diff --git a/UnicadoGUI/Backend/main.py b/UnicadoGUI/Backend/main.py
index 0cd07cd6ecd49fce632e757410d417ac9205a676..773e5da2f60c4a6fb90a5229eb25ea5fead22c61 100644
--- a/UnicadoGUI/Backend/main.py
+++ b/UnicadoGUI/Backend/main.py
@@ -1,11 +1,13 @@
import configparser
import json
-from fastapi import FastAPI
+from fastapi import FastAPI, File, UploadFile, HTTPException
from fastapi.responses import FileResponse
from fastapi.middleware.cors import CORSMiddleware
from pydantic import BaseModel
import xmltodict
from fastapi.encoders import jsonable_encoder
+import os
+import shutil
#FastAPI Backend for UNICADO Gui
app = FastAPI()
@@ -13,6 +15,7 @@ app = FastAPI()
origins = [
"http://localhost",
"http://localhost:5173",
+ "http://localhost:5174",
]
app.add_middleware(
@@ -110,3 +113,35 @@ async def get_csv(file: str):
async def get_report(file: str):
return FileResponse(f"output_files/reportHTML/{file}")
+#location for the porject lists
+UPLOAD_DIRECTORY = "./project_lists/"
+
+if not os.path.exists(UPLOAD_DIRECTORY):
+ os.makedirs(UPLOAD_DIRECTORY)
+
+#endpoint to save the project list on the server
+@app.post("/projects/")
+async def upload_project_list(file: UploadFile = File(...)):
+ if not file.filename.endswith(".zip"):
+ raise HTTPException(status_code=400, detail="Only .zip files are allowed")
+
+ file_path = os.path.join(UPLOAD_DIRECTORY, file.filename)
+
+ with open(file_path, "wb") as buffer:
+ shutil.copyfileobj(file.file, buffer)
+
+ return {"Project list successfully saved"}
+
+#endpoint to get the project list from the server
+@app.get("/projects/")
+async def get_project_list():
+ file_path = UPLOAD_DIRECTORY + "projects.zip"
+ return FileResponse(path=file_path, filename="projects.zip", media_type="application/zip")
+
+#TODO get file per project
+#endpoint to get the aircraft_exchange_file
+@app.get("/projects/aircraft_exchange_file/")
+async def get_aircraft_exchange_file():
+ with open("xml_configs/csmr-2020.xml", encoding='utf-8') as fd:
+ config = json.dumps(xmltodict.parse(fd.read()))
+ return config
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/requirements.txt b/UnicadoGUI/Backend/requirements.txt
index 6fef470e48622100f9e593b3349e10a855506f55..c884f2f838e34101f5a8b33ad1881f5affaf84b6 100644
--- a/UnicadoGUI/Backend/requirements.txt
+++ b/UnicadoGUI/Backend/requirements.txt
@@ -1,3 +1,4 @@
xmltodict~=0.13.0
fastapi~=0.109.2
-pydantic~=1.10.14
\ No newline at end of file
+pydantic~=1.10.14
+python-multipart==0.0.12
\ No newline at end of file
diff --git a/UnicadoGUI/Backend/xml_configs/csmr-2020.xml b/UnicadoGUI/Backend/xml_configs/csmr-2020.xml
new file mode 100644
index 0000000000000000000000000000000000000000..9df1fb1ba3af8dac24f2071ae40fc9821cbed3f5
--- /dev/null
+++ b/UnicadoGUI/Backend/xml_configs/csmr-2020.xml
@@ -0,0 +1,9187 @@
+<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">
+ <aerodynamic_technologies description="Integration of aerodynamic technologies on the aircraft: true / false">
+ <value>false</value>
+ </aerodynamic_technologies>
+ <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 / wide_body">
+ <value>single_aisle</value>
+ </fuselage_type>
+ <fuselage_pressurization description="Switch to select a pressurized fuselage. (true: pressurized fuselage, false: non pressurized fuselage)">
+ <value>true</value>
+ </fuselage_pressurization>
+ <blended_wing_body_configuration description="Additional design description for blended wing body configurations.">
+ <number_of_payload_tubes description="Number of fuselage tubes for blendend wing body configurations. For tube and wing configuration is set to 1.">
+ <value>1</value>
+ <unit>1</unit>
+ <default>1</default>
+ <lower_boundary>1</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </number_of_payload_tubes>
+ <center_body_wing_sweep description="Sweep of the leading edge of the center body.">
+ <value>60</value>
+ <unit>degree</unit>
+ <default>60</default>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ <center_body_wing_sweep_tolerance Desc="Permissible deviation of the actual from the desired leading edge sweep of the center body.">
+ <value>5</value>
+ <unit>degree</unit>
+ <default>5</default>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>15</upper_boundary>
+ </center_body_wing_sweep_tolerance>
+ </center_body_wing_sweep>
+ </blended_wing_body_configuration>
+ </fuselage_definition>
+ <wing_definition 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_definition>
+ <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>
+ <tank_definition 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>wing</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>inner_left</value>
+ </position>
+ <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </energy_share>
+ </tank>
+ <tank ID="1" description="single 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>wing</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>outer_left</value>
+ </position>
+ <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </energy_share>
+ </tank>
+ <tank ID="2" description="single 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>wing</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>inner_right</value>
+ </position>
+ <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </energy_share>
+ </tank>
+ <tank ID="3" description="single 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>wing</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>outer_right</value>
+ </position>
+ <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </energy_share>
+ </tank>
+ <tank ID="4" description="single 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>wing</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>center</value>
+ </position>
+ <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+ <value>0.0</value>
+ <unit>1</unit>
+ <lower_boundary>0.0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </energy_share>
+ </tank>
+ </tank_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>162</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000</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>
+ <multi_passenger_deck_layout description="Switch to select a multi passenger deck fuselage design. (true: multi passenger deck allowed, false: multi passenger deck denied)">
+ <value>false</value>
+ <default>false</default>
+ <specific_number_of_passenger_decks>
+ <value>2</value>
+ <unit>-</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>3</upper_boundary>
+ <default>2</default>
+ </specific_number_of_passenger_decks>
+ </multi_passenger_deck_layout>
+ <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="One specific energy carrier">
+ <type description="Energy type (for multifuel engine create new ID). Selector: kerosene / liquid_hydrogen / battery / saf">
+ <value>kerosene</value>
+ </type>
+ <density description="Energy carrier density.">
+ <value>783</value>
+ <unit>kg/m^3</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10000</upper_boundary>
+ </density>
+ <volumetric_density description="Volumetric energy density of energy carrier.">
+ <value>3.2325e+10</value>
+ <unit>J/m^3</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1e+12</upper_boundary>
+ </volumetric_density>
+ <gravimetric_density description="Gravimetric energy density of energy carrier.">
+ <value>43100000</value>
+ <unit>J/kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1e+12</upper_boundary>
+ </gravimetric_density>
+ </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. Selector: turbo / electric / fuel_cell">
+ <value>turbo</value>
+ </powertrain>
+ <type description="Type of main thrust generator. Selector: fan / prop">
+ <value>fan</value>
+ </type>
+ <position description="propulsor position (arrangement order acc to ID order)">
+ <parent_component description="position on component. Selector: wing / fuselage / empennage">
+ <value>wing</value>
+ </parent_component>
+ <x description="x-position (aircraft coordinate system). Selector: front / back">
+ <value>front</value>
+ </x>
+ <y description="y position (aircraft coordinate system). Selector: left / right">
+ <value>left</value>
+ </y>
+ <z description="z position (aircraft coordinate system). Selector: over / mid / under / in">
+ <value>under</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>0.5</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </thrust_share>
+ </propulsor>
+ <propulsor ID="1" description="Information for specific propulsor">
+ <powertrain description="Way the power is generated from the source. Selector: turbo / electric / fuel_cell">
+ <value>turbo</value>
+ </powertrain>
+ <type description="Type of main thrust generator. Selector: fan / prop">
+ <value>fan</value>
+ </type>
+ <position description="propulsor position (arrangement order acc to ID order)">
+ <parent_component description="position on component. Selector: wing / fuselage / empennage">
+ <value>wing</value>
+ </parent_component>
+ <x description="x-position (aircraft coordinate system). Selector: front / back">
+ <value>front</value>
+ </x>
+ <y description="y position (aircraft coordinate system). Selector: left / right">
+ <value>right</value>
+ </y>
+ <z description="z position (aircraft coordinate system). Selector: over / mid / under / in">
+ <value>under</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>0.5</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </thrust_share>
+ </propulsor>
+ <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>turbo</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>turbo</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>turbo</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>turbo</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>turbo</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>turbo</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>turbo</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>
+ </propulsion>
+ <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>
+ </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>1951</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>2425</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>0.82</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>67.65</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>12192</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>4572</value>
+ <unit>m</unit>
+ <lower_boundary>1500</lower_boundary>
+ <upper_boundary>12000</upper_boundary>
+ </maximum_one_engine_operating_altitude>
