment_water_volume>
+ <payload_compartment_length description="Total length of the paylaod compartment.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </payload_compartment_length>
+ </payload_compartment>
+ </payload_deck>
+ </payload_tube>
+ </fuselage_accommodation>
+ </fuselage>
+ </geometry>
+ </specific>
+ </fuselage>
+ <tank description="Description of aircraft tanks." tool_level="0">
+ <position description="Position of the tanks with regard to the global reference point.">
+ <x description="Distance between the foremost tank end and the global reference point in x-direction.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the foremost tank end and the global reference point in y-direction.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-40</lower_boundary>
+ <upper_boundary>40</upper_boundary>
+ </y>
+ <z description="Distance between the foremost tank end and the global reference point in z-direction.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </position>
+ <mass_properties description="Mass properties of all tanks.">
+ <mass description="Total tank mass.">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ <inertia description="Inertia of all tanks with regard to the total center of gravity.">
+ <j_xx description="Inertia of all tanks in x.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia of all tanks in y.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia of all tanks in z.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="Inertia of all tanks in xy.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="Inertia of all tanks in xz.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="Inertia of all tanks in yx.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="Inertia of all tanks in yz.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="Inertia of all tanks in zx.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="Inertia of all tanks in zy.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Center of gravity of all tanks.">
+ <x description="Center of gravity in x-direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-40</lower_boundary>
+ <upper_boundary>40</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <specific>
+ <tank ID="0" description="Description of one tank.">
+ <name description="Designator of the tank (right/left hand inner/outer wing tank, center tank, trim tank, cylindrical/conical tail cone tank, ...).">
+ <value>right hand inner wing tank</value>
+ </name>
+ <position description="Position of one tank with regard to the global reference point.">
+ <x description="Distance between the foremost tank end of one tank and the global reference point in x-direction.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the foremost tank end of one tank and the global reference point in y-direction.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-40</lower_boundary>
+ <upper_boundary>40</upper_boundary>
+ </y>
+ <z description="Distance between the foremost tank end of one tank and the global reference point in z-direction.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </position>
+ <mass_properties description="Mass properties of one tank.">
+ <mass description="Total dry mass of one tank.">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ <inertia description="Inertia of one tank with regard to its center of gravity.">
+ <j_xx description="Inertia of one tank in x.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia of one tank in y.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia of one tank in z.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="Inertia of one tank in xy.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="Inertia of one tank in xz.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="Inertia of one tank in yx.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="Inertia of one tank in yz.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="Inertia of one tank in zx.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="Inertia of one tank in zy.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Center of gravity of one tank.">
+ <x description="Center of gravity in x-direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-40</lower_boundary>
+ <upper_boundary>40</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <volume description="Total usable volume of one tank.">
+ <value>0</value>
+ <unit>m^3</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </volume>
+ <geometry description="Geometrical description of one tank.">
+ <cross_section ID="0" description="Geometrical description of one tank cross section.">
+ <name description="Designator of tank cross section.">
+ <value>first cross section</value>
+ </name>
+ <position description="Position of tank cross section with regard to the global reference point.">
+ <x description="Distance between the tank cross section and the global reference point in x-direction.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the tank cross section and the global reference point in y-direction.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-40</lower_boundary>
+ <upper_boundary>40</upper_boundary>
+ </y>
+ <z description="Distance between the tank cross section and the global reference point in z-direction.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </position>
+ <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+ <value>rectangular</value>
+ </shape>
+ <height description="Height of the cross section.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ <length description="Length of the cross section (if length > 0: curved cross section, e.g., dashed tank endcap).">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </length>
+ </cross_section>
+ </geometry>
+ </tank>
+ </specific>
+ </tank>
+ <empennage description="empennage component" tool_level="0">
+ <position description="position of empennage (most forward position of part composition)">
+ <x description="x position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </position>
+ <mass_properties description="mass_properties of component empennage">
+ <mass description="component mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="component inertia refered to center of gravity">
+ <j_xx description="inertia component in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia component in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia component in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia component in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia component in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia component in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia component in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia component in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia component in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="component center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <specific>
+ <geometry>
+ <aerodynamic_surface ID="0" description="aerodynamic surface">
+ <name description="name of aerodynamic surface">
+ <value>fin</value>
+ </name>
+ <position description="reference position in global coordinates">
+ <x description="x position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </position>
+ <parameters description="aerodynamic surface parameters">
+ <direction description="unit vector according to global coordinate system for direction applied at position">
+ <x description="x direction of unit vector">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </x>
+ <y description="y direction of unit vector">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </y>
+ <z description="z direction of unit vector">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </z>
+ </direction>
+ <symmetric description="symmetric to x-z plane (global) aerodynamic surface">
+ <value>true</value>
+ </symmetric>
+ <sections description="sections">
+ <section ID="0" description="section">
+ <chord_origin description="origin of chord (local)">
+ <x description="x position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z position">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </chord_origin>
+ <chord_length description="length of chord">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </chord_length>
+ <geometric_twist description="geometric twist at leading edge">
+ <value>0.0</value>
+ <unit>rad</unit>
+ <lower_boundary>-180</lower_boundary>
+ <upper_boundary>180</upper_boundary>
+ </geometric_twist>
+ <profile description="profile (data normalized on chord)">
+ <name>
+ <value>naca0012</value>
+ </name>
+ </profile>
+ </section>
+ </sections>
+ <spars description="spars">
+ <spar ID="0" description="front spar">
+ <position description="chord relative position of control device">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </spar>
+ <spar ID="1" description="rear spar">
+ <position description="chord relative position of control device">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </spar>
+ </spars>
+ <control_devices description="control devices">
+ <control_device ID="0" description="control device">
+ <type>
+ <value>aileron</value>
+ </type>
+ <deflection description="maximum positive and negative deflection of control device">
+ <full_negative_deflection description="full negative deflection">
+ <value>-25.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>25.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ <position description="chord relative position of control device">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </control_device>
+ </control_devices>
+ </parameters>
+ <mass_properties description="mass_properties of aerodynamic surface">
+ <mass description="component mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="component inertia refered to center of gravity">
+ <j_xx description="inertia component in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia component in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia component in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia component in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia component in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia component in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia component in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia component in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia component in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="component center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </aerodynamic_surface>
+ </geometry>
+ </specific>
+ </empennage>
+ <landing_gear description="Geometric description of the aircraft undercarriage." tool_level="0">
+ <position description="Position of the total undercarriage arrangment with regard to the global reference point.">
+ <x description="Distance in x direction with regard to the global reference point. (total undercarriage arrangment)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the global reference point. (total undercarriage arrangment)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>0</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the global reference point. (total undercarriage arrangment)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>0</upper_boundary>
+ </z>
+ </position>
+ <mass_properties description="Mass properties of the total undercarriage arrangment.">
+ <mass description="Mass of the total undercarriage arrangment.">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia of the total undercarriage arrangment with regard to the total center of gravity.">
+ <j_xx description="Inertia of the total undercarriage arrangment in x.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia of the total undercarriage arrangment in y.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia of the total undercarriage arrangment in z.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="Inertia of the total undercarriage arrangment in xy.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="Inertia of the total undercarriage arrangment in xz.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="Inertia of the total undercarriage arrangment in yx.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="Inertia of the total undercarriage arrangment in yz.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="Inertia of the total undercarriage arrangment in zx.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="Inertia of the total undercarriage arrangment in zy.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Center of gravity of the total undercarriage arrangment.">
+ <x description="Center of gravity in x-direction with regard to the global reference point. (total undercarriage arrangment)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point. (total undercarriage arrangment)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>0</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point. (total undercarriage arrangment)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>0</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <specific>
+ <aircraft_classification_number description="Aircraft classification number for the total undercarriage arrangment.">
+ <value>return_string</value>
+ </aircraft_classification_number>
+ <aircraft_classification_rating description="Aircraft classification rating for the total undercarriage arrangment.">
+ <value>return_string</value>
+ </aircraft_classification_rating>
+ <geometry>
+ <landing_gear_assembly ID="0" description="Geometrical description of one entire landing gear leg.">
+ <name description="Name of the landing gear leg.">
+ <value>nose_gear</value>
+ </name>
+ <position description="Position of one entire landing gear leg with regard to the global reference point.">
+ <x description="Distance in x direction with regard to the global reference point. (center line of the landing gear leg)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the global reference point. (center line of the landing gear leg)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-15</lower_boundary>
+ <upper_boundary>15</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the global reference point. (z coordinate refers to the mounting point of the landing gear leg.)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>0</upper_boundary>
+ </z>
+ </position>
+ <mass_properties description="Mass properties of one entire landing gear leg.">
+ <mass description="Mass of one entire landing gear leg.">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10000</upper_boundary>
+ </mass>
+ <inertia description="Inertia of one entire landing gear leg with regard to his center of gravity.">
+ <j_xx description="Inertia of one entire landing gear leg in x.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia of one entire landing gear leg in y.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia of one entire landing gear leg in z.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="Inertia of one entire landing gear leg xy.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="Inertia of one entire landing gear leg in xz.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="Inertia of one entire landing gear leg in yx.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="Inertia of one entire landing gear leg in yz.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="Inertia of one entire landing gear leg in zx.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="Inertia of one entire landing gear leg in zy.">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Center of gravity of one entire landing gear leg.">
+ <x description="Center of gravity in x-direction with regard to the global reference point. (entire landing gear leg)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point. (entire landing gear leg)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>0</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point. (entire landing gear leg)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>0</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <assambly_components>
+ <strut_diameter description="Diameter of the landing gear strut.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </strut_diameter>
+ <strut_length description="Length of the landing gear strut.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </strut_length>
+ <wheel_group_position description="Position of wheel group of one entire landing gear leg.">
+ <x description="Distance in x direction with regard to the global reference point (center line of the landing gear leg)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the global reference point (center line of the landing gear leg)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-15</lower_boundary>
+ <upper_boundary>15</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the global reference point (z coordinate refers to the end point of the landing gear leg.)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-20</lower_boundary>
+ <upper_boundary>0</upper_boundary>
+ </z>
+ </wheel_group_position>
+ <tire_description ID="0" description="Description of one tire of the wheel group">
+ <position description="Position of one tire of current landing gear strut.">
+ <x description="Distance in x direction with regard to the global reference point. (center line of the landing gear leg)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the global reference point. (center line of the landing gear leg)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-15</lower_boundary>
+ <upper_boundary>15</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the global reference point. (z coordinate refers to the mounting point of the landing gear leg.)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>0</upper_boundary>
+ </z>
+ </position>
+ <tire_diameter description="Diameter of the wheel group tires.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>2</upper_boundary>
+ </tire_diameter>
+ <tire_width description="Width of the wheel group tires.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </tire_width>
+ <tire_rated_load>
+ <value>0</value>
+ <unit>N</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000000</upper_boundary>
+ </tire_rated_load>
+ <tire_pressure description="Tire pressure of the wheel group tires.">
+ <value>0</value>
+ <unit>Pa</unit>
+ <lower_boundary>1000000</lower_boundary>
+ <upper_boundary>2000000</upper_boundary>
+ </tire_pressure>
+ <maximum_tire_speed description="Maximum permissible tire speed of the wheel group tires.">
+ <value>0</value>
+ <unit>m/s</unit>
+ <lower_boundary>50</lower_boundary>
+ <upper_boundary>125</upper_boundary>
+ </maximum_tire_speed>
+ </tire_description>
+ </assambly_components>
+ </landing_gear_assembly>
+ </geometry>
+ </specific>
+ </landing_gear>
+ <propulsion description="Propulsion components" tool_level="0">
+ <position description="Reference position of the propulsion assembly">
+ <x description="x position">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="y position">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="z position">
+ <unit>m</unit>
+ <value>0</value>
+ <lower_boundary>-20</lower_boundary>
+ <upper_boundary>40</upper_boundary>
+ </z>
+ </position>
+ <mass_properties description="Mass properties of the total propulsion assembly">
+ <mass description="Total propulsion mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10000</upper_boundary>
+ </mass>
+ <inertia description="Inertia of total propulsion system refered to its center of gravity">
+ <j_xx description="inertia component in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia component in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia component in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia component in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia component in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia component in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia component in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia component in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia component in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Propulsion center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <specific>
+ <propulsion ID="0" description="Description of one propulsion unit">
+ <nacelle ID="0" description="Description ">
+ <origin description="Origin of the nacelle in the global aircraft coordinate system">
+ <x description="x coordinate of point">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </x>
+ <y description="y coordinate of point">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </y>
+ <z description="z coordinate of point">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </origin>
+ <normal description="Normal direction of the nacelle in the global aircraft coordinate system">
+ <x description="x direction of unit vector">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </x>
+ <y description="y direction of unit vector">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </y>
+ <z description="z direction of unit vector">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </normal>
+ <mass_properties description="Mass properties of propulsion assembly">
