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index 0000000000000000000000000000000000000000..6f7ba2e58b9ddc3d9b52c3ea5801da3dea929b5a
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new file mode 100644
index 0000000000000000000000000000000000000000..ba8dfea4410631cdad6c13d1396f9c4446e86110
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+++ b/.idea/fastApiUnicado.iml
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+<module type="PYTHON_MODULE" version="4">
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+ <content url="file://$MODULE_DIR$">
+ <excludeFolder url="file://$MODULE_DIR$/.venv" />
+ </content>
+ <orderEntry type="inheritedJdk" />
+ <orderEntry type="sourceFolder" forTests="false" />
+ </component>
+ <component name="PackageRequirementsSettings">
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+ </component>
+</module>
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+ <settings>
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index 0000000000000000000000000000000000000000..afb8c60e7c8dea43411d38b3c71c1c64ae995059
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+<?xml version="1.0" encoding="UTF-8"?>
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+ </component>
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+</project>
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index 0000000000000000000000000000000000000000..c4a7cad97a48db15584c14ace7dd4f61fe9df5ee
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+</project>
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new file mode 100644
index 0000000000000000000000000000000000000000..94a25f7f4cb416c083d265558da75d457237d671
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index 0000000000000000000000000000000000000000..8fab4d76e857fd770f68b8469cf42c2c01668ca8
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+ <option name="number" value="00010" />
+ <option name="presentableId" value="LOCAL-00010" />
+ <option name="project" value="LOCAL" />
+ <updated>1725971455637</updated>
+ </task>
+ <task id="LOCAL-00011" summary="refactoring test file to tmp/modules">
+ <option name="closed" value="true" />
+ <created>1725972109933</created>
+ <option name="number" value="00011" />
+ <option name="presentableId" value="LOCAL-00011" />
+ <option name="project" value="LOCAL" />
+ <updated>1725972109933</updated>
+ </task>
+ <option name="localTasksCounter" value="12" />
+ <servers />
+ </component>
+ <component name="TypeScriptGeneratedFilesManager">
+ <option name="version" value="3" />
+ </component>
+ <component name="Vcs.Log.Tabs.Properties">
+ <option name="TAB_STATES">
+ <map>
+ <entry key="MAIN">
+ <value>
+ <State>
+ <option name="FILTERS">
+ <map>
+ <entry key="branch">
+ <value>
+ <list>
+ <option value="master" />
+ </list>
+ </value>
+ </entry>
+ </map>
+ </option>
+ </State>
+ </value>
+ </entry>
+ </map>
+ </option>
+ </component>
+ <component name="VcsManagerConfiguration">
+ <MESSAGE value="add update_Modules" />
+ <MESSAGE value="prototyp config, graph und log endpoints" />
+ <MESSAGE value="add get_modulePath" />
+ <MESSAGE value="refactor convergence endpoints update modules endpoints" />
+ <MESSAGE value="add modules conf save and load" />
+ <MESSAGE value="modify so it now uses the xmltodict package" />
+ <MESSAGE value="added saving of the new config xml file" />
+ <MESSAGE value="add reset to default" />
+ <MESSAGE value="bugfix utf-8 special char writing" />
+ <MESSAGE value="add config for available modules and a small script to generate add exampale settings of modules" />
+ <MESSAGE value="refactoring test file to tmp/modules" />
+ <option name="LAST_COMMIT_MESSAGE" value="refactoring test file to tmp/modules" />
+ </component>
+ <component name="com.intellij.coverage.CoverageDataManagerImpl">
+ <SUITE FILE_PATH="coverage/fastApiUnicado$fastApiUnicado.coverage" NAME="fastApiUnicado Coverage Results" MODIFIED="1726049164040" SOURCE_PROVIDER="com.intellij.coverage.DefaultCoverageFileProvider" RUNNER="coverage.py" COVERAGE_BY_TEST_ENABLED="false" COVERAGE_TRACING_ENABLED="false" WORKING_DIRECTORY="" />