+ <climb_or_descend_segment_gradient description="climb / descend segment gradient">
+ <value>0.024</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </climb_or_descend_segment_gradient>
+ </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>100</upper_boundary>
+ </delta_ISA>
+ <range description="Target range for the specified mission">
+ <value>4537400</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>20000000</upper_boundary>
+ </range>
+ <contingency description="Reserved Fuel Percentage">
+ <value>0.06</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>0.08</upper_boundary>
+ </contingency>
+ <alt_dist description="Reserved fuel - alternate distance">
+ <value>370400</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>926000</upper_boundary>
+ </alt_dist>
+ <loiter_time description="Reserved fuel - loiter time in seconds">
+ <value>1800</value>
+ <unit>s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>3600</upper_boundary>
+ </loiter_time>
+ <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>10058.4</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>128.6112</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>154.3334</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>128.6112</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>154.3334</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="Fuel estimation method. Selector: 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>100</upper_boundary>
+ </delta_ISA>
+ <range description="Target range for the specified mission">
+ <value>1481600</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 at top of descent. May be altered during cruise.">
+ <value>10668</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>128.6112</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>154.3334</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>128.6112</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>154.3334</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="Fuel estimation method. Selector: 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">
+ <landing_gear description="Landing gear requirements and operational conditions">
+ <friction_coefficient description="Friction coefficient of tyres and pavement: Raymer p.486 - Table 17.1: 0.03 - 0.05">
+ <value>0.03</value>
+ <default>0.03</default>
+ <unit>1</unit>
+ <lower_boundary>0.02</lower_boundary>
+ <upper_boundary>0.08</upper_boundary>
+ </friction_coefficient>
+ <breaking_coefficient description="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>
+ <default>0.34189</default>
+ <unit>1</unit>
+ <lower_boundary>0.06</lower_boundary>
+ <upper_boundary>0.5</upper_boundary>
+ </breaking_coefficient>
+ </landing_gear>
+ </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>
+ <duration_operation description="Operating years of aircraft">
+ <value>25</value>
+ <unit>a</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </duration_operation>
+ </assessment_scenario>
+ </requirements_and_specifications>
+ <analysis>
+ <masses_cg_inertia description="Masses, Center of Gravity, Inertias." tool_level="2">
+ <maximum_takeoff_mass>
+ <mass_properties>
+ <mass description="mass">
+ <value>64586.71283</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>300000</upper_boundary>
+ </mass>
+ <inertia>
+ <j_xx description="inertia in x">
+ <value>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</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</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</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</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</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</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</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</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity>
+ <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</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z component">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </maximum_takeoff_mass>
+ <operating_mass_empty description="OME">
+ <mass_properties description="operating mass empty properties">
+ <inertia description="Inertia with regard to the total center of gravity.">
+ <j_xx description="Inertia in x.">
+ <value>599569.7918648543</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia in y.">
+ <value>1693729.8225431978</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia in z.">
+ <value>2250064.0202634176</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 w.r.t global coordinate system.">
+ <x description="Center of gravity in x-direction with regard to the global reference point.">
+ <value>15.65578242991758</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point.">
+ <value>0.0016924404193550643</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point.">
+ <value>-0.7686391127807779</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ <mass description="Mass">
+ <value>36354.8858137</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ </mass_properties>
+ </operating_mass_empty>
+ <design_mass description="">
+ <mass_properties description="design mass properties">
+ <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+ <x description="Center of gravity in x-direction with regard to the global reference point.">
+ <value>15.822140859635715</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point.">
+ <value>0.0009526491672380705</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point.">
+ <value>-0.49323187357341247</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ <mass description="Mass">
+ <value>64586.71283</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia with regard to the total center of gravity.">
+ <j_xx description="Inertia in x.">
+ <value>1065172.977496338</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia in y.">
+ <value>3009016.235693439</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia in z.">
+ <value>3997378.4946150086</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>
+ </mass_properties>
+ </design_mass>
+ <most_forward_mass description="">
+ <mass_properties description="most forward mass properties">
+ <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+ <x description="Center of gravity in x-direction with regard to the global reference point.">
+ <value>14.971565471999668</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ <mass description="Mass">
+ <value>54132.712830000004</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia with regard to the total center of gravity.">
+ <j_xx description="Inertia in x.">
+ <value>599569.7918648543</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia in y.">
+ <value>1693729.8225431978</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia in z.">
+ <value>2250064.0202634176</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>
+ </mass_properties>
+ </most_forward_mass>
+ <most_afterward_mass description="">
+ <mass_properties description="most afterward mass properties">
+ <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+ <x description="Center of gravity in x-direction with regard to the global reference point.">
+ <value>16.190913398360987</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ <mass description="Mass">
+ <value>55092.712830000004</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia with regard to the total center of gravity.">
+ <j_xx description="Inertia in x.">
+ <value>599569.7918648543</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia in y.">
+ <value>1693729.8225431978</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia in z.">
+ <value>2250064.0202634176</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>
+ </mass_properties>
+ </most_afterward_mass>
+ <manufacturer_mass_empty description="MME">
+ <mass_properties description="manufacturer mass empty properties">
+ <mass description="Mass">
+ <value>33257.8766177</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia with regard to the total center of gravity.">
+ <j_xx description="Inertia in x.">
+ <value>548493.488983179</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia in y.">
+ <value>1549443.938581515</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia in z.">
+ <value>2058384.9981354333</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 w.r.t global coordinate system.">
+ <x description="Center of gravity in x-direction with regard to the global reference point.">
+ <value>15.654878612191535</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point.">
+ <value>0.0018500372003712442</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point.">
+ <value>-0.8402133014801614</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </manufacturer_mass_empty>
+ <maximum_zero_fuel_mass description="MZFM">
+ <mass_properties description="maximum zero fuel mass properties">
+ <mass description="Mass">
+ <value>66354.8858137</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia with regard to the total center of gravity.">
+ <j_xx description="Inertia in x.">
+ <value>1094333.9302566017</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia in y.">
+ <value>3091393.260043198</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia in z.">
+ <value>4106813.645439384</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 w.r.t global coordinate system.">
+ <x description="Center of gravity in x-direction with regard to the global reference point.">
+ <value>16.123871067575358</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point.">
+ <value>0.0009272637189805906</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point.">
+ <value>-0.5302215013355478</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </maximum_zero_fuel_mass>
+ <maximum_payload_mass description="">
+ <mass_properties description="maximum payload mass properties">
+ <mass description="Mass">
+ <value>30000.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia with regard to the total 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 w.r.t global coordinate system.">
+ <x description="Center of gravity in x-direction with regard to the global reference point.">
+ <value>16.6911147</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point.">
+ <value>-0.2413</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </maximum_payload_mass>
+ <maximum_landing_mass description="MLM">
+ <mass_properties description="maximum landing mass properties">
+ <mass description="Mass">