+ <mass description="Total propulsion mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10000</upper_boundary>
+ </mass>
+ <inertia description="Inertia of propulsion referred to its center of gravity">
+ <j_xx description="inertia component in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia component in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia component in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia component in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia component in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia component in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia component in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia component in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia component in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Propulsion center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <sections description="Geometrical description of the nacelle sections">
+ <section ID="0">
+ <origin description="Origin of the section (local)">
+ <x description="x coordinate of point">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </x>
+ <y description="y coordinate of point">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </y>
+ <z description="z coordinate of point">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </origin>
+ <width description="width of the section">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </width>
+ <height description="Height of the section">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </height>
+ <profile description="The profile name of the section">
+ <value>circle</value>
+ </profile>
+ </section>
+ </sections>
+ </nacelle>
+ <pylon description="Description of pylon">
+ <position description="Reference position of the pylon">
+ <x description="x position">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="y position">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="z position">
+ <unit>m</unit>
+ <value>0</value>
+ <lower_boundary>-20</lower_boundary>
+ <upper_boundary>40</upper_boundary>
+ </z>
+ </position>
+ <normal description="Unit vector according to global coordinate system for direction applied at position">
+ <x description="x direction of unit vector">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </x>
+ <y description="y direction of unit vector">
+ <value>-1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </y>
+ <z description="z direction of unit vector">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </normal>
+ <mass_properties description="Mass properties of the nacelle">
+ <mass description="Total propulsion mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10000</upper_boundary>
+ </mass>
+ <inertia description="Inertia of propulsion refered to its center of gravity">
+ <j_xx description="inertia component in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia component in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia component in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia component in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia component in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia component in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia component in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia component in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia component in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Propulsion center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <sections description="sections">
+ <section ID="0">
+ <origin description="origin of chord (local)">
+ <x description="x coordinate of point">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </x>
+ <y description="y coordinate of point">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </y>
+ <z description="z coordinate of point">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </origin>
+ <chord_length description="chord length of the section">
+ <value>2</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </chord_length>
+ <geometric_twist description="geometric twist of the section around leading edge">
+ <value>0</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </geometric_twist>
+ <profile description="profile (data normalized to chord length)">
+ <value>n0012</value>
+ </profile>
+ </section>
+ </sections>
+ </pylon>
+ <engine description="Description of engine">
+ <engine_model description="Name of selected engine model">
+ <value>0.0</value>
+ </engine_model>
+ <position description="Reference position of the engine">
+ <x description="x position">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="y position">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="z position">
+ <unit>m</unit>
+ <value>0</value>
+ <lower_boundary>-20</lower_boundary>
+ <upper_boundary>40</upper_boundary>
+ </z>
+ </position>
+ <mass_properties description="Mass properties of one propulsion unit">
+ <mass description="Mass of engine">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10000</upper_boundary>
+ </mass>
+ <inertia description="Inertia of propulsion refered to its center of gravity">
+ <j_xx description="inertia component in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia component in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia component in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia component in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia component in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia component in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia component in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia component in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia component in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Propulsion center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <scale_factor description="Scale factor for this engine">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </scale_factor>
+ </engine>
+ </propulsion>
+ </specific>
+ </propulsion>
+ <systems tool_level="0">
+ <position></position>
+ <mass_properties description="mass_properties of component systems">
+ <mass description="component mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia></inertia>
+ <center_of_gravity description="component center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <specific>
+ <geometry>
+ <mass_properties>
+ <auxiliary_power_unit description="Airbus Chapter 30, ATA49">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </auxiliary_power_unit>
+ <hydraulic_generation description="Airbus Chapter 31, ATA 29">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </hydraulic_generation>
+ <hydraulic_distribution description="Airbus Chapter 32, ATA 29">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </hydraulic_distribution>
+ <air_conditioning description="Airbus Chapter 33, ATA21">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </air_conditioning>
+ <de_icing description="Airbus Chapter 34, ATA30">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </de_icing>
+ <fire_protection description="Airbus Chapter 35, ATA26">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </fire_protection>
+ <flight_controls description="Airbus Chapter 36, ATA27">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </flight_controls>
+ <instruments description="Airbus Chapter 37, ATA31">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </instruments>
+ <automatic_flight_system description="Airbus Chapter 38, ATA 22">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </automatic_flight_system>
+ <navigation description="Airbus Chapter 39, ATA34">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </navigation>
+ <communication description="Airbus Chapter 40, ATA23">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </communication>
+ <electrical_generation description="Airbus Chapter 41, ATA24, generation">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </electrical_generation>
+ <electrical_distribution description="Airbus Chapter 42, ATA24, distribution">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </electrical_distribution>
+ <bleed_air_system description="Airbus Chapter 21, ATA36">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </bleed_air_system>
+ <fuel_system description="Airbus Chapter 25, ATA28">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </fuel_system>
+ </mass_properties>
+ </geometry>
+ <maximium_power_demand description="maximum power (hydraulic + electric) demand">
+ <value></value>
+ <unit>W</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </maximium_power_demand>
+ <maximium_bleed_air_demand description="maximum bleed air demand">
+ <value></value>
+ <unit>kg/s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </maximium_bleed_air_demand>
+ <average_power_demand description="average power (hydraulic + electric) demand">
+ <value></value>
+ <unit>W</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </average_power_demand>
+ <average_bleed_air_demand description="average bleed air demand"> <!-- average needed by mission?!-->
+ <value></value>
+ <unit>kg/s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </average_bleed_air_demand>
+ <inflight_entertainment>
+ <number>
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </number>
+ <mass>
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ </inflight_entertainment>
+ </specific>
+ </systems>
+ </component_design>
+ <analysis>
+ <masses_cg_inertia description="masses, cgs, inertias." tool_level="0">
+ <manufacturer_mass_empty description="MME">
+ <mass_properties description="manufacturer mass empty properties">
+ <mass description="mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="inertia refered to center of gravity">
+ <j_xx description="inertia in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </manufacturer_mass_empty>
+ <operating_mass_empty description="OME">
+ <mass_properties description="operating mass empty properties">
+ <mass description="mass">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>300000</upper_boundary>
+ </mass>
+ <inertia description="inertia refered to center of gravity">
+ <j_xx description="inertia in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </operating_mass_empty>
+ <maximum_zero_fuel_mass description="MZFM">
+ <mass_properties description="maximum zero fuel mass properties">
+ <mass description="mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="inertia refered to center of gravity">
+ <j_xx description="inertia in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </maximum_zero_fuel_mass>
+ <maximum_landing_mass description="MLM">
+ <mass_properties description="maximum landing mass properties">
+ <mass description="mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="inertia refered to center of gravity">
+ <j_xx description="inertia in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </maximum_landing_mass>
+ <maximum_takeoff_mass description="MTOM">
+ <mass_properties description="maximum takeoff mass properties">
+ <mass description="mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="inertia refered to center of gravity">
+ <j_xx description="inertia in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </maximum_takeoff_mass>
+ <maximum_payload_mass description="maximum payload mass">
+ <mass_properties description="maximum payload mass properties">
+ <mass description="mass">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>150000</upper_boundary>
+ </mass>
+ <inertia description="inertia refered to center of gravity">
+ <j_xx description="inertia in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </maximum_payload_mass>
+ <maximum_fuel_mass description="maximum fuel mass">
+ <mass_properties description="maximum fuel mass properties">
+ <mass description="mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="inertia refered to center of gravity">
+ <j_xx description="inertia in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </maximum_fuel_mass>
+ <most_forward_mass description="mass for most forward cg position">
+ <mass_properties description="maximum fuel mass properties">
+ <mass description="mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="inertia refered to center of gravity">
+ <j_xx description="inertia in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </most_forward_mass>
+ <design_mass description="design mass ">
+ <mass_properties description="design mass properties">
+ <mass description="mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="inertia refered to center of gravity">
+ <j_xx description="inertia in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </design_mass>
+ <most_afterward_mass description="mass for most afterward cg position">
+ <mass_properties description="most afterward mass properties">
+ <mass description="mass">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="inertia refered to center of gravity">
+ <j_xx description="inertia in x">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia in y">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia in z">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia in xy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia in xz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia in yx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia in yz">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia in zx">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia in zy">
+ <value>0.0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="center of gravity with respect to global coordinate system">
+ <x description="x component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </most_afterward_mass>
+ </masses_cg_inertia>
+ <aerodynamics description="Aerodynamical analysis." level="0">
+ <reference_values>
+ <b description="Total wing span" tool_level="0">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </b>
+ <MAC description="Mean aerodynamic chord" tool_level="0">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </MAC>
+ <S_ref description="Wing reference area" tool_level="0">
+ <value>126.5</value>
+ <unit>m^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000</upper_boundary>
+ </S_ref>
+ </reference_values>
+ <lift_coefficients>
+ <C_LmaxLanding description="Maximum lift coefficient in landing configuration" tool_level="0">
+ <value>2.8</value>
+ <lower_boundary>0.001</lower_boundary>
+ <upper_boundary>4</upper_boundary>
+ </C_LmaxLanding>
+ <C_LmaxT-O description="Maximum lift coefficient in take off configuration" tool_level="0">
+ <value>2.4</value>
+ <lower_boundary>0.001</lower_boundary>
+ <upper_boundary>4</upper_boundary>
+ </C_LmaxT-O>
+ <C_LoptimumCruise description="Lift coefficient at L/D_optimum at M_initial_cruise" tool_level="0">
+ <value>0.528</value>
+ <lower_boundary>0.001</lower_boundary>
+ <upper_boundary>2</upper_boundary>
+ </C_LoptimumCruise>
+ <C_LgroundRoll description="Lift coefficient on ground for ground roll calculation" tool_level="0">
+ <value>0.4</value>
+ <lower_boundary>0.001</lower_boundary>
+ <upper_boundary>2</upper_boundary>
+ </C_LgroundRoll>
+ </lift_coefficients>
+ <polar>
+ <polar_file description="Name of polar file" tool_level="0">
+ <value>/aeroData/CSR-02_polar.xml</value>
+ </polar_file>
+ <configurations description="Number of configurations in the polar file" tool_level="0">
+ <value>0</value>
+ </configurations>
+ <configuration ID="0" description="Configuration in polar file marked with ID - name can vary" tool_level="0">
+ <type>
+ <value>Cruise</value>
+ </type>
+ <name>
+ <value>Clean</value>
+ </name>
+ </configuration>
+ <configuration ID="1" description="Configuration in polar file marked with ID - name can vary" tool_level="0">
+ <type>
+ <value>Cruise</value>
+ </type>
+ <name>
+ <value>Clean</value>
+ </name>
+ <type>Departure</type>
+ <value>TakeOff</value>
+ </configuration>
+ <configuration ID="2" description="Configuration in polar file marked with ID - name can vary" tool_level="0">
+ <type>
+ <value>Departure</value>
+ </type>
+ <name>
+ <value>TakeOffLGRetracted</value>
+ </name>
+ </configuration>
+ <configuration ID="3" description="Configuration in polar file marked with ID - name can vary" tool_level="0">
+ <type>
+ <value>Departure</value>
+ </type>
+ <name>
+ <value>Climb</value>
+ </name>
+ </configuration>
+ <configuration ID="4" description="Configuration in polar file marked with ID - name can vary" tool_level="0">
+ <type>
+ <value>Approach</value>
+ </type>
+ <name>
+ <value>Approach</value>
+ </name>
+ </configuration>
+ <configuration ID="5" description="Configuration in polar file marked with ID - name can vary" tool_level="0">
+ <type>
+ <value>Approach</value>
+ </type>
+ <name>
+ <value>ApproachLG</value>
+ </name>
+ </configuration>
+ <configuration ID="6" description="Configuration in polar file marked with ID - name can vary" tool_level="0">
+ <type>
+ <value>Approach</value>
+ </type>
+ <name>
+ <value>Landing</value>
+ </name>
+ </configuration>
+ </polar>
+ <max_spoiler_factor description="Factor for maximum drag increase trough spoilers" tool_level="0">
+ <value>2.5</value>
+ <lower_boundary>0.001</lower_boundary>
+ <upper_boundary>4</upper_boundary>
+ </max_spoiler_factor>
+ </aerodynamics>
+ <mission description="Mission data." tool_level="0">
+ <design_mission description="Data of design mission">
+ <range description="Range for the whole mission">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5000000</upper_boundary>
+ </range>
+ <block_time description="Block time for the whole mission: Time from break release to end of taxiing after landing">
+ <value>0</value>
+ <unit>s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>45000</upper_boundary>
+ </block_time>
+ <flight_time description="Flight time for the whole mission">
+ <value>0</value>
+ <unit>s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>44500</upper_boundary>
+ </flight_time>
+ <taxi_energy ID="0" description="Amount of energy needed for taxi segment specified energy carrier">
+ <consumed_energy description="Energy amount">
+ <value>0</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1e12</upper_boundary>
+ </consumed_energy>
+ <energy_carrier_ID description="see energy carrier specification node">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </energy_carrier_ID>
+ </taxi_energy>
+ <mission_energy ID="0" description="Amount of energy needed for all segments of the whole mission (including reserves) for specified energy carrier">
+ <consumed_energy description="Energy amount">
+ <value>0</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1e12</upper_boundary>
+ </consumed_energy>
+ <energy_carrier_ID description="see energy carrier specification node">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </energy_carrier_ID>
+ </mission_energy>
+ <trip_energy ID="0" description="Amount of energy needed for trip segments (all segments from takeoff to landing) for specified energy carrier">
+ <consumed_energy description="Energy amount">
+ <value>0</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1e12</upper_boundary>
+ </consumed_energy>
+ <energy_carrier_ID description="see energy carrier specification node">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </energy_carrier_ID>
+ </trip_energy>
+ <payload_mass description="Total payload carried by the aircraft">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>150000</upper_boundary>
+ </payload_mass>
+ <number_of_pax description="Number of passengers for the mission">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000</upper_boundary>
+ </number_of_pax>
+ <cargo_mass description="Cargo mass">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </cargo_mass>
+ <takeoff_engine_derate description="Engine power demand">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </takeoff_engine_derate>
+ <cruise description="Characteristics of the cruise segment">
+ <cruise_steps description="Cruise step information">
+ <cruise_step ID="0" description="Data of a cruise step">
+ <relative_end_of_cruise_step description="End of cruise step relative to total cruise length">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </relative_end_of_cruise_step>
+ <altitude description="Altitude of cruise step">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>15000</upper_boundary>
+ </altitude>
+ </cruise_step>
+ </cruise_steps>
+ <top_of_climb_mass description="Total aircraft mass at top of climb (= start of initial cruise altitude (ICA))">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>150000</upper_boundary>
+ </top_of_climb_mass>
+ <top_of_climb_range description="Flown range from takeoff to top of climb (= start of initial cruise altitude (ICA))">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>500000</upper_boundary>
+ </top_of_climb_range>
+ <top_of_descent_mass description="Total aircraft mass at top of descent (TOD)">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>150000</upper_boundary>
+ </top_of_descent_mass>
+ <top_of_descent_range description="Flown range from takeoff to top of descent">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>5000000</upper_boundary>
+ </top_of_descent_range>