+ <SUITE FILE_PATH="coverage/fastApiUnicado$xmlConfigReader.coverage" NAME="xmlConfigReader Coverage Results" MODIFIED="1720078308255" SOURCE_PROVIDER="com.intellij.coverage.DefaultCoverageFileProvider" RUNNER="coverage.py" COVERAGE_BY_TEST_ENABLED="false" COVERAGE_TRACING_ENABLED="false" WORKING_DIRECTORY="$PROJECT_DIR$" />
+ <SUITE FILE_PATH="coverage/fastApiUnicado$test.coverage" NAME="test Coverage Results" MODIFIED="1711008069985" SOURCE_PROVIDER="com.intellij.coverage.DefaultCoverageFileProvider" RUNNER="coverage.py" COVERAGE_BY_TEST_ENABLED="true" COVERAGE_TRACING_ENABLED="false" WORKING_DIRECTORY="$PROJECT_DIR$" />
+ <SUITE FILE_PATH="coverage/fastApiUnicado$configWriter.coverage" NAME="configWriter Coverage Results" MODIFIED="1726053313909" SOURCE_PROVIDER="com.intellij.coverage.DefaultCoverageFileProvider" RUNNER="coverage.py" COVERAGE_BY_TEST_ENABLED="false" COVERAGE_TRACING_ENABLED="false" WORKING_DIRECTORY="$PROJECT_DIR$" />
+ </component>
+</project>
\ No newline at end of file
diff --git a/configWriter.py b/configWriter.py
new file mode 100644
index 0000000000000000000000000000000000000000..714e99b36d4ce8ca76aad7ed286523303a6535fc
--- /dev/null
+++ b/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/main.py b/main.py
new file mode 100644
index 0000000000000000000000000000000000000000..0cd07cd6ecd49fce632e757410d417ac9205a676
--- /dev/null
+++ b/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/requirements.txt b/requirements.txt
new file mode 100644
index 0000000000000000000000000000000000000000..6fef470e48622100f9e593b3349e10a855506f55
--- /dev/null
+++ b/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/test_main.http b/test_main.http
new file mode 100644
index 0000000000000000000000000000000000000000..70bc2485a18a553ec6db9b14c5739674ae76f439
--- /dev/null
+++ b/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/tmp/modules b/tmp/modules
new file mode 100644
index 0000000000000000000000000000000000000000..d0279f921797517036c734c4e9e48bf1bf243a88
--- /dev/null
+++ b/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/xml_configs/calculatePerformance_conf.xml b/xml_configs/calculatePerformance_conf.xml
new file mode 100644
index 0000000000000000000000000000000000000000..de72592a608fe017a45eb15d11665ccef9ebf878
--- /dev/null
+++ b/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/xml_configs/calculatePerformance_conf_default.xml b/xml_configs/calculatePerformance_conf_default.xml
new file mode 100644
index 0000000000000000000000000000000000000000..de72592a608fe017a45eb15d11665ccef9ebf878
--- /dev/null
+++ b/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/xml_configs/calculatePolar_conf.xml b/xml_configs/calculatePolar_conf.xml
new file mode 100644
index 0000000000000000000000000000000000000000..b7fefec7f7696b5ef79c072bae8f97ebb54d6396
--- /dev/null
+++ b/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/xml_configs/calculatePolar_conf_default.xml b/xml_configs/calculatePolar_conf_default.xml
new file mode 100644
index 0000000000000000000000000000000000000000..b7fefec7f7696b5ef79c072bae8f97ebb54d6396
--- /dev/null
+++ b/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/xml_configs/config.ini b/xml_configs/config.ini
new file mode 100644
index 0000000000000000000000000000000000000000..a83da65cd12ccfba68049ffa362cbbcf5b84bf03
--- /dev/null
+++ b/xml_configs/config.ini
@@ -0,0 +1,3 @@
+[available_Modules]
+modules = calculatePerformance,calculatePolar,createMissionXML,initialSizing,missionAnalysis,propulsionDesign,systemsDesign,weightAndBalanceAnalysis,wingDesign
+
diff --git a/xml_configs/convergenceLoop_conf.xml b/xml_configs/convergenceLoop_conf.xml
new file mode 100644
index 0000000000000000000000000000000000000000..625cf7c0638ed2cfb2822d3a40bf76749b49cde1
--- /dev/null