+ <value>55289.67959760656</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia with regard to the total center of gravity.">
+ <j_xx description="Inertia in x.">
+ <value>911845.0229355189</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_xx>
+ <j_yy description="Inertia in y.">
+ <value>2575878.7881554803</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </j_yy>
+ <j_zz description="Inertia in z.">
+ <value>3421969.728965175</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 w.r.t global coordinate system.">
+ <x description="Center of gravity in x-direction with regard to the global reference point.">
+ <value>15.65578242991758</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point.">
+ <value>0.0016924404193550643</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point.">
+ <value>-0.7686391127807779</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </maximum_landing_mass>
+ <maximum_fuel_mass description="">
+ <mass_properties description="maximum fuel mass properties">
+ <mass description="Mass">
+ <value>53058.889254535265</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia with regard to the total 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 w.r.t global coordinate system.">
+ <x description="Center of gravity in x-direction with regard to the global reference point.">
+ <value>15.409485429697211</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point.">
+ <value>0.0011596262013133772</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point.">
+ <value>-0.5266560904250428</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </maximum_fuel_mass>
+ </masses_cg_inertia>
+ <aerodynamics>
+ <lift_coefficients description="lift coefficients">
+ <C_LoptimumCruise description="optimum cruise CL">
+ <value>0.556</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>2</upper_boundary>
+ </C_LoptimumCruise>
+ <C_LmaxLanding description="C_LmaxLanding">
+ <value>1.629</value>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </C_LmaxLanding>
+ <C_LmaxT-O description="C_LmaxTO">
+ <value>1.627</value>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </C_LmaxT-O>
+ <C_LgroundRoll description="C_LgroundRoll">
+ <value>0.4</value>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </C_LgroundRoll>
+ </lift_coefficients>
+ <polar>
+ <polar_file description="Name of polar file">
+ <value>SMR-2020_polar.xml</value>
+ </polar_file>
+ <configurations description="Number of configurations in the polar file">
+ <value>7</value>
+ <unit>1</unit>
+ <lower_boundary>-2147483648</lower_boundary>
+ <upper_boundary>2147483647</upper_boundary>
+ </configurations>
+ <configuration ID="0" description="Configuration in polar file marked with ID - name can vary">
+ <type description=" Type">
+ <value>cruise</value>
+ </type>
+ <name description=" Name">
+ <value>clean</value>
+ </name>
+ </configuration>
+ <configuration ID="1" description="Configuration in polar file marked with ID - name can vary">
+ <type description=" Type">
+ <value>departure</value>
+ </type>
+ <name description=" Name">
+ <value>takeoff</value>
+ </name>
+ </configuration>
+ <configuration ID="2" description="Configuration in polar file marked with ID - name can vary">
+ <type description=" Type">
+ <value>departure</value>
+ </type>
+ <name description=" Name">
+ <value>takeoff_landing_gear_retracted</value>
+ </name>
+ </configuration>
+ <configuration ID="3" description="Configuration in polar file marked with ID - name can vary">
+ <type description=" Type">
+ <value>departure</value>
+ </type>
+ <name description=" Name">
+ <value>climb</value>
+ </name>
+ </configuration>
+ <configuration ID="4" description="Configuration in polar file marked with ID - name can vary">
+ <type description=" Type">
+ <value>approach</value>
+ </type>
+ <name description=" Name">
+ <value>approach</value>
+ </name>
+ </configuration>
+ <configuration ID="5" description="Configuration in polar file marked with ID - name can vary">
+ <type description=" Type">
+ <value>approach</value>
+ </type>
+ <name description=" Name">
+ <value>approach_landing_gear_out</value>
+ </name>
+ </configuration>
+ <configuration ID="6" description="Configuration in polar file marked with ID - name can vary">
+ <type description=" Type">
+ <value>approach</value>
+ </type>
+ <name description=" Name">
+ <value>landing</value>
+ </name>
+ </configuration>
+ </polar>
+ <reference_values>
+ <b description="Wing half span">
+ <value>32.9299991</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </b>
+ <MAC description="Mean aerodynamic chord">
+ <value>3.857492149</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </MAC>
+ <S_ref description="Wing reference area">
+ <value>105.2800817</value>
+ <unit>m^2</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </S_ref>
+ </reference_values>
+ <max_spoiler_factor description="max_spoiler_factor">
+ <value>2.5</value>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </max_spoiler_factor>
+ </aerodynamics>
+ <mission description="Mission data" tool_level="0">
+ <design_mission description="Data of design mission">
+ <range description="Traveled range from break release to end of taxi at destination">
+ <value>4538402.27</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5000000</upper_boundary>
+ </range>
+ <mission_energy ID="0" description="Amount of energy loaded into tanks (including reserves) for specified energy carrier">
+ <consumed_energy description="Energy amount">
+ <value>5.510329405e+11</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1e+12</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>4.494145685e+11</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1e+12</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>
+ <taxi_energy ID="0" description="Amount of energy needed for taxi segment specified energy carrier">
+ <consumed_energy description="Energy amount">
+ <value>1.299219544e+10</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1e+12</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>
+ <block_time description="Block time for the whole mission: Time from break release to end of taxiing after landing">
+ <value>20978.31905</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>20138.31905</value>
+ <unit>s</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>44500</upper_boundary>
+ </flight_time>
+ <takeoff_engine_derate description="Engine power demand">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </takeoff_engine_derate>
+ <cruise description="Characteristics of the cruise segment">
+ <average_lift_coefficient description="Lift coefficient CL_average: Arithmetic mean over the entire cruise flight">
+ <value>0.5137058423</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>0.4907014254</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>0.5572585237</value>
+ <unit>1</unit>
+ <lower_boundary>-0.01</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </maximum_lift_coefficient>
+ <top_of_climb_mass description="Total aircraft mass at top of climb (= start of initial cruise altitude (ICA))">
+ <value>63386.2862</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>150000</upper_boundary>
+ </top_of_climb_mass>
+ <top_of_descent_mass description="Total aircraft mass at top of descent (TOD)">
+ <value>54443.51796</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>150000</upper_boundary>
+ </top_of_descent_mass>
+ <top_of_climb_range description="Flown range from takeoff to top of climb (= start of initial cruise altitude (ICA))">
+ <value>203676.2478</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>500000</upper_boundary>
+ </top_of_climb_range>
+ <top_of_descent_range description="Flown range from takeoff to top of descent">
+ <value>4329735.435</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5000000</upper_boundary>
+ </top_of_descent_range>
+ <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>0.4999014739</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>10058.40002</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>15000</upper_boundary>
+ </altitude>
+ </cruise_step>
+ <cruise_step ID="1" description="Data of a cruise step">
+ <relative_end_of_cruise_step description="End of cruise step relative to total cruise length">
+ <value>1</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>10668.00002</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>15000</upper_boundary>
+ </altitude>
+ </cruise_step>
+ </cruise_steps>
+ </cruise>
+ </design_mission>
+ </mission>
+ </analysis>
+ <component_design>
+ <global_reference_point>
+ <reference_component description="Global reference point of aircraft geometry">
+ <value>fuselage</value>
+ </reference_component>
+ <x description="X coordinate of the global reference point">
+ <value>0</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>0</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>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </global_reference_point>
+ <fuselage description="Geometric description of the aircraft fuselage." tool_level="1">
+ <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>-100</lower_boundary>
+ <upper_boundary>100</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. (fuselage nose point)">
+ <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 fuselages.">
+ <mass description="Mass of all fuselages.">
+ <value>14004.22881</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia of all fuselages with regard to the total center of gravity.">
+ <j_xx description="Inertia of the of all 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 of all 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 of all 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 all 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 all 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 all 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 all 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 all 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 all 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 all fuselages.">
+ <x description="Center of gravity in x-direction with regard to the global reference point. (of all fuselages)">
+ <value>16.6911147</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. (of all fuselages)">
+ <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. (of all fuselages)">
+ <value>-0.2413</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <specific description="Fuselage design specific output parameter.">