+ <average_lift_coefficient description="Lift coefficient CL_avg: Arithmetic mean over the entire cruise flight">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-0.01</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </average_lift_coefficient>
+ <minimum_lift_coefficient description="Minimum cruise flight lift coefficient CL_min">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-0.01</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </minimum_lift_coefficient>
+ <maximum_lift_coefficient description="Maximum cruise flight lift coefficient CL_max">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-0.01</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </maximum_lift_coefficient>
+ </cruise>
+ </design_mission>
+ <study_mission description="Data of study mission">
+ <range description="Range for the whole mission">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5000000</upper_boundary>
+ </range>
+ <block_time description="Block time for the whole mission: Time from break release to end of taxiing after landing">
+ <value>0</value>
+ <unit>s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>45000</upper_boundary>
+ </block_time>
+ <flight_time description="Flight time for the whole mission">
+ <value>0</value>
+ <unit>s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>44500</upper_boundary>
+ </flight_time>
+ <taxi_energy ID="0" description="Amount of energy needed for taxi segment for energy carrier ID 0">
+ <value>0</value>
+ <unit>Ws</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000000000000</upper_boundary>
+ </taxi_energy>
+ <taxi_energy ID="1" description="Amount of energy needed for taxi segment for energy carrier ID 1">
+ <value>0</value>
+ <unit>Ws</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000000000000</upper_boundary>
+ </taxi_energy>
+ <mission_energy ID="0" description="Amount of energy needed for Wsole mission (including reserves) for energy carrier ID 0">
+ <value>0</value>
+ <unit>Ws</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000000000000</upper_boundary>
+ </mission_energy>
+ <mission_energy ID="1" description="Amount of energy needed for Wsole mission (including reserves) for energy carrier ID 1">
+ <value>0</value>
+ <unit>Ws</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000000000000</upper_boundary>
+ </mission_energy>
+ <trip_energy ID="0" description="Amount of energy needed for trip segment (from takeoff to landing) for energy carrier ID 0">
+ <value>0</value>
+ <unit>Ws</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000000000000</upper_boundary>
+ </trip_energy>
+ <trip_energy ID="1" description="Amount of energy needed for trip segment (from takeoff to landing) for energy carrier ID 1">
+ <value>0</value>
+ <unit>Ws</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000000000000</upper_boundary>
+ </trip_energy>
+ <payload_mass description="Total payload carried by the aircraft">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>150000</upper_boundary>
+ </payload_mass>
+ <number_of_pax description="Number of passengers for the mission">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000</upper_boundary>
+ </number_of_pax>
+ <cargo_mass description="Cargo mass of for the mission">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>150000</upper_boundary>
+ </cargo_mass>
+ <takeoff_engine_derate description="Engine power demand">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </takeoff_engine_derate>
+ <takeoff_mass description="Takeoff mass">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>150000</upper_boundary>
+ </takeoff_mass>
+ <cruise description="Characteristics of the cruise segment">
+ <cruise_steps description="Cruise step information">
+ <cruise_step ID="0" description="Data of a cruise step">
+ <relative_end_of_cruise_step description="End of cruise step relative to total cruise length">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </relative_end_of_cruise_step>
+ <altitude description="Altitude of cruise step">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>15000</upper_boundary>
+ </altitude>
+ </cruise_step>
+ </cruise_steps>
+ <top_of_climb_mass description="Total aircraft mass at top of climb (= start of initial cruise altitude (ICA))">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>150000</upper_boundary>
+ </top_of_climb_mass>
+ <top_of_climb_range description="Flown range from takeoff to top of climb (= start of initial cruise altitude (ICA))">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>250000</upper_boundary>
+ </top_of_climb_range>
+ <top_of_descent_mass description="Total aircraft mass at top of descent (TOD)">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>150000</upper_boundary>
+ </top_of_descent_mass>
+ <top_of_descent_range description="Flown range from takeoff to top of descent">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>5000000</upper_boundary>
+ </top_of_descent_range>
+ <average_lift_coefficient description="Lift coefficient CL_avg: Arithmetic mean over the entire cruise flight">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-0.01</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </average_lift_coefficient>
+ <minimum_lift_coefficient description="Minimum cruise flight lift coefficient CL_min">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-0.01</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </minimum_lift_coefficient>
+ <maximum_lift_coefficient description="Maximum cruise flight lift coefficient CL_max">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-0.01</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </maximum_lift_coefficient>
+ </cruise>
+ </study_mission>
+ </mission>
+ </analysis>
+ <assessment>
+ <performance description="Assessment of performance values">
+ <speed tool_level="0">
+ <maximum_operating_mach_number description="Maximum operating mach number">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </maximum_operating_mach_number>
+ <maximum_operating_velocity description="Maximum operating speed (maximum dynamic pressure)">
+ <value>0</value>
+ <unit>m/s</unit>
+ <lower_boundary>50</lower_boundary>
+ <upper_boundary>250</upper_boundary>
+ </maximum_operating_velocity>
+ <dive_mach_number description="Diving mach number">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </dive_mach_number>
+ <dive_velocity description="Diving speed">
+ <value>0</value>
+ <unit>m/s</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>500.0</upper_boundary>
+ </dive_velocity>
+ <one_g_stall_speed_velocity description="One g stall speed in clean configuration">
+ <value>0</value>
+ <unit>m/s</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </one_g_stall_speed_velocity>
+ </speed>
+ <takeoff tool_level="0">
+ <takeoff_distance_normal_safety description="Takeoff distance at Sea Level for MTOM and (ISA + deltaISA)-Conditions(calculated by missionAnalysis using missionDesign.xml settings) with all engines operating (AEO)">
+ <value>0</value>
+ <unit>m</unit>
+ </takeoff_distance_normal_safety>
+ <lift_off_speed_velocity description="Lift-off speed in take-off configuration">
+ <value>0</value>
+ <unit>m/s</unit>
+ </lift_off_speed_velocity>
+ <decision_speed description="Decision speed">
+ <value>0</value>
+ <unit>m/s</unit>
+ </decision_speed>
+ <takeoff_safety_speed description="Speed at screen height (35 ft)">
+ <value>0</value>
+ <unit>m/s</unit>
+ </takeoff_safety_speed>
+ <final_takeoff_speed description="Speed at final takeoff segment (1500 ft)">
+ <value>0</value>
+ <unit>m/s</unit>
+ </final_takeoff_speed>
+ <time_to_screen_height description="Time to screen height">
+ <value>0</value>
+ <unit>s</unit>
+ </time_to_screen_height>
+ <climb_or_descend_segment_climb_gradient description="Climb gradient in second takeoff segment">
+ <value>0</value>
+ <unit>1</unit>
+ </climb_or_descend_segment_climb_gradient>
+ <final_segment_climb_gradient description="Climb gradient in final takeoff segment">
+ <value>0</value>
+ <unit>1</unit>
+ </final_segment_climb_gradient>
+ <balanced_field_length description="Balanced field length">
+ <value>0</value>
+ <unit>m</unit>
+ </balanced_field_length>
+ </takeoff>
+ <climb>
+ <design_time_to_climb description="Time needed to climb from 1500ft to ICA (ISA + deltaISA)">
+ <value>0</value>
+ <unit>s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>7200</upper_boundary>
+ </design_time_to_climb>
+ <time_to_1500ft_ISA description="Time needed to climb from break release to 1500ft (ISA + deltaISA)">
+ <value>0</value>
+ <unit>s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>7200</upper_boundary>
+ </time_to_1500ft_ISA>
+ <time_to_ICA_ISA description="Time needed to climb from break release to ICA (ISA + deltaISA)">
+ <value>0</value>
+ <unit>s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>7200</upper_boundary>
+ </time_to_ICA_ISA>
+ <range_to_ICA_ISA description="Range needed to climb from break release to ICA (ISA + deltaISA)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>45000</upper_boundary>
+ </range_to_ICA_ISA>
+ <fuel_to_ICA_ISA description="Fuel mass needed to climb from break release to ICA (ISA + deltaISA)">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5000</upper_boundary>
+ </fuel_to_ICA_ISA>
+ </climb>
+ <landing tool_level="0">
+ <needed_runway_length description="Needed runway length with all engines operating and maximum landing mass">
+ <value>0</value>
+ <unit>m</unit>
+ </needed_runway_length>
+ <approach_speed description="Final approach speed in landing configuration and maximum landing mass">
+ <value>0</value>
+ <unit>m/s</unit>
+ </approach_speed>
+ </landing>
+ <range tool_level="0">
+ <range_max_payload_at_maximum_takeoff_mass description="Range at maximum payload and fuel mass till maximum take off mass limit">
+ <value>0</value>
+ <unit>m</unit>
+ </range_max_payload_at_maximum_takeoff_mass>
+ <range_max_fuel_at_maximum_takeoff_mass description="Range at full tanks and payload till maximum take off mass limit">
+ <value>0</value>
+ <unit>m</unit>
+ </range_max_fuel_at_maximum_takeoff_mass>
+ <payload_maximum_fuel_at_maximum_takeoff_mass description="Payload at full tanks and payload till maximum take off mass limit">
+ <value>0</value>
+ <unit>kg</unit>
+ </payload_maximum_fuel_at_maximum_takeoff_mass>
+ <range_maximum_fuel_empty description="Range for no payload and full tanks">
+ <value>0</value>
+ <unit>m</unit>
+ </range_maximum_fuel_empty>
+ </range>
+ <altitude>
+ <maximum_operating_altitude description="Maximum operating altitude (100 ft/min rate of climb)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>4500</lower_boundary>
+ <upper_boundary>20000</upper_boundary>
+ </maximum_operating_altitude>
+ <maximum_ceiling_altitude description="Maximum operating altitude (50 ft/min rate of climb)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>4500</lower_boundary>
+ <upper_boundary>20000</upper_boundary>
+ </maximum_ceiling_altitude>
+ <maximum_one_engine_operating_altitude description="Maximum operating altitude with one engine inoperative (100 ft/min rate of climb)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>1500</lower_boundary>
+ <upper_boundary>12000</upper_boundary>
+ </maximum_one_engine_operating_altitude>
+ </altitude>
+ </performance>
+ <direct_operating_cost description="Direct operating cost (sum of route independent and route dependent cost)">
+ <route_independent_cost_annual description="Route independent (fixed) cost per year">
+ <value>0</value>
+ <unit>EUR/a</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </route_independent_cost_annual>
+ <route_dependent_cost_annual description="Route dependent (variable) cost per year">
+ <value>0</value>
+ <unit>EUR/a</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </route_dependent_cost_annual>
+ <direct_operating_cost_annual description="Direct operating cost (DOC) per year">
+ <value>0</value>
+ <unit>EUR/a</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </direct_operating_cost_annual>
+ </direct_operating_cost>
+ <average_temperature_response description="Integrated temperature change per year caused by aircraft operation divided by operating lifetime" tool_level="2">
+ <value>0</value>
+ <unit>K</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1e-5</upper_boundary>
+ </average_temperature_response>
+ </assessment>
+ <requirement_compliance>
+ <top_level_aircraft_requirements tool_level="0">
+ <design_takeoff_distance description="Switch indicating if design takeoff distance can be maintained.">
+ <maintainable description="Value shows if design takeoff distance can be maintained.">
+ <value>false</value>
+ </maintainable>
+ <checked description="Indicates if the value has been checked against the requirement.">
+ <value>false</value>
+ </checked>
+ </design_takeoff_distance>
+ <design_landing_field_length description="Switch indicating if landing field length can be maintained.">
+ <maintainable description="Value shows if design landing field length can be maintained.">
+ <value>false</value>
+ </maintainable>
+ <checked description="Indicates if the value has been checked against the requirement.">
+ <value>false</value>
+ </checked>
+ </design_landing_field_length>
+ <design_approach_speed description="Switch indicating if approach speed can be maintained.">
+ <maintainable description="Value shows if design approach speed can be maintained.">
+ <value>false</value>
+ </maintainable>
+ <checked description="Indicates if the value has been checked against the requirement.">
+ <value>false</value>
+ </checked>
+ </design_approach_speed>
+ <initial_cruise_altitude description="Switch indicating if initial cruise design altitude can be maintained.">
+ <maintainable description="Value shows if initial cruise design altitude can be maintained.">
+ <value>false</value>
+ </maintainable>
+ <checked description="Indicates if the value has been checked against the requirement.">
+ <value>false</value>
+ </checked>
+ </initial_cruise_altitude>
+ <maximum_operating_altitude description="Switch indicating if the maximum operating altitude can be maintained.">
+ <maintainable description="Value shows if maximum operating altitude can be maintained.">
+ <value>false</value>
+ </maintainable>
+ <checked description="Indicates if the value has been checked against the requirement.">
+ <value>false</value>
+ </checked>
+ </maximum_operating_altitude>
+ <maximum_one_engine_operating_altitude description="Switch indicating if the maximum one engine operating altitude can be maintained.">
+ <maintainable description="Value shows if maximum one engine operating altitude can be maintained.">
+ <value>false</value>
+ </maintainable>
+ <checked description="Indicates if the value has been checked against the requirement.">
+ <value>false</value>
+ </checked>
+ </maximum_one_engine_operating_altitude>
+ <initial_cruise_mach_number description="Switch indicating if cruise design Mach number can be maintained.">
+ <maintainable description="Value shows if cruise design Mach number can be maintained.">
+ <value>false</value>
+ </maintainable>
+ <checked description="Indicates if the value has been checked against the requirement.">
+ <value>false</value>
+ </checked>
+ </initial_cruise_mach_number>
+ <design_time_to_climb description="Switch indicating if the design time to climb can be maintained.">
+ <maintainable description="Value shows if design time to climb can be maintained.">
+ <value>false</value>
+ </maintainable>
+ <checked description="Indicates if the value has been checked against the requirement.">
+ <value>false</value>
+ </checked>
+ </design_time_to_climb>
+ </top_level_aircraft_requirements>
+ <certification tool_level="0">
+ <climb_gradient_of_second_takeoff_segment description="Switch if climb gradient of second takeoff segment can be maintained">
+ <maintainable description="Value shows if climb gradient of second takeoff segment can be maintained.">
+ <value>false</value>
+ </maintainable>
+ <checked description="Indicates if the value has been checked against the requirement.">
+ <value>false</value>
+ </checked>
+ </climb_gradient_of_second_takeoff_segment>
+ <climb_gradient_of_final_takeoff_segment description="Switch if climb gradient of final takeoff segment can be maintained">
+ <maintainable description="Value shows if climb gradient of final takeoff segment can be maintained.">
+ <value>false</value>
+ </maintainable>
+ <checked description="Indicates if the value has been checked against the requirement.">
+ <value>false</value>
+ </checked>
+ </climb_gradient_of_final_takeoff_segment>
+ <climb_gradient_approach_one_engine_inoperative description="Switch if climb gradient approach one engine inoperative can be maintained">
+ <maintainable description="Value shows if climb gradient approach one engine inoperative can be maintained.">
+ <value>false</value>
+ </maintainable>
+ <checked description="Indicates if the value has been checked against the requirement.">
+ <value>false</value>
+ </checked>
+ </climb_gradient_approach_one_engine_inoperative>
+ <climb_gradient_all_engines_operative description="Switch if climb gradient all engines operative can be maintained">
+ <maintainable description="Value shows if climb gradient all engines operative can be maintained.">
+ <value>false</value>
+ </maintainable>
+ <checked description="Indicates if the value has been checked against the requirement.">
+ <value>false</value>
+ </checked>
+ </climb_gradient_all_engines_operative>
+ </certification>
+ </requirement_compliance>
+</aircraft_exchange_file>
diff --git a/UnicadoGUI/Backend/xml_configs/weightAndBalanceAnalysis_conf.xml b/UnicadoGUI/Backend/xml_configs/weightAndBalanceAnalysis_conf.xml
new file mode 100644
index 0000000..5d27e7e
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/weightAndBalanceAnalysis_conf.xml
@@ -0,0 +1,96 @@
+<?xml version="1.0" encoding="utf-8"?>
+<module_configuration_file Name="Weight and Balance Configuration">
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>template.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>../projects/CSR/CSR-02/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>2</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <html_output description="Switch to generate a HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </html_output>
+ <xml_output description="Switch to export module specific data to XML ('true': On, 'false': Off)">
+ <value>false</value>
+ </xml_output>
+ <tex_output description="Switch to generate a TeX report ('true': On, 'false': Off)">
+ <value>false</value>
+ </tex_output>
+ <info_file_output description="Switch to generate info files containing inputs, outputs and gui settings (False: Off, True: On)">
+ <value>false</value>
+ </info_file_output>
+ <gnuplot_script_name description="Specify the name of the plot file">
+ <value>weightAndBalanceAnalysis_plot.plt</value>
+ </gnuplot_script_name>
+ <log_file_name description="Specify the name of the log file">
+ <value>weightAndBalanceAnalysis.log</value>
+ </log_file_name>
+ <inkscape_path description="Path to the inkscape application (DEFAULT: Use inkscape from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application (DEFAULT: Use gnuplot from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings description="program settings">
+ <tube_and_wing description="weight and balance for tube and wing">
+ <category description="selector for category: standard, ...">
+ <value>standard</value>
+ </category>
+ <standard description="standard weight and balance">
+ <method description="selector for method: basic, ...">
+ <value>basic</value>
+ </method>
+ <basic description="Basic configuration">
+ <calculation_methods description="calculation methods for basic configuration">
+ <inertia description="selector mode_0: by_lth_table, mode_1: by_components">
+ <method description="selected method">
+ <value>mode_0</value>
+ </method>
+ </inertia>
+ <maximum_landing_mass description="selector mode_0: by_default_method (OME-Payload-Reserve_fuel), mode_1: by_regression_rwth">
+ <method description="selected method">
+ <value>mode_1</value>
+ </method>
+ </maximum_landing_mass>
+ <refueling_mode description="selector mode_0: by_default_method (design mission), mode_1: ferry range">
+ <method description="selected method">
+ <value>mode_0</value>
+ </method>
+ </refueling_mode>
+ <defueling_mode description="selector mode_0: by_default_method (design mission), mode_1: active">
+ <method description="selected method">
+ <value>mode_1</value>
+ </method>
+ </defueling_mode>
+ <passengers_boarding_mode description="selector mode_0: by_default_method (each row at a time), mode_1: window to aisle">
+ <method description="selected method">
+ <value>mode_0</value>
+ </method>
+ </passengers_boarding_mode>
+ </calculation_methods>
+ </basic>
+ </standard>
+ </tube_and_wing>
+ </program_settings>
+</module_configuration_file>
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/xml_configs/weightAndBalanceAnalysis_conf_default.xml b/UnicadoGUI/Backend/xml_configs/weightAndBalanceAnalysis_conf_default.xml
new file mode 100644
index 0000000..b5dfd2b
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/weightAndBalanceAnalysis_conf_default.xml
@@ -0,0 +1,96 @@
+<?xml version="1.0" encoding="UTF-8" ?>