+++ b/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/xml_configs/createMissionXML_conf.xml b/xml_configs/createMissionXML_conf.xml
new file mode 100644
index 0000000000000000000000000000000000000000..5723202096c241cc3bef701044d8d223ec68e11e
--- /dev/null
+++ b/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/xml_configs/createMissionXML_conf_default.xml b/xml_configs/createMissionXML_conf_default.xml
new file mode 100644
index 0000000000000000000000000000000000000000..ef4019ed3ec13e0452dceb6a9e240cf22dee5907
--- /dev/null
+++ b/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/xml_configs/initialSizing_conf.xml b/xml_configs/initialSizing_conf.xml
new file mode 100644
index 0000000000000000000000000000000000000000..3bf81bd1335036d32ea3656548fceb3400f82158
--- /dev/null
+++ b/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/xml_configs/initialSizing_conf_default.xml b/xml_configs/initialSizing_conf_default.xml
new file mode 100644
index 0000000000000000000000000000000000000000..fbb78c8e203f9ad11fed9b204dc05726b16af880
--- /dev/null
+++ b/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/xml_configs/missionAnalysis_conf.xml b/xml_configs/missionAnalysis_conf.xml
new file mode 100644
index 0000000000000000000000000000000000000000..9d6114bd52f6666d2d3da7ba2671d6a3768201f1
--- /dev/null
+++ b/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/xml_configs/missionAnalysis_conf_default.xml b/xml_configs/missionAnalysis_conf_default.xml
new file mode 100644
index 0000000000000000000000000000000000000000..5955d492e7a9aa67b1d9ed37b0c1a04c6418ee67
--- /dev/null
+++ b/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/xml_configs/propulsionDesign_conf.xml b/xml_configs/propulsionDesign_conf.xml
new file mode 100644
index 0000000000000000000000000000000000000000..0be5c3aeb17ee5f8cf869c2a7dfdf9150f45731b
--- /dev/null
+++ b/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/xml_configs/propulsionDesign_conf_default.xml b/xml_configs/propulsionDesign_conf_default.xml
new file mode 100644
index 0000000000000000000000000000000000000000..0be5c3aeb17ee5f8cf869c2a7dfdf9150f45731b
--- /dev/null
+++ b/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/xml_configs/systemsDesign_conf.xml b/xml_configs/systemsDesign_conf.xml
new file mode 100644
index 0000000000000000000000000000000000000000..8664a81446b18a387cf731341c8d9e59bfb86182
--- /dev/null
+++ b/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/xml_configs/systemsDesign_conf_default.xml b/xml_configs/systemsDesign_conf_default.xml
new file mode 100644
index 0000000000000000000000000000000000000000..fd1f7b126564b33aca07fa6beb374791ba338f7e
--- /dev/null
+++ b/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/xml_configs/template.xml b/xml_configs/template.xml
new file mode 100644
index 0000000000000000000000000000000000000000..61117458e8494cb7b642370f020864a7ad5d2343
--- /dev/null
+++ b/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/xml_configs/weightAndBalanceAnalysis_conf.xml b/xml_configs/weightAndBalanceAnalysis_conf.xml
new file mode 100644
index 0000000000000000000000000000000000000000..5d27e7e582cf7d03edb6569537f4aed66565e46e
--- /dev/null
+++ b/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/xml_configs/weightAndBalanceAnalysis_conf_default.xml b/xml_configs/weightAndBalanceAnalysis_conf_default.xml
new file mode 100644
index 0000000000000000000000000000000000000000..b5dfd2b6e79aa9718eb00d6d386192cf1d700da4
--- /dev/null
+++ b/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/xml_configs/wingDesign_conf.xml b/xml_configs/wingDesign_conf.xml
new file mode 100644
index 0000000000000000000000000000000000000000..a413da7765cfdb0d16ccb48b36de95b20bebfc14
--- /dev/null
+++ b/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/xml_configs/wingDesign_conf_default.xml b/xml_configs/wingDesign_conf_default.xml
new file mode 100644
index 0000000000000000000000000000000000000000..0e42f6084f94975938cebd2004aec6cacd4b504c
--- /dev/null
+++ b/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