+ <geometry description="Geometry description of the entire fuselage design.">
+ <fuselage ID="0" description="Geometrical description of one entire fuselage.">
+ <name description="Name of the fuselage.">
+ <value>fuselage_0</value>
+ </name>
+ <position description="Position of one entire fuselage with regard to the fuselage global position.">
+ <x description="Distance in x direction with regard to the fuselage gear global position.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the fuselage gear global position.">
+ <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 fuselage gear global position.">
+ <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="X component of the unit vector.">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </x>
+ <y description="Y component of the unit vector.">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </y>
+ <z description="Z component of the unit vector.">
+ <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 fuselage.">
+ <value>14004.228808373002</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 fuselage center of gravity position.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </x>
+ <y description="Center of gravity in x-direction with regard to the global fuselage center of gravity position.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </y>
+ <z description="Center of gravity in x-direction with regard to the global fuselage center of gravity position.">
+ <value>0.0</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_0</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>0.067576816</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.957580772</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>0.236859405</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>0.267784187</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>0.496500597</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="1" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_1</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>0.191436979</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.924669034</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>0.410780143</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>0.467145347</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>0.836740921</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="2" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_2</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>0.32358539</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.88671607</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>0.51432337</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>0.617001451</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>1.09949371</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="3" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_3</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>0.548621791</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.814819481</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>0.638938798</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>0.811634047</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>1.332869486</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="4" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_4</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>0.773360095</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.746964181</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>0.756396515</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>0.976318453</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>1.597847703</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="5" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_5</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>1.115421815</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.624593025</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>0.945319536</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>1.21146329</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>1.950706682</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="6" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_6</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>1.427740836</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.499674101</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>1.097107435</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>1.429827854</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>2.243644807</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="7" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_7</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>2.112564592</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.21769763</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>1.34967515</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>1.867364888</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>2.796234326</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="8" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_8</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>2.599915253</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.174885536</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>1.558414858</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>1.971983901</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>3.095828445</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="9" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_9</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>3.420628612</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.083279283</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>1.734079899</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>2.113593806</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>3.508608277</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="10" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_10</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>4.164243156</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>-0.041639641</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>1.833938046</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>2.167125385</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>3.762303773</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="11" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_11</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>5.130942918</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance 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>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>1.877197398</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>2.219197163</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>3.908262138</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="12" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_12</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>6.17200442</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance 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>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>1.915417119</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>2.227075627</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>3.967986828</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="13" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_13</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>6.172260794</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance 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>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>1.915417119</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>2.227075627</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>3.967986828</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="14" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_14</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>27.23273937</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance 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>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>1.915413925</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>2.227071912</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>3.967986828</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="15" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_15</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>27.22660641</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance 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>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>1.915413925</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>2.227071912</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>3.967986828</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="16" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_16</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>31.6198242</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance 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>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>1.699062858</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>1.736603193</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>3.3288491</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="17" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_17</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>32.46197422</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance 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>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>1.657090968</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>1.517243141</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>3.095828445</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="18" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_18</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>34.14627427</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance 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>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>1.575335554</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>0.939595006</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>2.46334671</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ <section ID="19" description="Geometrical description of one fuselage section.">
+ <name description="Name of the fuselage section.">
+ <value>section_19</value>
+ </name>