+ <module_configuration_file Name="Weight and Balance Configuration"> <!-- Change naming according to module name -->
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>template.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>../projects/CSR/CSR-02/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>2</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <html_output description="Switch to generate a HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </html_output>
+ <xml_output description="Switch to export module specific data to XML ('true': On, 'false': Off)">
+ <value>false</value>
+ </xml_output>
+ <tex_output description="Switch to generate a TeX report ('true': On, 'false': Off)">
+ <value>false</value>
+ </tex_output>
+ <info_file_output description="Switch to generate info files containing inputs, outputs and gui settings (False: Off, True: On)">
+ <value>false</value>
+ </info_file_output>
+ <gnuplot_script_name description="Specify the name of the plot file">
+ <value>weightAndBalanceAnalysis_plot.plt</value>
+ </gnuplot_script_name>
+ <log_file_name description="Specify the name of the log file">
+ <value>weightAndBalanceAnalysis.log</value>
+ </log_file_name>
+ <inkscape_path description="Path to the inkscape application (DEFAULT: Use inkscape from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application (DEFAULT: Use gnuplot from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings description="program settings">
+ <tube_and_wing description="weight and balance for tube and wing">
+ <category description="selector for category: standard, ...">
+ <value>standard</value>
+ </category>
+ <standard description="standard weight and balance">
+ <method description="selector for method: basic, ...">
+ <value>basic</value>
+ </method>
+ <basic description="Basic configuration">
+ <calculation_methods description="calculation methods for basic configuration">
+ <inertia description="selector mode_0: by_lth_table, mode_1: by_components">
+ <method description="selected method">
+ <value>mode_0</value>
+ </method>
+ </inertia>
+ <maximum_landing_mass description="selector mode_0: by_default_method (OME-Payload-Reserve_fuel), mode_1: by_regression_rwth">
+ <method description="selected method">
+ <value>mode_1</value>
+ </method>
+ </maximum_landing_mass>
+ <refueling_mode description="selector mode_0: by_default_method (design mission), mode_1: ferry range">
+ <method description="selected method">
+ <value>mode_0</value>
+ </method>
+ </refueling_mode>
+ <defueling_mode description="selector mode_0: by_default_method (design mission), mode_1: active">
+ <method description="selected method">
+ <value>mode_1</value>
+ </method>
+ </defueling_mode>
+ <passengers_boarding_mode description="selector mode_0: by_default_method (each row at a time), mode_1: window to aisle">
+ <method description="selected method">
+ <value>mode_0</value>
+ </method>
+ </passengers_boarding_mode>
+ </calculation_methods>
+ </basic>
+ </standard>
+ </tube_and_wing>
+ </program_settings>
+ </module_configuration_file>
diff --git a/UnicadoGUI/Backend/xml_configs/wingDesign_conf.xml b/UnicadoGUI/Backend/xml_configs/wingDesign_conf.xml
new file mode 100644
index 0000000..a413da7
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/wingDesign_conf.xml
@@ -0,0 +1,731 @@
+<?xml version="1.0" encoding="utf-8"?>
+<module_configuration_file name="wingDesign_conf.xml">
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>csmr-2020.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>../../rAIRCRAFTREFERENCES/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>3</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>true</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>false</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>TOOLNAME_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>wing_design.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings>
+ <modes description="mode selection">
+ <design_mode description="selector mode_0: design, mode_1: redesign (axml must hold a wing)">
+ <value>mode_0</value>
+ </design_mode>
+ </modes>
+ <tube_and_wing description="settings for tube and wing (TAW)">
+ <wing_configuration description="selector mode_0: cantilever">
+ <value>mode_0</value>
+ </wing_configuration>
+ <cantilever description="cantilever design information">
+ <calculation_methods description="calculation methods for specific parameter">
+ <wing_area description="wing area calculation method">
+ <method description="selector mode_0: user_defined, mode_1: by_loading_and_mtom">
+ <value>mode_1</value>
+ </method>
+ <parameters>
+ <mode_0 description="user_defined">
+ <wing_area description="wing area">
+ <value>126.34</value>
+ <unit>m^2</unit>
+ <lower_boundary>50.0</lower_boundary>
+ <upper_boundary>5000.0</upper_boundary>
+ </wing_area>
+ </mode_0>
+ </parameters>
+ </wing_area>
+ <sweep description="sweep calculation method">
+ <method description="selector mode_0: user_defined, mode_1: drag_divergence">
+ <value>mode_0</value>
+ </method>
+ <parameters description="sweep method parameters">
+ <mode_0 description="user_defined">
+ <sweep_angle description="sweep angle at quarter chord">
+ <value>25</value>
+ <unit>deg</unit>
+ <lower_boundary>-60</lower_boundary>
+ <upper_boundary>60</upper_boundary>
+ </sweep_angle>
+ </mode_0>
+ <mode_1 description="drag_divergence">
+ <korn_technology_factor description="technology factor">
+ <value>0.96</value>
+ <unit>1</unit>
+ <lower_boundary>0.85</lower_boundary>
+ <upper_boundary>0.96</upper_boundary>
+ </korn_technology_factor>
+ <delta_drag_divergence_to_mach_design description="offset between mach design and drag divergence">
+ <value>0.02</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>0.03</upper_boundary>
+ </delta_drag_divergence_to_mach_design>
+ </mode_1>
+ </parameters>
+ </sweep>
+ <taper_ratio description="taper ratio calculation method">
+ <method description="selector mode_0: user_defined, mode_1: howe">
+ <value>mode_1</value>
+ </method>
+ <parameters>
+ <mode_0 description="user_defined">
+ <taper_ratio description="taper ratio of overall wing">
+ <value>0.17</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </taper_ratio>
+ </mode_0>
+ </parameters>
+ </taper_ratio>
+ <dihedral description="dihedral calculation method">
+ <method description="selector mode_0: user_defined, mode_1: by_wing_position_and_quarter_chord_sweep">
+ <value>mode_1</value>
+ </method>
+ <parameters description="parameters for methods">
+ <mode_0 description="user_defined">
+ <dihedral_angle description="dihedral angle">
+ <value>4</value>
+ <unit>deg</unit>
+ <lower_boundary>-20</lower_boundary>
+ <upper_boundary>20</upper_boundary>
+ </dihedral_angle>
+ </mode_0>
+ <mode_1 description="by_wing_position_and_quarter_chord_sweep">
+ <dihedral_limitation description="selector mode_0: raymer, mode_1: howe">
+ <value>mode_0</value>
+ </dihedral_limitation>
+ </mode_1>
+ </parameters>
+ </dihedral>
+ <aspect_ratio description="aspect ratio calculation method">
+ <method description="selector mode_0: user_defined, mode_1: by_pitch_up_limit_function">
+ <value>mode_1</value>
+ </method>
+ <parameters description="Mode parameters">
+ <mode_0 description="user_defined">
+ <aspect_ratio description="user aspect ratio">
+ <value>11.0</value>
+ <unit>1</unit>
+ <lower_boundary>6</lower_boundary>
+ <upper_boundary>15</upper_boundary>
+ </aspect_ratio>
+ </mode_0>
+ </parameters>
+ </aspect_ratio>
+ <relative_kink_position description="relative kink position method">
+ <method description="selector mode_0: user_defined, mode_1: based_on_landing_gear_track">
+ <value>mode_0</value>
+ </method>
+ <parameters>
+ <mode_0 description="user_defined">
+ <relative_kink_position description="relative to half span - only used if low wing and wing mounted landing gear">
+ <value>0.3</value>
+ <unit>1</unit>
+ <lower_boundary>0.25</lower_boundary>
+ <upper_boundary>0.38</upper_boundary>
+ </relative_kink_position>
+ <maximum_inner_trailing_edge_sweep description="maximum inner trailing edge sweep - sets maximum possible inner trailing edge sweep">
+ <value>10.0</value>
+ <unit>deg</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>20.0</upper_boundary>
+ </maximum_inner_trailing_edge_sweep>
+ </mode_0>
+ <mode_1>
+ <initial_relative_kink_position description="relative to half span - only used if low wing and wing mounted landing gear - initial value -> will change over iteration">
+ <value>0.3</value>
+ <unit>1</unit>
+ <lower_boundary>0.25</lower_boundary>
+ <upper_boundary>0.38</upper_boundary>
+ </initial_relative_kink_position>
+ <maximum_inner_trailing_edge_sweep description="maximum inner trailing edge sweep - sets maximum possible inner trailing edge sweep">
+ <value>10.0</value>
+ <unit>deg</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>20.0</upper_boundary>
+ </maximum_inner_trailing_edge_sweep>
+ </mode_1>
+ </parameters>
+ </relative_kink_position>
+ <wing_profile_and_thickness_distribution description="wing profile calculation methods">
+ <method description="selector mode_0: user_defined, mode_1: torenbeek_jenkinson">
+ <value>mode_1</value>
+ </method>
+ <parameters description="wing profile parameters">
+ <mode_0 description="user_defined - thickness to chord ratio's must be from root to tip - linear interpolation">
+ <wing_profile_and_thickness description="wing profile and thickness at half span" ID="0">
+ <wing_profile description="wing profile">
+ <value>F15</value>
+ </wing_profile>
+ <thickness_to_chord description="Thickness to chord ratio">
+ <ratio description="thickness to chord ratio value">
+ <value>0.16</value>
+ <unit>1</unit>
+ <lower_boundary>0.05</lower_boundary>
+ <upper_boundary>0.40</upper_boundary>
+ </ratio>
+ <at_half_span description="thickness to chord ratio value at half span">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </at_half_span>
+ </thickness_to_chord>
+ </wing_profile_and_thickness>
+ <wing_profile_and_thickness description="wing profile and thickness at half span" ID="1">
+ <wing_profile description="wing profile">
+ <value>F15</value>
+ </wing_profile>
+ <thickness_to_chord description="Thickness to chord ratio">
+ <ratio description="thickness to chord ratio value">
+ <value>0.13</value>
+ <unit>1</unit>
+ <lower_boundary>0.05</lower_boundary>
+ <upper_boundary>0.40</upper_boundary>
+ </ratio>
+ <at_half_span description="thickness to chord ratio value at half span">
+ <value>0.3</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </at_half_span>
+ </thickness_to_chord>
+ </wing_profile_and_thickness>
+ <wing_profile_and_thickness description="wing profile and thickness at half span" ID="2">
+ <wing_profile description="wing profile">
+ <value>F15</value>
+ </wing_profile>
+ <thickness_to_chord description="Thickness to chord ratio">
+ <ratio description="thickness to chord ratio value">
+ <value>0.12</value>
+ <unit>1</unit>
+ <lower_boundary>0.05</lower_boundary>
+ <upper_boundary>0.40</upper_boundary>
+ </ratio>
+ <at_half_span description="thickness to chord ratio value at half span">
+ <value>0.45</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </at_half_span>
+ </thickness_to_chord>
+ </wing_profile_and_thickness>
+ <wing_profile_and_thickness description="wing profile and thickness at half span" ID="3">
+ <wing_profile description="wing profile">
+ <value>F15</value>
+ </wing_profile>
+ <thickness_to_chord description="Thickness to chord ratio">
+ <ratio description="thickness to chord ratio value">
+ <value>0.11</value>
+ <unit>1</unit>
+ <lower_boundary>0.05</lower_boundary>
+ <upper_boundary>0.40</upper_boundary>
+ </ratio>
+ <at_half_span description="thickness to chord ratio value at half span">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </at_half_span>
+ </thickness_to_chord>
+ </wing_profile_and_thickness>
+ </mode_0>
+ <mode_1 description="torenbeek_jenkinson">
+ <wing_profile description="wing profile">
+ <value>F15</value>
+ </wing_profile>
+ <max_thickness_to_chord_ratio description="maximum thickness to chord ratio - will be applied at root inner wing">
+ <value>0.15</value>
+ <unit>1</unit>
+ <lower_boundary>0.10</lower_boundary>
+ <upper_boundary>0.40</upper_boundary>
+ </max_thickness_to_chord_ratio>
+ <airfoil_critical_factor description="factor to describe technology factor of airfoil - conventional 1.0, high speed 1960-1970 technology (peaky) airfoils 1.05, supercritical airfoils 1.12 - 1.15">
+ <value>1.12</value>
+ <unit>1</unit>
+ <lower_boundary>1.0</lower_boundary>
+ <upper_boundary>1.15</upper_boundary>
+ </airfoil_critical_factor>
+ </mode_1>
+ </parameters>
+ </wing_profile_and_thickness_distribution>
+ <mass description="mass calculation methods">
+ <method description="selector mode_0: flops, mode_1: chiozzotto_wer">
+ <value>mode_0</value>
+ </method>
+ <parameters>
+ <mode_0 description="flops">
+ <fstrt description="wing strut bracing factor from 0.0 (no strut) to 1.0 (full benefit from strut bracing)">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </fstrt>
+ <faert description="aeroelastic tailoring factor from 0.0 (no tailoring) to 1.0 (maximum tailoring)">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </faert>
+ <fcomp description="composite utilization factor from 0.0 (no composites) to 1.0 (maximum use of composites)">
+ <value>0.5</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </fcomp>
+ </mode_0>
+ <mode_1 description="chiozzotto_wer">
+ <technology_factor description="technology factor for wing mass: factor below 1 -> higher technology level (less weight), factor above 1 lower technology level (higher weight)">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.7</lower_boundary>
+ <upper_boundary>1.3</upper_boundary>
+ </technology_factor>
+ <material description="material options: AL (Aluminium), CFRP (Carbon fiber reinforced plastic)">
+ <value>AL</value>
+ </material>
+ </mode_1>
+ </parameters>
+ </mass>
+ <control_devices description="control devices calculation method">
+ <method description="selector mode_0: user_defined, mode_1: empirical">
+ <value>mode_1</value>
+ </method>
+ <parameters description="control device method parameters">
+ <mode_0 description="user_defined parameters">
+ <control_device ID="0" description="control device">
+ <type description="control device type - aileron, rudder, elevator, slat, ...">
+ <value>aileron</value>
+ </type>
+ <deflection description="maximum positive and negative deflection of control device">
+ <full_negative_deflection description="full negative deflection">
+ <value>-25.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>25.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ <position description="chord relative position of control device">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.8</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>0.95</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.8</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </control_device>
+ <control_device ID="1" description="control device">
+ <type description="control device type - aileron, rudder, elevator, slat, ...">
+ <value>slat</value>
+ </type>
+ <deflection description="maximum positive and negative deflection of control device">
+ <full_negative_deflection description="full negative deflection">
+ <value>-25.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>0.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ <position description="chord relative position of control device">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>0.9</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </control_device>
+ <control_device ID="2" description="control device">
+ <type description="control device type - aileron, rudder, elevator, slat, ...">
+ <value>fowler</value>
+ </type>
+ <deflection description="maximum positive and negative deflection of control device">
+ <full_negative_deflection description="full negative deflection">
+ <value>0.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>25.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ <position description="chord relative position of control device">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.8</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.8</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </control_device>
+ <control_device ID="3" description="control device">
+ <type description="control device type - aileron, rudder, elevator, slat, ...">
+ <value>spoiler</value>
+ </type>
+ <deflection description="maximum positive and negative deflection of control device">
+ <full_negative_deflection description="full negative deflection">
+ <value>0.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>10.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ <position description="chord relative position of control device">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.8</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>0.65</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.65</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.8</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </control_device>
+ </mode_0>
+ <mode_1 description="empirical parameters">
+ <high_lift_device_type_leading_edge description="slat, krueger, droop_nose, morphing_droop_nose">
+ <value>slat</value>
+ </high_lift_device_type_leading_edge>
+ <high_lift_device_type_trailing_edge description="flaperon, droop_aileron, flap_plain, flap_fowler, flap_fowler_double_slotted, flap_fowler_triple_slotted">
+ <value>flap_fowler</value>
+ </high_lift_device_type_trailing_edge>
+ </mode_1>
+ </parameters>
+ </control_devices>
+ <spars description="spars calculation method">
+ <method description="selector mode_0: user_defined">
+ <value>mode_0</value>
+ </method>
+ <parameters description="spars method parameters">
+ <mode_0 description="user_defined parameters">
+ <spar ID="0" description="component spar">
+ <name description="name of spar">
+ <value>front_spar</value>
+ </name>
+ <position description="chord relative position of spar">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>1.</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </spar>
+ <spar ID="1" description="component spar">
+ <name description="name of spar">
+ <value>rear_spar</value>
+ </name>
+ <position description="chord relative position of spar">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </spar>
+ </mode_0>
+ </parameters>
+ </spars>
+ </calculation_methods>
+ </cantilever>
+ </tube_and_wing>
+ <blended_wing_body>
+ <fidelity_selection description="selection of fidelity level">
+ <value>low</value>
+ </fidelity_selection>
+ <low_fidelity></low_fidelity>
+ </blended_wing_body>
+ </program_settings>
+</module_configuration_file>
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/xml_configs/wingDesign_conf_default.xml b/UnicadoGUI/Backend/xml_configs/wingDesign_conf_default.xml
new file mode 100644
index 0000000..0e42f60
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/wingDesign_conf_default.xml
@@ -0,0 +1,732 @@
+<?xml version="1.0" encoding="utf-8" ?>
+<module_configuration_file name="wingDesign_conf.xml">
+ <control_settings description="General control settings for this tool">
+ <aircraft_exchange_file_name description="Specify the name of the exchange file">
+ <value>csmr-2020.xml</value>
+ </aircraft_exchange_file_name>
+ <aircraft_exchange_file_directory description="Specify the direction in which the aircraft exchange file can be found">
+ <value>../../rAIRCRAFTREFERENCES/</value>
+ </aircraft_exchange_file_directory>
+ <own_tool_level description="Specify the tool level of this tool">
+ <value>3</value>
+ </own_tool_level>
+ <console_output description="Selector to specify the console output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </console_output>
+ <log_file_output description="Selector to specify the log file output ('mode_0': Off, 'mode_1': only out/err/warn, 'mode_2': 1 + info, 'mode_3': 2 + debug)">
+ <value>mode_1</value>
+ </log_file_output>
+ <plot_output description="Specify the way plotting shall be handled">
+ <enable description="Switch to enable plotting ('true': On, 'false': Off)">
+ <value>true</value>
+ </enable>
+ <copy_plotting_files description="Switch if plotting files shall be copied ('true': On, 'false': Off)">
+ <value>true</value>
+ </copy_plotting_files>
+ <delete_plotting_files_from_tool_folder description="Switch if plotting files shall be deleted from folder ('true': On, 'false': Off)">
+ <value>true</value>
+ </delete_plotting_files_from_tool_folder>
+ </plot_output>
+ <report_output description="Switch to generate an HTML report ('true': On, 'false': Off)">
+ <value>true</value>
+ </report_output>
+ <tex_report description="Switch to generate a Tex report ('true': On, 'false': Off)">
+ <value>true</value>
+ </tex_report>
+ <write_info_files description="Switch to generate info files ('true': On, 'false': Off)">
+ <value>false</value>
+ </write_info_files>
+ <gnuplot_script description="Specify the name of the plot file">
+ <value>TOOLNAME_plot.plt</value>
+ </gnuplot_script>
+ <log_file description="Specify the name of the log file">
+ <value>wing_design.log</value>
+ </log_file>
+ <inkscape_path description="Path to the inkscape application ('DEFAULT': Use inkscape from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </inkscape_path>