+ <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+ <value>ellipse</value>
+ </section_shape>
+ <origin description="Origin of fuselage section (local).">
+ <z description="Distance in x direction with regard to the global reference point.">
+ <value>37.08549195</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>75</upper_boundary>
+ </z>
+ <x description="Distance in y direction with regard to the global reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-25</lower_boundary>
+ <upper_boundary>25</upper_boundary>
+ </x>
+ <y description="Distance in z direction with regard to the global reference point.">
+ <value>0.92429206</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </y>
+ </origin>
+ <upper_height description="Height of the upper half of the fuselage section.">
+ <value>0.528165979</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>0.614104138</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </lower_height>
+ <width description="Width of the fuselage section.">
+ <value>0.559150813</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </width>
+ </section>
+ </sections>
+ <number_of_required_cabin_crew description="Number of minimum required flight attendants.">
+ <value>4</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </number_of_required_cabin_crew>
+ <mass_breakdown description="Mass breakdown of fuselage design module in accordance to CPACS.">
+ <fuselage_structure description="Mass breakdown of the fuselage structure block.">
+ <component_mass ID="0" description="Mass of a single component of the fuselage structure block.">
+ <name description="Name of the fuselage structure component.">
+ <value>door_mass</value>
+ </name>
+ <mass description="Mass of the fuselage structure component.">
+ <value>360.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="1" description="Mass of a single component of the fuselage structure block.">
+ <name description="Name of the fuselage structure component.">
+ <value>fuselage_mass</value>
+ </name>
+ <mass description="Mass of the fuselage structure component.">
+ <value>7717.542772675</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ </fuselage_structure>
+ <fuselage_furnishing description="Mass breakdown of the fuselage furnishing block.">
+ <component_mass ID="0" description="Mass of a single component of the fuselage furnishing block.">
+ <name description="Name of the fuselage furnishing component.">
+ <value>lavatory_mass</value>
+ </name>
+ <mass description="Mass of the fuselage furnishing component.">
+ <value>386.68</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="1" description="Mass of a single component of the fuselage furnishing block.">
+ <name description="Name of the fuselage furnishing component.">
+ <value>flight_attendant_seat_mass</value>
+ </name>
+ <mass description="Mass of the fuselage furnishing component.">
+ <value>48.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="2" description="Mass of a single component of the fuselage furnishing block.">
+ <name description="Name of the fuselage furnishing component.">
+ <value>floor_covering_mass</value>
+ </name>
+ <mass description="Mass of the fuselage furnishing component.">
+ <value>157.909712567</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="3" description="Mass of a single component of the fuselage furnishing block.">
+ <name description="Name of the fuselage furnishing component.">
+ <value>wall_covering_mass</value>
+ </name>
+ <mass description="Mass of the fuselage furnishing component.">
+ <value>286.170627658</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="4" description="Mass of a single component of the fuselage furnishing block.">
+ <name description="Name of the fuselage furnishing component.">
+ <value>ceiling_covering_mass</value>
+ </name>
+ <mass description="Mass of the fuselage furnishing component.">
+ <value>105.8244264</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="5" description="Mass of a single component of the fuselage furnishing block.">
+ <name description="Name of the fuselage furnishing component.">
+ <value>linings_mass</value>
+ </name>
+ <mass description="Mass of the fuselage furnishing component.">
+ <value>391.995054058</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="6" description="Mass of a single component of the fuselage furnishing block.">
+ <name description="Name of the fuselage furnishing component.">
+ <value>acoustic_and_thermal_insolation_mass</value>
+ </name>
+ <mass description="Mass of the fuselage furnishing component.">
+ <value>612.814955814</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="7" description="Mass of a single component of the fuselage furnishing block.">
+ <name description="Name of the fuselage furnishing component.">
+ <value>overhead_bin_mass</value>
+ </name>
+ <mass description="Mass of the fuselage furnishing component.">
+ <value>347.40342</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="8" description="Mass of a single component of the fuselage furnishing block.">
+ <name description="Name of the fuselage furnishing component.">
+ <value>passenger_safety_unit_mass</value>
+ </name>
+ <mass description="Mass of the fuselage furnishing component.">
+ <value>81.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="9" description="Mass of a single component of the fuselage furnishing block.">
+ <name description="Name of the fuselage furnishing component.">
+ <value>lightning_panel_mass</value>
+ </name>
+ <mass description="Mass of the fuselage furnishing component.">
+ <value>64.8</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="10" description="Mass of a single component of the fuselage furnishing block.">
+ <name description="Name of the fuselage furnishing component.">
+ <value>oxygen_system_mass</value>
+ </name>
+ <mass description="Mass of the fuselage furnishing component.">
+ <value>182.728</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="11" description="Mass of a single component of the fuselage furnishing block.">
+ <name description="Name of the fuselage furnishing component.">
+ <value>cargo_linings_mass</value>
+ </name>
+ <mass description="Mass of the fuselage furnishing component.">
+ <value>316.484166377</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="12" description="Mass of a single component of the fuselage furnishing block.">
+ <name description="Name of the fuselage furnishing component.">
+ <value>cargo_loadings_mass</value>
+ </name>
+ <mass description="Mass of the fuselage furnishing component.">
+ <value>264.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="13" description="Mass of a single component of the fuselage furnishing block.">
+ <name description="Name of the fuselage furnishing component.">
+ <value>miscellaneous_mass</value>
+ </name>
+ <mass description="Mass of the fuselage furnishing component.">
+ <value>277.281530882</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ </fuselage_furnishing>
+ <fuselage_operator_items description="Mass breakdown of the fuselage operator items block.">
+ <component_mass ID="0" description="Mass of a single component of the fuselage operator items block.">
+ <name description="Name of the fuselage operator items component.">
+ <value>total_emergency_equipment_masses</value>
+ </name>
+ <mass description="Mass of the fuselage operator item component.">
+ <value>236.14919600000002</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="1" description="Mass of a single component of the fuselage operator items block.">
+ <name description="Name of the fuselage operator items component.">
+ <value>flight_attendant_mass</value>
+ </name>
+ <mass description="Mass of the fuselage operator item component.">
+ <value>280.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="2" description="Mass of a single component of the fuselage operator items block.">
+ <name description="Name of the fuselage operator items component.">
+ <value>in_flight_entertainment</value>
+ </name>
+ <mass description="Mass of the fuselage operator item component.">
+ <value>81.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="3" description="Mass of a single component of the fuselage operator items block.">
+ <name description="Name of the fuselage operator items component.">
+ <value>total_fixed_galley_mass</value>
+ </name>
+ <mass description="Mass of the fuselage operator item component.">
+ <value>280.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="4" description="Mass of a single component of the fuselage operator items block.">
+ <name description="Name of the fuselage operator items component.">
+ <value>total_seat_mass</value>
+ </name>
+ <mass description="Mass of the fuselage operator item component.">
+ <value>1153.2</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ <component_mass ID="5" description="Mass of a single component of the fuselage operator items block.">
+ <name description="Name of the fuselage operator items component.">
+ <value>catering_mass</value>
+ </name>
+ <mass description="Mass of the fuselage operator item component.">
+ <value>846.24</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ </component_mass>
+ </fuselage_operator_items>
+ </mass_breakdown>
+ <fuselage_accommodation description="Description of the accommodation of current fuselage.">
+ <position description="Position of the payload tubes with regard to the fuselage position.">
+ <x description="Distance in x direction with regard to the fuselage position.">
+ <value>3.75</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the fuselage position.">
+ <value>0.0</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 fuselage position.">
+ <value>0.0</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 fuselage.">
+ <value>5926.686035698</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </mass>
+ <center_of_gravity description="Center of gravity of all payload tubes.">
+ <x description="Center of gravity in x-direction with regard to the center of gravity of the fuselage.">
+ <value>0.0</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 center of gravity of the fuselage.">
+ <value>0.0</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 center of gravity of the fuselage.">
+ <value>0.0</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.">
+ <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 referred 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>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Payload tube reference point in y-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>35</upper_boundary>
+ </y>
+ <z description="Payload tube reference point in z-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-15</lower_boundary>
+ <upper_boundary>15</upper_boundary>
+ </z>
+ <upper_z description="Upper payload tube reference point in z-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>15</upper_boundary>
+ </upper_z>
+ <lower_z description="Lower payload tube reference point in z-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-15</lower_boundary>
+ <upper_boundary>0</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>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Payload tube reference point in y-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>35</upper_boundary>
+ </y>
+ <z description="Payload tube reference point in z-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-15</lower_boundary>
+ <upper_boundary>15</upper_boundary>
+ </z>
+ <upper_z description="Upper payload tube reference point in z-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>15</upper_boundary>
+ </upper_z>
+ <lower_z description="Lower payload tube reference point in z-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-15</lower_boundary>
+ <upper_boundary>0</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 referred to fuselage nose point.">
+ <front_reference_points description="Reference points in the front of payload tube.">
+ <x description="Wall reference point in x-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <left_y description="Left wall reference point in y-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-35</lower_boundary>
+ <upper_boundary>35</upper_boundary>
+ </left_y>
+ <right_y description="Right wall reference point in y-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-35</lower_boundary>
+ <upper_boundary>35</upper_boundary>
+ </right_y>
+ <z description="Wall reference point in z-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-15</lower_boundary>
+ <upper_boundary>15</upper_boundary>
+ </z>
+ </front_reference_points>
+ <aft_reference_points description="Reference points in the aft of payload tube.">
+ <x description="Wall reference point in x-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <left_y description="Left wall reference point in y-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-35</lower_boundary>
+ <upper_boundary>35</upper_boundary>
+ </left_y>
+ <right_y description="Right wall reference point in y-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-35</lower_boundary>
+ <upper_boundary>35</upper_boundary>
+ </right_y>
+ <z description="Wall reference point in z-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-15</lower_boundary>
+ <upper_boundary>15</upper_boundary>
+ </z>
+ </aft_reference_points>
+ </payload_tube_wall_reference_points>
+ <payload_tube_structural_wall_thickness description="Structural wall thickness of the payload tube.">
+ <value>0.137414</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 payload tube.">
+ <value>187.15636792302973</value>
+ <unit>m^3</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1000</upper_boundary>
+ </payload_tube_water_volume>
+ <payload_decks description="Geometrical description of the payload decks.">
+ <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_1</value>
+ </name>
+ <position description="Position of the payload deck with regard to the payload tube reference point.">
+ <x description="Distance in x direction with regard to the payload tube reference point.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the payload tube reference point.">
+ <value>0.0</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 payload tube reference point.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </position>
+ <payload_deck_structural_floor_thickness description="Structural floor thickness of current payload deck.">
+ <value>0.20624799999999996</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </payload_deck_structural_floor_thickness>
+ <payload_deck_water_volume description="Total water volume of the payload deck.">
+ <value>124.77091194868649</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 payload deck.">
+ <value>26.723339999999997</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </payload_deck_length>
+ <payload_deck_required_galley_power description="Required galley power of the payload deck.">
+ <value>8000</value>
+ <unit>W</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </payload_deck_required_galley_power>
+ </payload_deck>
+ <payload_deck ID="1" description="Geometrical description of the payload decks in one payload tube.">
+ <name description="Name of the payload deck.">
+ <value>cargo_deck</value>
+ </name>
+ <position description="Position of the payload deck with regard to the payload tube reference point.">
+ <x description="Distance in x direction with regard to the payload tube reference point.">
+ <value>3.75</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the payload tube reference point.">
+ <value>0.0</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 payload tube reference point.">
+ <value>-1.831848</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </position>
+ <payload_deck_structural_floor_thickness description="Structural floor thickness of current payload deck.">
+ <value>0.20624799999999996</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </payload_deck_structural_floor_thickness>
+ <payload_deck_water_volume description="Total water volume of the payload deck.">
+ <value>62.385455974343245</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 payload deck.">
+ <value>13.361669999999998</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </payload_deck_length>
+ <payload_deck_required_galley_power description="Required galley power of the payload deck.">
+ <value>0</value>
+ <unit>W</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100000</upper_boundary>
+ </payload_deck_required_galley_power>
+ </payload_deck>
+ </payload_decks>
+ </payload_tube>
+ </fuselage_accommodation>
+ </fuselage>
+ </geometry>
+ </specific>
+ </fuselage>
+ <wing>
+ <mass_properties description="mass_properties of component wing">
+ <mass description="component mass">
+ <value>5899.686597</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="component inertia referred to local center of gravity">
+ <j_xx description="wing inertia in x">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xx>
+ <j_yy description="wing inertia in y">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yy>
+ <j_zz description="wing inertia in z">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zz>
+ <j_xy description="wing inertia in xy">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xy>
+ <j_xz description="wing inertia in xz">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xz>
+ <j_yx description="wing inertia in yx">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yx>
+ <j_yz description="wing inertia in yz">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yz>
+ <j_zx description="wing inertia in zx">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zx>
+ <j_zy description="wing inertia in zy">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="component center of gravity with respect to global coordinate system">
+ <x description="x position of center of gravity">
+ <value>16.97777054</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y position of center of gravity">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z position of center of gravity">
+ <value>-0.6705636773</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <position description="position of wing">
+ <x description="x position">
+ <value>13.15649787</value>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y position">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </y>
+ <z description="z position">
+ <value>-1.030445071</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </position>
+ <specific>
+ <geometry>
+ <aerodynamic_surface ID="0" description="main_wing">
+ <name description="name of surface">
+ <value>main_wing</value>
+ </name>
+ <position description="reference position in aircraft coordinates">
+ <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>
+ </position>
+ <parameters description="aerodynamic surface parameters">
+ <direction description="unit vector according to aircraft 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>
+ </direction>
+ <symmetric description="symmetric to local x-z plane">
+ <value>true</value>
+ </symmetric>
+ <sections description="sections">
+ <section ID="0">
+ <chord_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>
+ </chord_origin>
+ <chord_length description="chord length of the section">
+ <value>5.622599153</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>
+ <scale_thickness description="scale the thickness defined by the profile with this factor">
+ <value>1.36425648</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </scale_thickness>
+ <profile description="profile (data normalized to chord length)">
+ <value>F15</value>
+ </profile>
+ </section>
+ <section ID="1">
+ <chord_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>-1.983993414</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </chord_origin>
+ <chord_length description="chord length of the section">
+ <value>5.622599153</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>
+ <scale_thickness description="scale the thickness defined by the profile with this factor">
+ <value>1.36425648</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </scale_thickness>
+ <profile description="profile (data normalized to chord length)">
+ <value>F15</value>
+ </profile>
+ </section>
+ <section ID="2">
+ <chord_origin description="origin of chord (local)">
+ <x description="x coordinate of point">
+ <value>1.956243826</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>0.2585733096</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>-4.939499866</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </chord_origin>
+ <chord_length description="chord length of the section">
+ <value>3.821246858</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>
+ <scale_thickness description="scale the thickness defined by the profile with this factor">
+ <value>1.255091095</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </scale_thickness>
+ <profile description="profile (data normalized to chord length)">