+ <gnuplot_path description="Path to the gnuplot application ('DEFAULT': Use gnuplot from the UNICADO repo structure)">
+ <value>DEFAULT</value>
+ </gnuplot_path>
+ </control_settings>
+ <program_settings>
+ <modes description="mode selection">
+ <design_mode description="selector mode_0: design, mode_1: redesign (axml must hold a wing)">
+ <value>mode_0</value>
+ </design_mode>
+ </modes>
+ <tube_and_wing description="settings for tube and wing (TAW)">
+ <wing_configuration description="selector mode_0: cantilever">
+ <value>mode_0</value>
+ </wing_configuration>
+ <cantilever description="cantilever design information">
+ <calculation_methods description="calculation methods for specific parameter">
+ <wing_area description="wing area calculation method">
+ <method description="selector mode_0: user_defined, mode_1: by_loading_and_mtom">
+ <value>mode_1</value>
+ </method>
+ <parameters>
+ <mode_0 description="user_defined">
+ <wing_area description="wing area">
+ <value>126.34</value>
+ <unit>m^2</unit>
+ <lower_boundary>50.0</lower_boundary>
+ <upper_boundary>5000.0</upper_boundary>
+ </wing_area>
+ </mode_0>
+ </parameters>
+ </wing_area>
+ <sweep description="sweep calculation method">
+ <method description="selector mode_0: user_defined, mode_1: drag_divergence">
+ <value>mode_0</value>
+ </method>
+ <parameters description="sweep method parameters">
+ <mode_0 description="user_defined">
+ <sweep_angle description="sweep angle at quarter chord">
+ <value>25</value>
+ <unit>deg</unit>
+ <lower_boundary>-60</lower_boundary>
+ <upper_boundary>60</upper_boundary>
+ </sweep_angle>
+ </mode_0>
+ <mode_1 description="drag_divergence">
+ <korn_technology_factor description="technology factor">
+ <value>0.96</value>
+ <unit>1</unit>
+ <lower_boundary>0.85</lower_boundary>
+ <upper_boundary>0.96</upper_boundary>
+ </korn_technology_factor>
+ <delta_drag_divergence_to_mach_design description="offset between mach design and drag divergence">
+ <value>0.02</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>0.03</upper_boundary>
+ </delta_drag_divergence_to_mach_design>
+ </mode_1>
+ </parameters>
+ </sweep>
+ <taper_ratio description="taper ratio calculation method">
+ <method description="selector mode_0: user_defined, mode_1: howe">
+ <value>mode_1</value>
+ </method>
+ <parameters>
+ <mode_0 description="user_defined">
+ <taper_ratio description="taper ratio of overall wing">
+ <value>0.17</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </taper_ratio>
+ </mode_0>
+ </parameters>
+ </taper_ratio>
+ <dihedral description="dihedral calculation method">
+ <method description="selector mode_0: user_defined, mode_1: by_wing_position_and_quarter_chord_sweep">
+ <value>mode_1</value>
+ </method>
+ <parameters description="parameters for methods">
+ <mode_0 description="user_defined">
+ <dihedral_angle description="dihedral angle">
+ <value>4</value>
+ <unit>deg</unit>
+ <lower_boundary>-20</lower_boundary>
+ <upper_boundary>20</upper_boundary>
+ </dihedral_angle>
+ </mode_0>
+ <mode_1 description="by_wing_position_and_quarter_chord_sweep">
+ <dihedral_limitation description="selector mode_0: raymer, mode_1: howe">
+ <value>mode_0</value>
+ </dihedral_limitation>
+ </mode_1>
+ </parameters>
+ </dihedral>
+ <aspect_ratio description="aspect ratio calculation method">
+ <method description="selector mode_0: user_defined, mode_1: by_pitch_up_limit_function">
+ <value>mode_1</value>
+ </method>
+ <parameters description="Mode parameters">
+ <mode_0 description="user_defined">
+ <aspect_ratio description="user aspect ratio">
+ <value>11.0</value>
+ <unit>1</unit>
+ <lower_boundary>6</lower_boundary>
+ <upper_boundary>15</upper_boundary>
+ </aspect_ratio>
+ </mode_0>
+ </parameters>
+ </aspect_ratio>
+ <relative_kink_position description="relative kink position method">
+ <method description="selector mode_0: user_defined, mode_1: based_on_landing_gear_track">
+ <value>mode_0</value>
+ </method>
+ <parameters>
+ <mode_0 description="user_defined">
+ <relative_kink_position description="relative to half span - only used if low wing and wing mounted landing gear">
+ <value>0.3</value>
+ <unit>1</unit>
+ <lower_boundary>0.25</lower_boundary>
+ <upper_boundary>0.38</upper_boundary>
+ </relative_kink_position>
+ <maximum_inner_trailing_edge_sweep description="maximum inner trailing edge sweep - sets maximum possible inner trailing edge sweep">
+ <value>10.0</value>
+ <unit>deg</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>20.0</upper_boundary>
+ </maximum_inner_trailing_edge_sweep>
+ </mode_0>
+ <mode_1>
+ <initial_relative_kink_position description="relative to half span - only used if low wing and wing mounted landing gear - initial value -> will change over iteration">
+ <value>0.3</value>
+ <unit>1</unit>
+ <lower_boundary>0.25</lower_boundary>
+ <upper_boundary>0.38</upper_boundary>
+ </initial_relative_kink_position>
+ <maximum_inner_trailing_edge_sweep description="maximum inner trailing edge sweep - sets maximum possible inner trailing edge sweep">
+ <value>10.0</value>
+ <unit>deg</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>20.0</upper_boundary>
+ </maximum_inner_trailing_edge_sweep>
+ </mode_1>
+ </parameters>
+ </relative_kink_position>
+ <wing_profile_and_thickness_distribution description="wing profile calculation methods">
+ <method description="selector mode_0: user_defined, mode_1: torenbeek_jenkinson">
+ <value>mode_1</value>
+ </method>
+ <parameters description="wing profile parameters">
+ <mode_0 description="user_defined - thickness to chord ratio's must be from root to tip - linear interpolation">
+ <wing_profile_and_thickness description="wing profile and thickness at half span" ID="0">
+ <wing_profile description="wing profile">
+ <value>F15</value>
+ </wing_profile>
+ <thickness_to_chord description="Thickness to chord ratio">
+ <ratio description="thickness to chord ratio value">
+ <value>0.16</value>
+ <unit>1</unit>
+ <lower_boundary>0.05</lower_boundary>
+ <upper_boundary>0.40</upper_boundary>
+ </ratio>
+ <at_half_span description="thickness to chord ratio value at half span">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </at_half_span>
+ </thickness_to_chord>
+ </wing_profile_and_thickness>
+ <wing_profile_and_thickness description="wing profile and thickness at half span" ID="1">
+ <wing_profile description="wing profile">
+ <value>F15</value>
+ </wing_profile>
+ <thickness_to_chord description="Thickness to chord ratio">
+ <ratio description="thickness to chord ratio value">
+ <value>0.13</value>
+ <unit>1</unit>
+ <lower_boundary>0.05</lower_boundary>
+ <upper_boundary>0.40</upper_boundary>
+ </ratio>
+ <at_half_span description="thickness to chord ratio value at half span">
+ <value>0.3</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </at_half_span>
+ </thickness_to_chord>
+ </wing_profile_and_thickness>
+ <wing_profile_and_thickness description="wing profile and thickness at half span" ID="2">
+ <wing_profile description="wing profile">
+ <value>F15</value>
+ </wing_profile>
+ <thickness_to_chord description="Thickness to chord ratio">
+ <ratio description="thickness to chord ratio value">
+ <value>0.12</value>
+ <unit>1</unit>
+ <lower_boundary>0.05</lower_boundary>
+ <upper_boundary>0.40</upper_boundary>
+ </ratio>
+ <at_half_span description="thickness to chord ratio value at half span">
+ <value>0.45</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </at_half_span>
+ </thickness_to_chord>
+ </wing_profile_and_thickness>
+ <wing_profile_and_thickness description="wing profile and thickness at half span" ID="3">
+ <wing_profile description="wing profile">
+ <value>F15</value>
+ </wing_profile>
+ <thickness_to_chord description="Thickness to chord ratio">
+ <ratio description="thickness to chord ratio value">
+ <value>0.11</value>
+ <unit>1</unit>
+ <lower_boundary>0.05</lower_boundary>
+ <upper_boundary>0.40</upper_boundary>
+ </ratio>
+ <at_half_span description="thickness to chord ratio value at half span">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </at_half_span>
+ </thickness_to_chord>
+ </wing_profile_and_thickness>
+ </mode_0>
+ <mode_1 description="torenbeek_jenkinson">
+ <wing_profile description="wing profile">
+ <value>F15</value>
+ </wing_profile>
+ <max_thickness_to_chord_ratio description="maximum thickness to chord ratio - will be applied at root inner wing">
+ <value>0.15</value>
+ <unit>1</unit>
+ <lower_boundary>0.10</lower_boundary>
+ <upper_boundary>0.40</upper_boundary>
+ </max_thickness_to_chord_ratio>
+ <airfoil_critical_factor description="factor to describe technology factor of airfoil - conventional 1.0, high speed 1960-1970 technology (peaky) airfoils 1.05, supercritical airfoils 1.12 - 1.15">
+ <value>1.12</value>
+ <unit>1</unit>
+ <lower_boundary>1.0</lower_boundary>
+ <upper_boundary>1.15</upper_boundary>
+ </airfoil_critical_factor>
+ </mode_1>
+ </parameters>
+ </wing_profile_and_thickness_distribution>
+ <mass description="mass calculation methods">
+ <method description="selector mode_0: flops, mode_1: chiozzotto_wer">
+ <value>mode_0</value>
+ </method>
+ <parameters>
+ <mode_0 description="flops">
+ <fstrt description="wing strut bracing factor from 0.0 (no strut) to 1.0 (full benefit from strut bracing)">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </fstrt>
+ <faert description="aeroelastic tailoring factor from 0.0 (no tailoring) to 1.0 (maximum tailoring)">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </faert>
+ <fcomp description="composite utilization factor from 0.0 (no composites) to 1.0 (maximum use of composites)">
+ <value>0.5</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </fcomp>
+ </mode_0>
+ <mode_1 description="chiozzotto_wer">
+ <technology_factor description="technology factor for wing mass: factor below 1 -> higher technology level (less weight), factor above 1 lower technology level (higher weight)">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.7</lower_boundary>
+ <upper_boundary>1.3</upper_boundary>
+ </technology_factor>
+ <material description="material options: AL (Aluminium), CFRP (Carbon fiber reinforced plastic)">
+ <value>AL</value>
+ </material>
+ </mode_1>
+ </parameters>
+ </mass>
+ <control_devices description="control devices calculation method">
+ <method description="selector mode_0: user_defined, mode_1: empirical">
+ <value>mode_1</value>
+ </method>
+ <parameters description="control device method parameters">
+ <mode_0 description="user_defined parameters">
+ <control_device ID="0" description="control device">
+ <type description="control device type - aileron, rudder, elevator, slat, ...">
+ <value>aileron</value>
+ </type>
+ <deflection description="maximum positive and negative deflection of control device">
+ <full_negative_deflection description="full negative deflection">
+ <value>-25.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>25.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ <position description="chord relative position of control device">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.8</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>0.95</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.8</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </control_device>
+ <control_device ID="1" description="control device">
+ <type description="control device type - aileron, rudder, elevator, slat, ...">
+ <value>slat</value>
+ </type>
+ <deflection description="maximum positive and negative deflection of control device">
+ <full_negative_deflection description="full negative deflection">
+ <value>-25.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>0.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ <position description="chord relative position of control device">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>0.9</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </control_device>
+ <control_device ID="2" description="control device">
+ <type description="control device type - aileron, rudder, elevator, slat, ...">
+ <value>fowler</value>
+ </type>
+ <deflection description="maximum positive and negative deflection of control device">
+ <full_negative_deflection description="full negative deflection">
+ <value>0.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>25.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ <position description="chord relative position of control device">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.8</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.8</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </control_device>
+ <control_device ID="3" description="control device">
+ <type description="control device type - aileron, rudder, elevator, slat, ...">
+ <value>spoiler</value>
+ </type>
+ <deflection description="maximum positive and negative deflection of control device">
+ <full_negative_deflection description="full negative deflection">
+ <value>0.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>10.0</value>
+ <unit>deg</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ <position description="chord relative position of control device">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.8</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>0.65</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.65</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.8</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </control_device>
+ </mode_0>
+ <mode_1 description="empirical parameters">
+ <high_lift_device_type_leading_edge description="slat, krueger, droop_nose, morphing_droop_nose">
+ <value>slat</value>
+ </high_lift_device_type_leading_edge>
+ <high_lift_device_type_trailing_edge description="flaperon, droop_aileron, flap_plain, flap_fowler, flap_fowler_double_slotted, flap_fowler_triple_slotted">
+ <value>flap_fowler</value>
+ </high_lift_device_type_trailing_edge>
+ </mode_1>
+ </parameters>
+ </control_devices>
+ <spars description="spars calculation method">
+ <method description="selector mode_0: user_defined">
+ <value>mode_0</value>
+ </method>
+ <parameters description="spars method parameters">
+ <mode_0 description="user_defined parameters">
+ <spar ID="0" description="component spar">
+ <name description="name of spar">
+ <value>front_spar</value>
+ </name>
+ <position description="chord relative position of spar">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>1.</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </spar>
+ <spar ID="1" description="component spar">
+ <name description="name of spar">
+ <value>rear_spar</value>
+ </name>
+ <position description="chord relative position of spar">
+ <inner_position description="relative inner position">
+ <spanwise description="relative spanwise position">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <spanwise description="relative spanwise position">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </spanwise>
+ <chord description="control device chord position">
+ <from description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </to>
+ </chord>
+ </outer_position>
+ </position>
+ </spar>
+ </mode_0>
+ </parameters>
+ </spars>
+ </calculation_methods>
+ </cantilever>
+ </tube_and_wing>
+ <blended_wing_body>
+ <fidelity_selection description="selection of fidelity level">
+ <value>low</value>
+ </fidelity_selection>
+ <low_fidelity>
+ </low_fidelity>
+ </blended_wing_body>
+ </program_settings>
+</module_configuration_file>
\ No newline at end of file
diff --git a/UnicadoGUI/Frontend/.npmrc b/UnicadoGUI/Frontend/.npmrc
new file mode 100644
index 0000000..b6f27f1
--- /dev/null
+++ b/UnicadoGUI/Frontend/.npmrc
@@ -0,0 +1 @@
+engine-strict=true
diff --git a/UnicadoGUI/Frontend/README.md b/UnicadoGUI/Frontend/README.md
new file mode 100644
index 0000000..5ce6766
--- /dev/null
+++ b/UnicadoGUI/Frontend/README.md
@@ -0,0 +1,38 @@
+# create-svelte
+
+Everything you need to build a Svelte project, powered by [`create-svelte`](https://github.com/sveltejs/kit/tree/main/packages/create-svelte).
+
+## Creating a project
+
+If you're seeing this, you've probably already done this step. Congrats!
+
+```bash
+# create a new project in the current directory
+npm create svelte@latest
+
+# create a new project in my-app
+npm create svelte@latest my-app
+```
+
+## Developing
+
+Once you've created a project and installed dependencies with `npm install` (or `pnpm install` or `yarn`), start a development server:
+
+```bash
+npm run dev
+
+# or start the server and open the app in a new browser tab
+npm run dev -- --open
+```
+
+## Building
+
+To create a production version of your app:
+
+```bash
+npm run build
+```
+
+You can preview the production build with `npm run preview`.
+
+> To deploy your app, you may need to install an [adapter](https://kit.svelte.dev/docs/adapters) for your target environment.
diff --git a/UnicadoGUI/Frontend/package-lock.json b/UnicadoGUI/Frontend/package-lock.json
new file mode 100644
index 0000000..b61a62d
--- /dev/null
+++ b/UnicadoGUI/Frontend/package-lock.json
@@ -0,0 +1,2244 @@
+{
+ "name": "unicadowebapp",
+ "version": "0.0.1",
+ "lockfileVersion": 3,
+ "requires": true,
+ "packages": {
+ "": {
+ "name": "unicadowebapp",
+ "version": "0.0.1",
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+ "layercake": "^8.0.2",
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+ "svelte-drag-drop-touch": "^0.1.9",
+ "svelte-sortable-flat-list-view": "^1.0.0"
+ },
+ "devDependencies": {
+ "@sveltejs/adapter-auto": "^3.0.0",
+ "@sveltejs/kit": "^2.0.0",
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+ "svelte": "^4.2.10",
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+ }
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+ },
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+ "funding": {
+ "url": "https://github.com/vitejs/vite?sponsor=1"
+ },
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+ "fsevents": "~2.3.3"
+ },
+ "peerDependencies": {
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+ "less": "*",
+ "lightningcss": "^1.21.0",
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+ "dev": true,
+ "peerDependencies": {
+ "vite": "^3.0.0 || ^4.0.0 || ^5.0.0"
+ },
+ "peerDependenciesMeta": {
+ "vite": {
+ "optional": true
+ }
+ }
+ },
+ "node_modules/wrappy": {
+ "version": "1.0.2",
+ "resolved": "https://registry.npmjs.org/wrappy/-/wrappy-1.0.2.tgz",
+ "integrity": "sha512-l4Sp/DRseor9wL6EvV2+TuQn63dMkPjZ/sp9XkghTEbV9KlPS1xUsZ3u7/IQO4wxtcFB4bgpQPRcR3QCvezPcQ==",
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+ }
+}
diff --git a/UnicadoGUI/Frontend/package.json b/UnicadoGUI/Frontend/package.json
new file mode 100644
index 0000000..af5e6bb
--- /dev/null
+++ b/UnicadoGUI/Frontend/package.json
@@ -0,0 +1,32 @@
+{
+ "name": "unicadowebapp",
+ "version": "0.0.1",
+ "private": true,
+ "scripts": {
+ "dev": "vite dev",
+ "build": "vite build",
+ "preview": "vite preview",
+ "check": "svelte-kit sync && svelte-check --tsconfig ./tsconfig.json",
+ "check:watch": "svelte-kit sync && svelte-check --tsconfig ./tsconfig.json --watch"
+ },
+ "devDependencies": {
+ "@sveltejs/adapter-auto": "^3.0.0",
+ "@sveltejs/kit": "^2.0.0",
+ "@sveltejs/vite-plugin-svelte": "^3.0.0",
+ "svelte": "^4.2.10",
+ "svelte-check": "^3.6.0",
+ "tslib": "^2.4.1",
+ "typescript": "^5.0.0",
+ "vite": "^5.0.3"
+ },
+ "type": "module",
+ "dependencies": {
+ "@rollup/plugin-dsv": "^3.0.2",
+ "@sveltestrap/sveltestrap": "^6.2.4",
+ "layercake": "^8.0.2",
+ "svelte-chartjs": "^3.1.5",
+ "svelte-drag-and-drop-actions": "^1.0.2",
+ "svelte-drag-drop-touch": "^0.1.9",
+ "svelte-sortable-flat-list-view": "^1.0.0"
+ }
+}
diff --git a/UnicadoGUI/Frontend/src/app.d.ts b/UnicadoGUI/Frontend/src/app.d.ts
new file mode 100644
index 0000000..743f07b
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/app.d.ts
@@ -0,0 +1,13 @@
+// See https://kit.svelte.dev/docs/types#app
+// for information about these interfaces
+declare global {
+ namespace App {
+ // interface Error {}
+ // interface Locals {}
+ // interface PageData {}
+ // interface PageState {}
+ // interface Platform {}
+ }
+}
+
+export {};
diff --git a/UnicadoGUI/Frontend/src/app.html b/UnicadoGUI/Frontend/src/app.html
new file mode 100644
index 0000000..77a5ff5
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/app.html
@@ -0,0 +1,12 @@
+<!doctype html>
+<html lang="en">
+ <head>
+ <meta charset="utf-8" />
+ <link rel="icon" href="%sveltekit.assets%/favicon.png" />
+ <meta name="viewport" content="width=device-width, initial-scale=1" />
+ %sveltekit.head%
+ </head>
+ <body data-sveltekit-preload-data="hover">
+ <div style="display: contents">%sveltekit.body%</div>
+ </body>
+</html>
diff --git a/UnicadoGUI/Frontend/src/global.d.ts b/UnicadoGUI/Frontend/src/global.d.ts
new file mode 100644
index 0000000..7c46b1e
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/global.d.ts
@@ -0,0 +1,3 @@
+/// <reference types="@sveltejs/kit" />
+
+declare module '*.csv';
diff --git a/UnicadoGUI/Frontend/src/lib/index.ts b/UnicadoGUI/Frontend/src/lib/index.ts
new file mode 100644
index 0000000..856f2b6
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/lib/index.ts
@@ -0,0 +1 @@
+// place files you want to import through the `$lib` alias in this folder.