+ <value>F15</value>
+ </profile>
+ </section>
+ <section ID="3">
+ <chord_origin description="origin of chord (local)">
+ <x description="x coordinate of point">
+ <value>8.545130477</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>1.266923874</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>-16.46499955</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </chord_origin>
+ <chord_length description="chord length of the section">
+ <value>0.9558418561</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>
+ <scale_thickness description="scale the thickness defined by the profile with this factor">
+ <value>0.8293821242</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </scale_thickness>
+ <profile description="profile (data normalized to chord length)">
+ <value>F15</value>
+ </profile>
+ </section>
+ </sections>
+ <spars>
+ <spar ID="0" description="front_spar">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ </spar>
+ <spar ID="1" description="rear_spar">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ </spar>
+ </spars>
+ <control_devices>
+ <control_device ID="0" description="slat">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.122907582</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.294</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ <deflection>
+ <full_negative_deflection description="full negative deflection">
+ <value>0</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>0.6981317008</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ </control_device>
+ <control_device ID="1" description="slat">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.306</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.95</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ <deflection>
+ <full_negative_deflection description="full negative deflection">
+ <value>0</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>0.6981317008</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ </control_device>
+ <control_device ID="2" description="flap_fowler">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.75</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.122907582</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.75</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.297</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ <deflection>
+ <full_negative_deflection description="full negative deflection">
+ <value>0</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>0.7853981634</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ </control_device>
+ <control_device ID="3" description="flap_fowler">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.75</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.303</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.75</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.78</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ <deflection>
+ <full_negative_deflection description="full negative deflection">
+ <value>0</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>0.7853981634</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ </control_device>
+ <control_device ID="4" description="aileron">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.8</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.98</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ <deflection>
+ <full_negative_deflection description="full negative deflection">
+ <value>-0.3490658504</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>0.3490658504</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ </control_device>
+ <control_device ID="5" description="spoiler_ground">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.85</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.208453791</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.85</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.294</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ <deflection>
+ <full_negative_deflection description="full negative deflection">
+ <value>0</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>0.7853981634</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ </control_device>
+ <control_device ID="6" description="spoiler_air">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.85</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.306</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.85</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.4195</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ <deflection>
+ <full_negative_deflection description="full negative deflection">
+ <value>0</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>0.7853981634</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ </control_device>
+ <control_device ID="7" description="spoiler_air">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.85</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.4195</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.85</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.533</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ <deflection>
+ <full_negative_deflection description="full negative deflection">
+ <value>0</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>0.7853981634</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ </control_device>
+ <control_device ID="8" description="spoiler_air">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.85</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.533</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.85</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.6465</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ <deflection>
+ <full_negative_deflection description="full negative deflection">
+ <value>0</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>0.7853981634</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ </control_device>
+ <control_device ID="9" description="spoiler_air">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.85</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.6465</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.85</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.76</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ <deflection>
+ <full_negative_deflection description="full negative deflection">
+ <value>0</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>0.7853981634</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ </control_device>
+ </control_devices>
+ </parameters>
+ </aerodynamic_surface>
+ </geometry>
+ </specific>
+ </wing>
+ <empennage>
+ <position description="position of empennage">
+ <x description="x position">
+ <value>30.44658691</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </x>
+ <y description="y position">
+ <value>0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </y>
+ <z description="z position">
+ <value>0.92429206</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </position>
+ <mass_properties description="mass_properties of component Conventional tail overall mass">
+ <mass description="component mass">
+ <value>903.1495027</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="component inertia referred to local center of gravity">
+ <j_xx description="Conventional tail overall mass inertia in x">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xx>
+ <j_yy description="Conventional tail overall mass inertia in y">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yy>
+ <j_zz description="Conventional tail overall mass inertia in z">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zz>
+ <j_xy description="Conventional tail overall mass inertia in xy">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xy>
+ <j_xz description="Conventional tail overall mass inertia in xz">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xz>
+ <j_yx description="Conventional tail overall mass inertia in yx">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yx>
+ <j_yz description="Conventional tail overall mass inertia in yz">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yz>
+ <j_zx description="Conventional tail overall mass inertia in zx">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zx>
+ <j_zy description="Conventional tail overall mass inertia in zy">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="component center of gravity with respect to global coordinate system">
+ <x description="x position of center of gravity">
+ <value>34.58488958</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y position of center of gravity">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z position of center of gravity">
+ <value>3.050854727</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="vertical_stabiliser">
+ <name description="name of surface">
+ <value>vertical_stabiliser</value>
+ </name>
+ <position description="reference position in aircraft coordinates">
+ <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>
+ </position>
+ <parameters description="aerodynamic surface parameters">
+ <direction description="unit vector according to aircraft 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>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>
+ </direction>
+ <symmetric description="symmetric to local x-z plane">
+ <value>false</value>
+ </symmetric>
+ <sections description="sections">
+ <section ID="0">
+ <chord_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>
+ </chord_origin>
+ <chord_length description="chord length of the section">
+ <value>5.071328227</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>
+ <scale_thickness description="scale the thickness defined by the profile with this factor">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </scale_thickness>
+ <profile description="profile (data normalized to chord length)">
+ <value>n0012</value>
+ </profile>
+ </section>
+ <section ID="1">
+ <chord_origin description="origin of chord (local)">
+ <x description="x coordinate of point">
+ <value>5.351645488</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>-6.608731805</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </chord_origin>
+ <chord_length description="chord length of the section">
+ <value>1.344916246</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>
+ <scale_thickness description="scale the thickness defined by the profile with this factor">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </scale_thickness>
+ <profile description="profile (data normalized to chord length)">