diff --git a/UnicadoGUI/Frontend/src/routes/+layout.svelte b/UnicadoGUI/Frontend/src/routes/+layout.svelte
new file mode 100644
index 0000000..924aa6c
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/routes/+layout.svelte
@@ -0,0 +1,73 @@
+<script lang="ts">
+ import {Container, Image, Row, Styles, Col, Nav, NavItem, NavLink, Icon} from '@sveltestrap/sveltestrap';
+</script>
+<Container fluid>
+ <Row class="flex-nowrap">
+ <Col class="auto col-md-3 col-xl-2 px-sm-2 px-0 bg-dark" style="position: fixed">
+ <div class="d-flex flex-column align-items-center align-items-sm-start px-3 pt-2 text-white min-vh-100">
+ <a href="/" class="d-flex align-items-center pb-3 mb-md-0 me-md-auto text-white text-decoration-none">
+ <Image fluid alt="" src="./favicon.png" style="max-width:20%;padding-right: 10px"/>
+ <span class="fs-2 d-none d-sm-inline">Unicado</span>
+ </a>
+ <Nav class="nav-pills flex-column mb-sm-auto mb-0 align-items-center align-items-sm-start " id="menu">
+ <NavItem>
+ <NavLink href="/" class="align-middle px-0 text-light">
+ <Icon name="house"></Icon>
+ <span class="ms-1 d-none d-sm-inline">Home</span>
+ </NavLink>
+ </NavItem>
+ <NavItem>
+ <NavLink href="/model" class="align-middle px-0 text-light">
+ <Icon name="airplane"></Icon>
+ <span class="ms-1 d-none d-sm-inline">Aircraft Projects</span>
+ </NavLink>
+ </NavItem>
+ <NavItem>
+ <NavLink href="/graphs" class="align-middle px-0 text-light">
+ <Icon name="graph-down"></Icon>
+ <span class="ms-1 d-none d-sm-inline">Graphs</span>
+ </NavLink>
+ </NavItem>
+ <NavItem>
+ <NavLink href="/reports" class="align-middle px-0 text-light">
+ <Icon name="journal-richtext"></Icon>
+ <span class="ms-1 d-none d-sm-inline">Reports</span>
+ </NavLink>
+ </NavItem>
+ <NavItem>
+ <NavLink href="/logs" class="align-middle px-0 text-light">
+ <Icon name="card-text"></Icon>
+ <span class="ms-1 d-none d-sm-inline">Logs</span>
+ </NavLink>
+ </NavItem>
+ <NavItem>
+ <NavLink href="/settings" class="align-middle px-0 text-light">
+ <Icon name="gear"></Icon>
+ <span class="ms-1 d-none d-sm-inline">Settings</span>
+ </NavLink>
+ </NavItem>
+ </Nav>
+ <hr>
+ <Nav class="pb-4" style="width: 100%; display: flex; justify-content: space-between">
+ <NavItem>
+ <NavLink href="/" class="align-middle text-light">
+ <Icon name="box-arrow-in-right"></Icon>
+ <span class="ms-1 d-none d-sm-inline">Login</span>
+ </NavLink>
+ </NavItem>
+ <NavItem>
+ <NavLink href="/" class="align-middle text-light">
+ <Icon name="question-circle"></Icon>
+ <span class="ms-1 d-none d-sm-inline">Help</span>
+ </NavLink>
+ </NavItem>
+ </Nav>
+ </div>
+ </Col>
+ <Col class="py-3" style="margin-left: 18%">
+ <slot></slot>
+ </Col>
+ </Row>
+</Container>
+
+<Styles/>
diff --git a/UnicadoGUI/Frontend/src/routes/+page.svelte b/UnicadoGUI/Frontend/src/routes/+page.svelte
new file mode 100644
index 0000000..d10b460
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/routes/+page.svelte
@@ -0,0 +1,8 @@
+<script>
+ import {Styles} from "@sveltestrap/sveltestrap";
+</script>
+<h1>Welcome to the UNICADO WebApp</h1>
+
+<p>Create new Project....<br>Open existing Project...</p>
+
+<Styles/>
\ No newline at end of file
diff --git a/UnicadoGUI/Frontend/src/routes/graphs/+page.svelte b/UnicadoGUI/Frontend/src/routes/graphs/+page.svelte
new file mode 100644
index 0000000..89817bf
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/routes/graphs/+page.svelte
@@ -0,0 +1,48 @@
+<script>
+ //Dummy Page
+
+ import {Styles} from "@sveltestrap/sveltestrap";
+ import { LayerCake, Svg } from 'layercake';
+
+ import Line from './_components/Line.svelte';
+ import Area from './_components/Area.svelte';
+ import AxisX from './_components/AxisX.svelte';
+ import AxisY from './_components/AxisY.svelte';
+
+ import points from './_data/points.csv';
+
+ const xKey = 'myX';
+ const yKey = 'myY';
+
+ points.forEach((/** @type {{ [columnName: string]: number; }} */ row) => {
+ row[yKey] = +row[yKey];
+ });
+
+</script>
+<h1>Welcome to the UNICADO WebApp</h1>
+<div class="chart-container">
+ <LayerCake
+ padding={{ right: 10, bottom: 20, left: 25 }}
+ x={xKey}
+ y={yKey}
+ yDomain={[0, null]}
+ data={points}
+ debug={true}
+ >
+ <Svg>
+ <AxisX />
+ <AxisY />
+ <Line />
+ <Area />
+ </Svg>
+ </LayerCake>
+</div>
+
+<Styles/>
+<style>
+ .chart-container {
+ width: 80%;
+ height: 80vh;
+ margin: 25px auto;
+ }
+</style>
\ No newline at end of file
diff --git a/UnicadoGUI/Frontend/src/routes/logs/+page.svelte b/UnicadoGUI/Frontend/src/routes/logs/+page.svelte
new file mode 100644
index 0000000..4882b2a
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/routes/logs/+page.svelte
@@ -0,0 +1,40 @@
+<script>
+ //Testpage to show logs
+
+ import {Container, Styles, TabContent, TabPane} from "@sveltestrap/sveltestrap";
+ import {onMount} from "svelte";
+ let tabs = ["convergenceLoop", "calculatePolar","createMissionXML","empennageSizing","engineSizing","fuselageDesign","initialSizing","landingGearDesign","propulsionIntegration","wingDesign"]
+ let dict = {}
+ onMount(async ()=>{
+ for (const element of tabs) {
+ const res = await fetch("http://127.0.0.1:8000/log/"+element+".log",{ cache: "no-cache" });
+ await res.text().then(function (text) {
+ let lineBreak = "\n";
+ text = text.split(lineBreak).reverse().join(lineBreak);
+ dict[element]= text;
+ });
+ }
+ })
+</script>
+<TabContent vertical pills>
+ {#each tabs as tab}
+ {#if tab =="convergenceLoop"}
+ <TabPane tabId="{tab}" tab={tab} active>
+ <Container md>
+ <p style="white-space: pre-line">
+ {dict[tab]}
+ </p>
+ </Container>
+ </TabPane>
+ {:else}
+ <TabPane tabId={tab} tab={tab}>
+ <Container md>
+ <p style="white-space: pre-line">
+ {dict[tab]}
+ </p>
+ </Container>
+ </TabPane>
+ {/if}
+ {/each}
+</TabContent>
+<Styles/>
\ No newline at end of file
diff --git a/UnicadoGUI/Frontend/src/routes/model/+page.svelte b/UnicadoGUI/Frontend/src/routes/model/+page.svelte
new file mode 100644
index 0000000..bf0d19b
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/routes/model/+page.svelte
@@ -0,0 +1,618 @@
+<script lang="ts">
+ //Prototyp Page for a modular Simulationmodelpage
+
+ import {
+ Alert,
+ Button,
+ ButtonGroup,
+ Col,
+ Container, Form, FormGroup,
+ Icon, Input, InputGroup, InputGroupText, Label,
+ ListGroup,
+ ListGroupItem, Modal, ModalBody, ModalFooter, ModalHeader,
+ Row,
+ Styles, Tooltip
+ } from "@sveltestrap/sveltestrap";
+ import {onMount} from "svelte";
+ import InPlaceEdit from './InPlaceEdit.svelte';
+
+ //Interface for Ui-elements in module settings and it's implementations
+ interface SettingsUi {
+ type: string;
+ label: string;
+ description: string;
+ bind: string;
+ }
+
+ class SettingsSwitch implements SettingsUi {
+ readonly type = "switch";
+ label: string;
+ description: string;
+ bind: string;
+
+ constructor(label: string, description: string, bind: string) {
+ this.bind = bind;
+ this.label = label;
+ this.description = description;
+ }
+ }
+
+ class SettingsSelector implements SettingsUi {
+ readonly type = "selector";
+ label: string;
+ description: string;
+ bind: string;
+ options: string[];
+
+ constructor(label: string, description: string, bind: string, options: string[]) {
+ this.bind = bind;
+ this.label = label;
+ this.description = description;
+ this.options = options;
+ }
+ }
+
+ class SettingsTextfield implements SettingsUi {
+ readonly type = "textfield";
+ label: string;
+ description: string;
+ bind: string;
+ input: string;
+
+ constructor(label: string, description: string, bind: string, input: string) {
+ this.bind = bind;
+ this.label = label;
+ this.description = description;
+ this.input = input;
+ }
+ }
+
+ class SettingsNumberfield implements SettingsUi {
+ readonly type = "numberfield";
+ label: string;
+ description: string;
+ bind: string;
+ unit: string = '-';
+ max: number = Number.POSITIVE_INFINITY;
+ min: number = Number.NEGATIVE_INFINITY;
+
+ constructor(label: string, description: string, bind: string) {
+ this.bind = bind;
+ this.label = label;
+ this.description = description;
+ }
+ setMax(max:number){
+ this.max=max;
+ }
+ setMin(min:number){
+ this.min=min;
+ }
+ setUnit(unit:string){
+ this.unit=unit;
+ }
+ }
+
+ class SettingsLabel {
+ readonly type = "label";
+ label: string;
+
+ constructor(label: string) {
+ this.label = label;
+ }
+ }
+
+ //template for datatype of dictionaries, only to avoid errors in Typescript
+ type dictionary = {
+ [key: string]: any
+ }
+
+ /* Dictionary with information of the module
+ * including the json response and the settings elements it needs to implement in the dom
+ */
+ let modalModule: dictionary = {
+ name: '',
+ response: {},
+ html: []
+ }
+
+ //Class for a group of modules
+ class group {
+ name: string;
+ loop: string = 'true';
+ loopsize: number;
+ modules: string[] = [];
+
+ constructor(name: string, loopsize: number) {
+ this.name = name;
+ this.loopsize = loopsize;
+ }
+ }
+
+ //Index for drag and drop
+ let dropIndex: number | null = null;
+
+ //Flag for changes in simulation model by the user
+ let changed = false;
+
+ //Flag for Alarm which is invoked by changes
+ let saveAlert = false;
+
+ //Flag for changes in settings modal by the user
+ let modalChanged: boolean = false;
+
+ //Array of all the groups of the model
+ let groups: group[] = [];
+
+ //Array of available modules to choose
+ let modules: string[] = [];
+
+ //Variables and Methods for modals
+ let open: boolean = false;
+ let loopOpen: boolean = false;
+ let modulesModalOpen: boolean = false;
+ let modulesModalIndex: number;
+ const toggle = () => (open = !open);
+ const toggleModules = () => (modulesModalOpen = !modulesModalOpen);
+ const toggleLoop = () => (loopOpen = !loopOpen);
+
+ onMount(async () => {
+ await loadAvailableModules();
+ await loadModel();
+ })
+
+ //Function for loading list of available modules from server
+ async function loadAvailableModules() {
+ //transitionally reading from convergenceloop_conf.xml
+ //TO-DO: replace with something more recent
+ const res = await fetch("http://127.0.0.1:8000//modules/selection");
+ const data = await res.json();
+ modules = data['availableModules'];
+ modules = Array.from(new Set(modules));
+ modules.sort();
+ }
+
+ //Function for loading the recent saved model from server
+ async function loadModel() {
+ const res = await fetch("http://127.0.0.1:8000/modules");
+ const data = await res.json();
+ groups = data["groups"];
+ changed = false;
+ changed = changed;
+ saveAlert = false;
+ saveAlert = saveAlert;
+ }
+
+ async function startModel() {
+ //dummy-Function
+ }
+
+ //Function to save model on the server
+ async function uploadModel() {
+ const response = await fetch('http://127.0.0.1:8000/modules/update', {
+ method: 'PUT',
+ body: JSON.stringify({groups}),
+ headers: {
+ 'content-type': 'application/json'
+ }
+ })
+ .then(response => response.json())
+ changed = false;
+ changed = changed;
+ saveAlert = false;
+ saveAlert = saveAlert;
+ }
+
+ //Function for loading the selected settings xml config and show it on the DOM
+ async function getModuleConf(module: string) {
+ //TO-DO: Implementation for editing xml files in an unknown format
+ try {
+ const res = await fetch(`http://127.0.0.1:8000/modules/${module}/config`);
+ const data = await res.json();
+ modalModule.name = module;
+ modalModule.response = JSON.parse(data);
+ modalModule.html = [];
+ modalModule = modalModule;
+ generateHTML(modalModule.response);
+ modalChanged = false;
+ modalChanged = modalChanged;
+ modalModule = modalModule;
+ } catch (error) {
+ console.error(error);
+ modalModule.name = "no";
+ modalModule.response = {};
+ modalModule.html = [];
+ modalModule.html.push(new SettingsLabel("No config found!"));
+ }
+ }
+
+ //Wrapper to give Click-Event handler a synchronous Output
+ function getModuleConfClickWrapper(item: string) {
+ getModuleConf(item).catch(console.error);
+ return (event: MouseEvent & { currentTarget: EventTarget & HTMLLIElement }) => {
+ toggle();
+ loadAvailableModules().catch(console.error);
+ getModuleConf(item).catch(console.error);
+ };
+ }
+
+ /*Parse json response to matching SettingsUi-Elements
+ * to portray it later in the DOM
+ * recursive Function
+ * */
+ function generateHTML(json: dictionary) {
+ Object.entries(json).forEach(([key, value]) => {
+ if (value == null) {
+ return
+ }
+ if (value.hasOwnProperty("value")) {
+ if (value["@description"] && value["@description"].toLowerCase().includes("switch")) {
+ value.value = (value.value === 'true' || value.value === "1") //transform string input to boolean for easier binding
+ modalModule.html.push(new SettingsSwitch(key, value["@description"], value))
+ } else if (value["@description"] && value["@description"].toLowerCase().includes("selector")) {
+ let options = [];
+ for (let i = 0; i < 5; i++) {
+ if (value["@description"].includes("mode_" + i)) {
+ options.push("mode_" + i)
+ }
+ }
+ modalModule.html.push(new SettingsSelector(key, value["@description"], value, options))
+ }else if(isNumber(value.value)){
+ value.value=parseFloat(value.value);
+ let numberField = new SettingsNumberfield(key, value["@description"], value)
+ if(value.hasOwnProperty('lower_boundary')&&isNumber(value['lower_boundary'])){numberField.setMin(value['lower_boundary'])}
+ if(value.hasOwnProperty('upper_boundary')&&isNumber(value['upper_boundary'])){numberField.setMax(value['upper_boundary'])}
+ if(value.hasOwnProperty("@unit")){numberField.setUnit(value["@unit"])}//spaeter entweder unit oder Unit in XML
+ if(value.hasOwnProperty("@Unit")){numberField.setUnit(value["@Unit"])}
+ if(value.hasOwnProperty("unit")){numberField.setUnit(value["unit"])}
+ if(value.hasOwnProperty("Unit")){numberField.setUnit(value["Unit"])}
+ modalModule.html.push(numberField);
+ } else {
+ modalModule.html.push(new SettingsTextfield(key, value["@description"], value, key))
+ }
+ } else if (typeof value === "object") {
+ modalModule.html.push(new SettingsLabel(key))
+ generateHTML(json[key])
+ } else {
+ return;
+ }
+ })
+ }
+
+ //Save Settings of Module to Server
+ async function uploadModuleConf() {
+ const response = await fetch('http://127.0.0.1:8000/modules/config/update', {
+ method: 'PUT',
+ body: JSON.stringify(modalModule.response),
+ headers: {
+ 'content-type': 'application/json'
+ }
+ })
+ .then(response => response.json())
+ modalChanged = false;
+ modalChanged = modalChanged;
+ }
+
+ //Replacing underscores to space
+ function formatLabel(label: string) {
+ return label.replaceAll("_", " ")
+ }
+
+ //check if the settings modal of a module changed
+ function checkModalChanged() {
+ modalChanged = true;
+ modalChanged = modalChanged;
+ }
+
+ //reset settings of an module
+ async function resetModuleConf() {
+ const res = await fetch(`http://127.0.0.1:8000/modules/${modalModule.name}/config/reset`);
+ getModuleConf(modalModule.name);
+ }
+
+ //Methods for drag and drop of modules
+
+ function dragStart(event: any, groupIndex: number, itemIndex: number) {
+ const data = {groupIndex, itemIndex};
+ event.dataTransfer.setData('text/plain', JSON.stringify(data));
+ }
+
+ function drop(event: any, targetGroupIndex: number) {
+ event.preventDefault();
+ const json = event.dataTransfer.getData("text/plain");
+ const data = JSON.parse(json);
+ const {groupIndex, itemIndex} = data;
+
+ const [item] = groups[data.groupIndex].modules.splice(data.itemIndex, 1);
+ groups[targetGroupIndex].modules.splice(dropIndex ?? groups[targetGroupIndex].modules.length, 0, item);
+ updateAll();
+ }
+
+ function dragOver(e: any) {
+ dropIndex = null;
+ const itemElement = e.target.closest('[data-index]');
+ if (itemElement == null)
+ return;
+ const {index} = itemElement.dataset;
+ dropIndex = index;
+ }
+
+ //update Page with new inputs
+ function updateAll() {
+ groups = groups;
+ changed = true;
+ saveAlert = true;
+ saveAlert = saveAlert;
+ changed = changed;
+ }
+
+ //Makes new group and adding it to groups
+ function addGroup() {
+ groups.push(new group("group " + groups.length, 1))
+ updateAll()
+ }
+
+ //Adding a Module to a group
+ function addModules(index: number, modulname: string) {
+ groups.at(index)?.modules.push(modulname)
+ updateAll()
+ }
+
+ //Change name of a group
+ function submitGrpName(field: number) {
+ return ({detail}: { detail: string }) => {
+ groups[field].name = detail;
+ }
+ }
+
+ //Clearing groups
+ function clearModel() {
+ groups = []
+ }
+
+ //Deleting a group
+ function deleteGroup(index: number) {
+ groups.splice(index, 1);
+ updateAll()
+ }
+
+ //Deleting a model in a group
+ function deleteModule(grpIndex: number, moduleIndex: number) {
+ groups.at(grpIndex)?.modules.splice(moduleIndex, 1);
+ updateAll()
+ }
+
+ //Copy selected group
+ function copyGroup(index: number) {
+ const newGroup = new group("copy of " + groups[index].name, groups[index].loopsize);
+ newGroup.modules = newGroup.modules.concat(groups[index].modules);
+ newGroup.loop = newGroup.loop;
+ groups.push(newGroup);
+ updateAll()
+ }
+
+ //Calculate Stepsize of number inputs from current value
+ function calcStepSize(value:number){
+ const numberString = value.toString()
+ if (!numberString.includes('.')) {
+ return 1;
+ } else {
+ const decimalPart = numberString.split('.')[1];
+ return Math.pow(10, -decimalPart.length);
+ }
+ }
+ //check if string is a number
+ function isNumber(n:string){
+ return!isNaN(parseFloat(n))&&isFinite(parseFloat(n))
+ }
+ //check if number is in boundry
+ function validateNumber(index:number){
+ console.log("validateNumber")
+ if(modalModule.html[index].bind.value<modalModule.html[index].min){
+ modalModule.html[index].bind.value=modalModule.html[index].min;
+ }else if(modalModule.html[index].bind.value>modalModule.html[index].max){
+ modalModule.html[index].bind.value=modalModule.html[index].max;
+ }
+ }
+
+</script>
+<Container>
+ <h2>Simulationsmodel</h2>
+ <Alert color="primary" isOpen={saveAlert} toggle={() => (saveAlert = false)}>
+ Changes in Model please save or reload before starting!.
+ </Alert>
+ <ButtonGroup>
+ <Button color="dark" outline on:click={addGroup}>
+ <Icon name="window-plus"/>
+ new Group
+ </Button>
+ <Button color="dark" outline on:click={clearModel}>
+ <Icon name="window-dash"/>
+ Clear
+ </Button>
+ <Button disabled color="dark" outline on:click={startModel}>
+ <Icon name="play-fill"/>
+ Start
+ </Button>
+ {#if changed}
+ <Button color="danger" outline on:click={uploadModel} active>
+ <Icon name="cloud-upload"/>
+ Save
+ </Button>
+ {:else}
+ <Button color="dark" outline on:click={uploadModel}>
+ <Icon name="cloud-upload"/>
+ Save
+ </Button>
+ {/if}
+ <Button color="dark" outline on:click={loadModel}>
+ <Icon name="cloud-download"/>
+ Load
+ </Button>
+ </ButtonGroup>
+ <Row class="py-3">
+ {#each groups as groupitem, groupIndex(groupitem)}
+ <Col>
+ <Row>
+ <h3>
+ <InPlaceEdit bind:value={groupitem.name} on:submit={submitGrpName(groupIndex)}/>
+ </h3>
+ <ButtonGroup>
+ <Button color="dark" outline on:click={()=>{modulesModalIndex=groupIndex;toggleModules()}}>
+ <Icon name="boxes"/>
+ Modules
+ </Button>
+ <Button color="dark" outline on:click={()=>{modulesModalIndex=groupIndex;toggleLoop()}}>
+ <Icon name="arrow-clockwise"/>
+ {#if groupitem.loop === 'true'}
+ {groupitem.loopsize}
+ {:else}
+ auto
+ {/if}
+ </Button>
+ <Button color="dark" outline on:click={()=>copyGroup(groupIndex)}>
+ <Icon name="copy"/>
+ </Button>
+ <Button color="dark" outline on:click={()=>deleteGroup(groupIndex)}>
+ <Icon name="trash"/>
+ </Button>
+ </ButtonGroup>
+ </Row>
+ <ul class="list-group"
+ on:drop={event=>drop(event,groupIndex)}
+ on:dragover|preventDefault={event=>dragOver(event)}>
+ {#each groupitem.modules as item, itemIndex(itemIndex)}
+ <div class="item" data-index={itemIndex}>
+ <li class="list-group-item list-group-item-action"
+ draggable="true"
+ on:dragstart={event=>dragStart(event,groupIndex,groupitem.modules.indexOf(item))}
+ on:click={getModuleConfClickWrapper(item)}>
+ {item}
+ </li>
+ </div>
+ {/each}
+ </ul>
+ </Col>
+ {/each}
+ </Row>
+ <Modal isOpen={open} toggle={toggle} scrollable>
+ <ModalHeader toggle={toggle}>{modalModule.name} settings</ModalHeader>
+ <ModalBody>
+ {#each modalModule.html as element, index}
+ {#if element.type == "switch"}
+ <Input id="uiElement{index}" type="switch" label="{formatLabel(element.label)}"
+ bind:checked={element.bind.value} on:change={()=>checkModalChanged()}/>
+ <Tooltip target="uiElement{index}" placement="left">
+ {element.description}
+ </Tooltip>
+ {:else if element.type == "label"}
+ <h3>{formatLabel(element.label)}</h3>
+ {:else if element.type == "selector"}
+ <h6>{formatLabel(element.label)}</h6>
+ <Input id="uiElement{index}" type="select" bind:value={element.bind.value}
+ on:change={()=>checkModalChanged()}>
+ {#each element.options as option}
+ <option>{option}</option>
+ {/each}
+ </Input>
+ <Tooltip target="uiElement{index}" placement="left">
+ {element.description}
+ </Tooltip>
+ {:else if element.type == "textfield"}
+ <h7>{formatLabel(element.label)}</h7>
+ <Input id="uiElement{index}" type="text" bind:value={element.bind.value}
+ on:change={()=>checkModalChanged()}/>
+ <Tooltip target="uiElement{index}" placement="left">
+ {element.description}
+ </Tooltip>
+ {:else if element.type == "numberfield"}
+ {#if element.unit != "1" && element.unit != "-" && element.unit != "count"}
+ <h7>{formatLabel(element.label)} (in {element.unit})</h7>
+ {:else}
+ <h7>{formatLabel(element.label)}</h7>
+ {/if}
+ {#if element.max != Number.POSITIVE_INFINITY && element.min != Number.NEGATIVE_INFINITY}
+ <Input type="range" min={element.min} max={element.max} step=0.01 bind:value={element.bind.value}
+ placeholder="range placeholder" on:change={()=>checkModalChanged()}/>
+ <Input id="uiElement{index}" type="number" min={element.min} max={element.max} step=0.01
+ bind:value={element.bind.value} on:change={()=>checkModalChanged()} on:blur={()=>validateNumber(index)}/>
+ {:else}
+ <Input id="uiElement{index}" type="number" min={element.min} max={element.max} step={calcStepSize(element.bind.value)}
+ bind:value={element.bind.value} on:change={()=>checkModalChanged()} on:blur={()=>validateNumber(index)}/>
+ {/if}
+
+ <Tooltip target="uiElement{index}" placement="left">
+ {element.description}
+ </Tooltip>
+ {/if}
+ {/each}
+ </ModalBody>
+ {#if modalModule.name != "no"}
+ <ModalFooter>
+ <ButtonGroup>
+ {#if modalChanged}
+ <Button color="primary" on:click={uploadModuleConf}>
+ <Icon name="floppy"/>
+ Save
+ </Button>
+ {/if}
+ <Button color="danger" on:click={resetModuleConf}>
+ <Icon name="bootstrap-reboot"/>
+ Reset to Default
+ </Button>
+ </ButtonGroup>
+ </ModalFooter>
+ {/if}
+ </Modal>
+ <Modal isOpen={modulesModalOpen} toggle={toggleModules} size = 'lg' scrollable>
+ <ModalHeader toggle={toggleModules}>Select Modules to add to {groups[modulesModalIndex].name}</ModalHeader>
+ <ModalBody>
+ <Row>
+ <Col>
+ <h6>Click to add</h6>
+ <ListGroup>
+ {#each modules as module}
+ <ListGroupItem id="{module}" tag="button" action
+ on:click={()=>addModules(modulesModalIndex,module)}>{module}</ListGroupItem>
+ {/each}
+ </ListGroup>
+ </Col>
+ <Col>
+ <h6>Current Modules in {groups[modulesModalIndex].name} (click to delete)</h6>
+ <ListGroup>
+ {#each groups[modulesModalIndex].modules as module, modulIndex(modulIndex)}
+ <ListGroupItem tag="button" action
+ on:click={()=>deleteModule(modulesModalIndex,modulIndex)}>{module}</ListGroupItem>
+ {/each}
+ </ListGroup>
+ </Col>
+ </Row>
+ </ModalBody>
+ </Modal>
+ <Modal isOpen={loopOpen} toggle={toggleLoop} scrollable>
+ <ModalHeader toggle={toggleLoop}>Loop Settings for {groups[modulesModalIndex].name}</ModalHeader>
+ <ModalBody>
+ <Form>
+ <Label>Loopkind:</Label>
+ <Input name="loop" type="radio" bind:group={groups[modulesModalIndex].loop} value="true"
+ label={"manual Loopsize"}/>
+ <Input name="loop" type="radio" bind:group={groups[modulesModalIndex].loop} value="false"
+ label={"Autoloop"}/>
+ <br>
+ {#if groups[modulesModalIndex].loop === 'true'}
+ <InputGroup size="sm">
+ <InputGroupText>Loopsize</InputGroupText>
+ <Input type="number" min={0} bind:value={groups[modulesModalIndex].loopsize}
+ placeholder={groups[modulesModalIndex].loopsize.toString()}/>
+ </InputGroup>
+ {:else}
+ <p>
+ Placeholder for Convsettings
+ </p>
+ {/if}
+
+ </Form>
+ </ModalBody>
+
+ </Modal>
+</Container>
+<Styles/>
\ No newline at end of file
diff --git a/UnicadoGUI/Frontend/src/routes/model/InPlaceEdit.svelte b/UnicadoGUI/Frontend/src/routes/model/InPlaceEdit.svelte
new file mode 100644
index 0000000..95b0b20
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/routes/model/InPlaceEdit.svelte
@@ -0,0 +1,58 @@
+<script>
+ import { createEventDispatcher, onMount } from 'svelte'
+
+ export let value, required = true
+
+ const dispatch = createEventDispatcher()
+ let editing = false, original
+
+ onMount(() => {
+ original = value
+ })
+
+ function edit() {
+ editing = true
+ }
+
+ function submit() {
+ if (value != original) {
+ dispatch('submit', value)
+ }
+
+ editing = false
+ }
+
+ function keydown(event) {
+ if (event.key == 'Escape') {
+ event.preventDefault()
+ value = original
+ editing = false
+ }
+ }
+
+ function focus(element) {
+ element.focus()
+ }
+</script>
+
+{#if editing}
+ <form on:submit|preventDefault={submit} on:keydown={keydown}>
+ <input bind:value on:blur={submit} {required} use:focus/>
+ </form>
+{:else}
+ <div on:click={edit}>
+ {value}
+ </div>
+{/if}
+
+<style>
+ input {
+ border: none;
+ background: none;
+ font-size: inherit;
+ color: inherit;
+ font-weight: inherit;
+ text-align: inherit;
+ box-shadow: none;
+ }
+</style>
\ No newline at end of file
diff --git a/UnicadoGUI/Frontend/src/routes/reports/+page.svelte b/UnicadoGUI/Frontend/src/routes/reports/+page.svelte
new file mode 100644
index 0000000..49c924a
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/routes/reports/+page.svelte
@@ -0,0 +1,37 @@
+<script>
+ //Testpage to show html report outputs
+
+ import {Container, Styles, TabContent, TabPane} from "@sveltestrap/sveltestrap";
+ import {onMount} from "svelte";
+
+ let tabs = ["convergenceLoop","empennageSizing","engineSizing","fuselageDesign","landingGearDesign","propulsionIntegration","wingDesign"]
+ let dict = {}
+ onMount(async ()=>{
+ for (const element of tabs) {
+ const res = await fetch("http://127.0.0.1:8000/report/"+element+"_report.html",{ cache: "no-cache" });
+ await res.text().then(function (html) {
+ let parser = new DOMParser();
+ let doc = parser.parseFromString(html, "text/html");
+ dict[element]= doc.querySelector('body').innerHTML;
+ });
+ }
+ })
+</script>
+<TabContent vertical pills>
+ {#each tabs as tab}
+ {#if tab =="convergenceLoop"}
+ <TabPane tabId="{tab}" tab={tab} active>
+ <Container md>
+ {@html dict[tab]}
+ </Container>
+ </TabPane>
+ {:else}
+ <TabPane tabId={tab} tab={tab}>
+ <Container md>
+ {@html dict[tab]}
+ </Container>
+ </TabPane>
+ {/if}
+ {/each}
+</TabContent>
+<Styles/>
\ No newline at end of file
diff --git a/UnicadoGUI/Frontend/src/routes/settings/+page.svelte b/UnicadoGUI/Frontend/src/routes/settings/+page.svelte
new file mode 100644
index 0000000..85503ea
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/routes/settings/+page.svelte
@@ -0,0 +1,343 @@
+<script lang="ts">
+ //Testpage to show possible look of a settingspage
+
+ import {
+ Button,
+ ButtonGroup,
+ Form,
+ FormGroup,
+ Icon,
+ Input,
+ Styles,
+ TabContent,
+ TabPane
+ } from "@sveltestrap/sveltestrap";
+ let changed = false;
+
+ class EnergyCarrier{
+ constructor(value : string, id :number) {
+ this.value = value;
+ this.id = id;
+ }
+ }
+ class Propulsor{
+ constructor(powertrain : string,type : string,position : string ,energycarrier: EnergyCarrier[],thrust_share: string) {
+ this.powertrain = powertrain;
+ this.type = type;
+ this.position = position;
+ this.energycarrier = energycarrier;
+ this.thrust_share = thrust_share;
+ }
+ }
+ //Energy Carriers
+ let kerosin = new EnergyCarrier("kerosin",1);
+ let liquid_hydrogen = new EnergyCarrier("liquid_hydrogen",2);
+ let battery = new EnergyCarrier("battery",3);
+ let saf = new EnergyCarrier("saf",4);
+
+
+ let propulsors : Propulsor[]= [];
+ let energycarriers : EnergyCarrier[]=[];
+
+ let max_load_factor= 2;
+ let min_load_factor= -1;
+ let maneuver_load_factor= 1.1;
+ let passenger_nr= 150;
+ let mass_per_passenger=80;
+ let luggage_mass_per_passenger=17;
+ let additional_cargo_mass= 500;
+ let cargo_density =165;
+ let thrust_share = 1;
+ let thickness = 0.003;
+ let maximum_structrual_payload_mass = 30000;
+ let takeoff_distance = 2122;
+ let landing_field_length = 2387;
+ let requirements ={
+ general:{
+ type: String,
+ model: String,
+ },
+ mission_files: {
+ design_mission_file: String,
+ study_mission_file: String,
+ requirements_mission_file: String,
+ },
+ design_specification:{
+ configuration: {
+ configuration_type: String,
+ fuselage_type: String,
+ mounting: String,
+ empennage_type: String,
+ undercarriage_definition:{
+ main_gear_mounting: String,
+ undercarriage_retractability: String,
+ },
+
+
+
+ },
+
+
+ }
+ }
+
+</script>
+<h1>Aircraftmodelsettings</h1>
+<ButtonGroup style="margin-bottom: 20px">
+ <Button color="dark" outline ><Icon name="bootstrap-reboot"/> Reset </Button>
+ {#if changed}
+ <Button color="danger" outline active><Icon name="cloud-upload" /> Save </Button>
+ {:else}
+ <Button color="dark" outline ><Icon name="cloud-upload" /> Save </Button>
+ {/if}
+ <Button color="dark" outline ><Icon name="cloud-download" /> Load </Button>
+</ButtonGroup>
+
+<TabContent vertical pills>
+ <TabPane tabId="general" tab="General" active>
+ <Form>
+ <h5>General aircraft information</h5>
+ <FormGroup floating label="Aircraft type">
+ <Input placeholder="Enter a value"/>
+ </FormGroup>
+ <FormGroup floating label="Model - Version">
+ <Input placeholder="Enter a value"/>
+ </FormGroup>
+
+ <h5>Name of xml files which are located in the missionData directory and contain the flight phase data</h5>
+ <FormGroup floating label="Name of the study mission xml">
+ <Input placeholder="Enter a value"/>
+ </FormGroup>
+ <FormGroup floating label="Name of the requirements mission xml">
+ <Input placeholder="Enter a value"/>
+ </FormGroup>
+ </Form>
+ </TabPane>
+ <TabPane tabId="design_specification" tab="Design Specification">
+ <Form>
+ <h5>Configuration information</h5>
+ <FormGroup floating label="Aircraft configuration">
+ <Input type="select" placeholder="Enter a value">
+ <option value="tube_and_wing">tube and wing</option>
+ <option value="blended_wing_body">blended wing body</option>
+ </Input>
+ </FormGroup>
+ <FormGroup floating label="Design description of the fuselage">
+ <Input type="select" placeholder="Enter a value">
+ <option value="single_aisle">single aisle</option>
+ <option value="weight_body">weight body</option>
+ </Input>
+ </FormGroup>
+ <FormGroup floating label="Definitions for wing design">
+ <Input type="select" placeholder="Enter a value">
+ <option value="low">low</option>
+ <option value="mid">mid</option>
+ <option value="high">high</option>
+ </Input>
+ </FormGroup>
+ <!-- <FormGroup floating label="Definitions for empennage design">-->
+ <!-- <Input type="select" placeholder="Enter a value">-->
+ <!-- <option value="low">low</option>-->
+ <!-- <option value="mid">mid</option>-->
+ <!-- </Input>-->
+ <!-- </FormGroup>-->
+
+ <h5>Design description of the undercarriage</h5>
+ <FormGroup floating label="Mounting position of the main landing gear">
+ <Input type="select" placeholder="Enter a value">
+ <option value="wing_mounted">wing mounted</option>
+ <option value="fuselage_mounted">fuselage mounted</option>
+ </Input>
+ </FormGroup>
+ <FormGroup floating label="Retractability of landing gear">
+ <Input type="select" placeholder="Enter a value">
+ <option value="retractable">retractable</option>
+ <option value="non_retractable">non retractable</option>
+ </Input>
+ </FormGroup>
+
+ <h5> Design Load information</h5>
+ <FormGroup floating label="maximum load factor">
+ <Input type="number" min={0} max={4} step={0.1} bind:value={max_load_factor} placeholder="number placeholder"/>
+ <Input type="range" min={0} max={4} step={0.1} bind:value={max_load_factor} placeholder="range placeholder"/>
+ </FormGroup>
+ <FormGroup floating label="minimum load factor">
+ <Input type="number" min={-2} max={0} step={0.1} bind:value={min_load_factor} placeholder="number placeholder"/>
+ <Input type="range" min={-2} max={0} step={0.1} bind:value={min_load_factor} placeholder="range placeholder"/>
+ </FormGroup>
+ <FormGroup floating label="standard maneuver load factor for e.g. flare">
+ <Input type="number" min={0} max={2} step={0.1} bind:value={maneuver_load_factor} placeholder="number placeholder"/>
+ <Input type="range" min={0} max={2} step={0.1} bind:value={maneuver_load_factor} placeholder="range placeholder"/>
+ </FormGroup>
+
+ <h5> Passenger definition</h5>
+ <FormGroup floating label="Number of passengers">
+ <Input type="number" min={0} step={1} bind:value={passenger_nr} placeholder="number placeholder"/>
+ </FormGroup>
+ <FormGroup floating label="Design mass of a single passenger WITHOUT luggage in kg">
+ <Input type="number" min={50} max={200} step={1} bind:value={mass_per_passenger} placeholder="number placeholder"/>
+ <Input type="range" min={50} max={200} step={1} bind:value={mass_per_passenger} placeholder="range placeholder"/>
+ </FormGroup>
+ <FormGroup floating label="Design mass of a the luggage for a single passenger in kg">
+ <Input type="number" min={0} max={25} step={1} bind:value={luggage_mass_per_passenger} placeholder="number placeholder"/>
+ <Input type="range" min={0} max={25} step={1} bind:value={luggage_mass_per_passenger} placeholder="range placeholder"/>
+ </FormGroup>
+ <h6>passenger class distro with bar and 5 classes</h6>
+
+ <h5>Cargo definition</h5>
+ <FormGroup floating label="Mass of cargo which does not belong to passengers in kg">
+ <Input type="number" min={0} max={1000} step={1} bind:value={additional_cargo_mass} placeholder="number placeholder"/>
+ <Input type="range" min={0} max={1000} step={1} bind:value={additional_cargo_mass} placeholder="range placeholder"/>
+ </FormGroup>
+ <FormGroup floating label="Density of cargo which does not belong to passengers in kg/m^3">
+ <Input type="number" min={150} max={200} step={1} bind:value={cargo_density} placeholder="number placeholder"/>
+ <Input type="range" min={150} max={200} step={1} bind:value={cargo_density} placeholder="range placeholder"/>
+ </FormGroup>
+ </Form>
+ </TabPane>
+ <TabPane tabId="requirements" tab="Requirements">
+ <Form>
+
+ </Form>
+ </TabPane>
+ <TabPane tabId="assessment_scenario" tab="Assessment Scenario">
+ <Form>
+
+ </Form>
+ </TabPane>
+</TabContent>
+<Form>
+ <h2>Requirements and Specifications</h2>
+
+
+
+ <h5>Design specification</h5>
+
+
+ <h5>Energy carriers information</h5>
+ <FormGroup floating label="ID of Energy type: kerosene / liquid_hydrogen / battery / saf (for multifuel engine create new ID)">
+ <Input type="number" placeholder="number placeholder"/>
+ </FormGroup>
+
+ <h5>Propulsion information?</h5>
+ <FormGroup floating label="Way the power is generated from the source">
+ <Input type="select" placeholder="Enter a value">
+ <option value="turbo">turbo</option>
+ <option value="electric">electric</option>
+ <option value="fuel_cell">fuel_cell</option>
+ </Input>
+ </FormGroup>
+ <FormGroup floating label="Type of main thrust generator">
+ <Input type="select" placeholder="Enter a value">
+ <option value="fan">fan</option>
+ <option value="prop">prop</option>
+ </Input>
+ </FormGroup>
+ <FormGroup floating label="position on component">
+ <Input type="select" placeholder="Enter a value">
+ <option value="wing">wing</option>
+ <option value="fuselage">fuselage</option>
+ <option value="empennage">empennage</option>
+ </Input>
+ </FormGroup>
+ <FormGroup floating label="x-position (aircraft coordinate system)">
+ <Input type="select" placeholder="Enter a value">
+ <option value="front">front</option>
+ <option value="back">back</option>
+ </Input>
+ </FormGroup>
+ <FormGroup floating label="y-position (aircraft coordinate system)">
+ <Input type="select" placeholder="Enter a value">
+ <option value="left">left</option>
+ <option value="right">right</option>
+ </Input>
+ </FormGroup>
+ <FormGroup floating label="z-position (aircraft coordinate system)">
+ <Input type="select" placeholder="Enter a value">
+ <option value="over">over</option>
+ <option value="mid">mid</option>
+ <option value="under">under</option>
+ <option value="in">in</option>
+ </Input>
+ </FormGroup>
+ <FormGroup floating label="see energy carrier specification node">
+ <Input type="number" min={0} max={5} step={1} bind:value={energycarriers} placeholder="number placeholder"/>
+ <Input type="range" min={0} max={5} step={1} bind:value={energycarriers} placeholder="range placeholder"/>
+ </FormGroup>
+ <FormGroup floating label="Share of this thrust in relation to required aircraft thrust">
+ <Input type="number" min={0} max={1} step={0.1} bind:value={thrust_share} placeholder="number placeholder"/>
+ <Input type="range" min={0} max={1} step={0.1} bind:value={thrust_share} placeholder="range placeholder"/>
+ </FormGroup>
+
+ <h5>Systems information</h5>
+ <FormGroup floating label="Way the power is generated from the source">
+ <Input type="select" placeholder="Enter a value">
+ <option value="propulsor">propulsor</option>
+ <option value="turbo">turbo</option>
+ <option value="electric">electric</option>
+ <option value="fuel_cell">fuel_cell</option>
+ </Input>
+ </FormGroup>
+ <p>dieser bereich ist verwirrend, unterkategorien?</p>
+
+ <h5>Skinning Information</h5>
+ <FormGroup floating label="Material of skinning">
+ <Input placeholder="Enter a value"/>
+ </FormGroup>
+ <FormGroup floating label="Thickness of skinning">
+ <Input type="number" min={0.0001} max={0.1} step={0.0001} bind:value={thickness} placeholder="number placeholder"/>
+ <Input type="range" min={0.0001} max={0.1} step={0.0001} bind:value={thickness} placeholder="range placeholder"/>
+ </FormGroup>
+
+ <h5>Technology</h5>
+ <Input type="switch" label="Switch if variable camber is used" />
+
+ <h5>Energy tanks information?</h5>
+ <p>energiecarrier wieder, machmal bei auswahl zahlen manchmal direkt wörter</p>
+ <FormGroup floating label="Component where the tank is located">
+ <Input type="select" placeholder="Enter a value">
+ <option value="fusalage">fusalage</option>
+ <option value="wing">wing</option>
+ <option value="horizontal_stabilizer">horizontal_stabilizer</option>
+ </Input>
+ </FormGroup>
+ <FormGroup floating label="Position of tank in location">
+ <Input type="select" placeholder="Enter a value">
+ <option value="tailcone">tailcone</option>
+ <option value="rear">rear</option>
+ <option value="front">front</option>
+ <option value="top">top</option>
+ <option value="bottom">bottom</option>
+ <option value="center">center</option>
+ <option value="inner_left">inner_left</option>
+ <option value="outer_left">outer_left</option>
+ <option value="inner_right">inner_right</option>
+ <option value="outer_right">outer_right</option>
+ <option value="total">total</option>
+ </Input>
+ </FormGroup>
+
+ <h5>Aircraft design requirements</h5>
+ <h6>TLAR</h6>
+ <FormGroup floating label="Maximum structual payload mass which can be carried by the aircraft (e.g. for short trips) in kg">
+ <Input type="number" min={100} max={150000} step={100} bind:value={maximum_structrual_payload_mass} placeholder="number placeholder"/>
+ <Input type="range" min={100} max={150000} step={100} bind:value={maximum_structrual_payload_mass} placeholder="range placeholder"/>
+ </FormGroup>
+ <FormGroup floating label="Design takeoff distance (Balanced Field Length) at Sea Level with maximum takeoff mass (MTOM) and (ISA + deltaISA)-Conditions in m">
+ <Input type="number" min={600} max={5000} step={1} bind:value={takeoff_distance} placeholder="number placeholder"/>
+ <Input type="range" min={600} max={5000} step={1} bind:value={takeoff_distance} placeholder="range placeholder"/>
+ </FormGroup>
+ <FormGroup floating label="Needed runway length at Sea Level with maximum landing mass (MLM) and (ISA + deltaISA)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6) in m">
+ <Input type="number" min={600} max={5000} step={1} bind:value={landing_field_length} placeholder="number placeholder"/>
+ <Input type="range" min={600} max={5000} step={1} bind:value={landing_field_length} placeholder="range placeholder"/>
+ </FormGroup>
+ <FormGroup floating label="ICAO reference code - code_number 1-4 (field length) + code_letter A-F (wing span limits) + faa ADG code number I-VI (wing span limits + tail height limits) + Aircraft Approach Category letter A-D">
+ <Input placeholder="Enter a value"/>
+ </FormGroup>
+ <p>mit check dass code stimmt?</p>
+
+
+</Form>
+
+
+<Styles/>
\ No newline at end of file
diff --git a/UnicadoGUI/Frontend/static/favicon.png b/UnicadoGUI/Frontend/static/favicon.png
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diff --git a/UnicadoGUI/Frontend/svelte.config.js b/UnicadoGUI/Frontend/svelte.config.js
new file mode 100644
index 0000000..2b35fe1
--- /dev/null
+++ b/UnicadoGUI/Frontend/svelte.config.js
@@ -0,0 +1,18 @@
+import adapter from '@sveltejs/adapter-auto';
+import { vitePreprocess } from '@sveltejs/vite-plugin-svelte';
+
+/** @type {import('@sveltejs/kit').Config} */
+const config = {
+ // Consult https://kit.svelte.dev/docs/integrations#preprocessors
+ // for more information about preprocessors
+ preprocess: vitePreprocess(),
+
+ kit: {
+ // adapter-auto only supports some environments, see https://kit.svelte.dev/docs/adapter-auto for a list.
+ // If your environment is not supported or you settled on a specific environment, switch out the adapter.
+ // See https://kit.svelte.dev/docs/adapters for more information about adapters.
+ adapter: adapter()
+ }
+};
+
+export default config;
diff --git a/UnicadoGUI/Frontend/tsconfig.json b/UnicadoGUI/Frontend/tsconfig.json
new file mode 100644
index 0000000..82081ab
--- /dev/null
+++ b/UnicadoGUI/Frontend/tsconfig.json
@@ -0,0 +1,18 @@
+{
+ "extends": "./.svelte-kit/tsconfig.json",
+ "compilerOptions": {
+ "allowJs": true,
+ "checkJs": true,
+ "esModuleInterop": true,
+ "forceConsistentCasingInFileNames": true,
+ "resolveJsonModule": true,
+ "skipLibCheck": true,
+ "sourceMap": true,
+ "strict": true,
+ "moduleResolution": "bundler"
+ }
+ // Path aliases are handled by https://kit.svelte.dev/docs/configuration#alias
+ //
+ // If you want to overwrite includes/excludes, make sure to copy over the relevant includes/excludes
+ // from the referenced tsconfig.json - TypeScript does not merge them in
+}
diff --git a/UnicadoGUI/Frontend/vite.config.ts b/UnicadoGUI/Frontend/vite.config.ts
new file mode 100644
index 0000000..0166cb1
--- /dev/null
+++ b/UnicadoGUI/Frontend/vite.config.ts
@@ -0,0 +1,8 @@
+import { sveltekit } from '@sveltejs/kit/vite';
+import { defineConfig } from 'vite';
+// @ts-ignore
+import dsv from '@rollup/plugin-dsv';
+
+export default defineConfig({
+ plugins: [sveltekit(), dsv()]
+});
--
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