+ <value>n0012</value>
+ </profile>
+ </section>
+ </sections>
+ <spars>
+ <spar ID="0" description="front_spar">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ </spar>
+ <spar ID="1" description="rear_spar">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ </spar>
+ </spars>
+ <control_devices>
+ <control_device ID="0" description="rudder">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.9</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ <deflection>
+ <full_negative_deflection description="full negative deflection">
+ <value>-0.4363323125</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>0.4363323125</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ </control_device>
+ </control_devices>
+ </parameters>
+ </aerodynamic_surface>
+ <aerodynamic_surface ID="1" description="horizontal_stabiliser">
+ <name description="name of surface">
+ <value>horizontal_stabiliser</value>
+ </name>
+ <position description="reference position in aircraft coordinates">
+ <x description="x coordinate of point">
+ <value>2.348595458</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>-0.5869147714</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </position>
+ <parameters description="aerodynamic surface parameters">
+ <direction description="unit vector according to aircraft 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>
+ </direction>
+ <symmetric description="symmetric to local x-z plane">
+ <value>true</value>
+ </symmetric>
+ <sections description="sections">
+ <section ID="0">
+ <chord_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>
+ </chord_origin>
+ <chord_length description="chord length of the section">
+ <value>3.22273277</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>
+ <scale_thickness description="scale the thickness defined by the profile with this factor">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </scale_thickness>
+ <profile description="profile (data normalized to chord length)">
+ <value>n0012</value>
+ </profile>
+ </section>
+ <section ID="1">
+ <chord_origin description="origin of chord (local)">
+ <x description="x coordinate of point">
+ <value>3.523890414</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>0.4933838767</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>-5.639403513</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </chord_origin>
+ <chord_length description="chord length of the section">
+ <value>0.9094551877</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>
+ <scale_thickness description="scale the thickness defined by the profile with this factor">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </scale_thickness>
+ <profile description="profile (data normalized to chord length)">
+ <value>n0012</value>
+ </profile>
+ </section>
+ </sections>
+ <spars>
+ <spar ID="0" description="front_spar">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ </spar>
+ <spar ID="1" description="rear_spar">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>0.6</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ </spar>
+ </spars>
+ <control_devices>
+ <control_device ID="0" description="elevator">
+ <position description="relative chord position">
+ <inner_position description="relative inner position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.2</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </inner_position>
+ <outer_position description="relative outer position">
+ <chord description="chord position">
+ <from description="relative chord position">
+ <value>0.7</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </from>
+ <to description="relative chord position">
+ <value>1</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </to>
+ </chord>
+ <spanwise description="relative spanwise position">
+ <value>-0.9</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </spanwise>
+ </outer_position>
+ </position>
+ <deflection>
+ <full_negative_deflection description="full negative deflection">
+ <value>-0.4363323125</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_negative_deflection>
+ <full_positive_deflection description="full positive deflection">
+ <value>0.4363323125</value>
+ <unit>rad</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </full_positive_deflection>
+ </deflection>
+ </control_device>
+ </control_devices>
+ </parameters>
+ </aerodynamic_surface>
+ </geometry>
+ </specific>
+ </empennage>
+ <tank description="Description of aircraft tanks." tool_level="2">
+ <position description="Tank reference point, 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>13.15649787</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>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-40</lower_boundary>
+ <upper_boundary>40</upper_boundary>
+ </y>
+ <z description="Distance between the foremost middle tank end and the global reference point in z-direction.">
+ <value>-1.030445071</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>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</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>0.0</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>0.0</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>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <specific description="Tank design specific output parameter.">
+ <additional_fuselage_length description="Additional fuselage length (if smaller than 0: shrink fuselage, if greater than 0: stretch fuselage).">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </additional_fuselage_length>
+ <tank ID="0" description="Description of one tank.">
+ <name description="Name of the tank.">
+ <value>tank_0</value>
+ </name>
+ <designator description="Designator of the tank.">
+ <value>wing_inner_left</value>
+ </designator>
+ <position description="Local reference point, position of one tank wrt. the tank reference point.">
+ <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+ <value>-0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-80</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+ <value>1.124519831</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 tank reference point in z-direction.">
+ <value>1.983993414</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="X component of the unit vector.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </x>
+ <y description="Y component of the unit vector.">
+ <value>1</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </y>
+ <z description="Z component of the unit vector.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </z>
+ </direction>
+ <mass_properties description="Mass properties of one tank.">
+ <mass description="Total dry mass of one tank.">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia of one tank with regard to its center of gravity.">
+ <j_xx description="Inertia of the 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 the 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 the 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>0.0</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>0.0</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>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ <centroid description="Centroid of one tank.">
+ <x description="Centroid in x-direction with regard to the local reference point.">
+ <value>1.010691405</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Centroid in y-direction with regard to the local reference point.">
+ <value>2.452697049</value>
+ <unit>m</unit>
+ <lower_boundary>-40</lower_boundary>
+ <upper_boundary>40</upper_boundary>
+ </y>
+ <z description="Centroid in z-direction with regard to the local reference point.">
+ <value>0.341108349</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </centroid>
+ </mass_properties>
+ <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+ <value>1.19652444e+11</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </maximum_energy_capacity>
+ <geometry description="Geometrical description of one tank.">
+ <cross_section ID="0" description="Geometrical description of one tank cross section.">
+ <name description="Name of tank cross section.">
+ <value>tank_section_0</value>
+ </name>
+ <position description="Position of tank cross section with regard to the local reference point.">
+ <x description="Distance between the tank cross section and the local reference point in x-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-80</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the tank cross section and the local reference point in y-direction.">
+ <value>0.0</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 local reference point in z-direction.">
+ <value>0.0</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>0.759050885655</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>2.2490396612</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </width>
+ <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </length>
+ </cross_section>
+ <cross_section ID="1" description="Geometrical description of one tank cross section.">
+ <name description="Name of tank cross section.">
+ <value>tank_section_1</value>
+ </name>
+ <position description="Position of tank cross section with regard to the local reference point.">
+ <x description="Distance between the tank cross section and the local reference point in x-direction.">
+ <value>1.956243826</value>
+ <unit>m</unit>
+ <lower_boundary>-80</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the tank cross section and the local reference point in y-direction.">
+ <value>-0.101697149</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 local reference point in z-direction.">
+ <value>2.955506452</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>0.51586832583</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>1.5284987431999997</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </width>
+ <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </length>
+ </cross_section>
+ </geometry>
+ </tank>
+ <tank ID="1" description="Description of one tank.">
+ <name description="Name of the tank.">
+ <value>tank_1</value>
+ </name>
+ <designator description="Designator of the tank.">
+ <value>wing_outer_left</value>
+ </designator>
+ <position description="Local reference point, position of one tank wrt. the tank reference point.">
+ <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+ <value>1.956243826</value>
+ <unit>m</unit>
+ <lower_boundary>-80</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+ <value>1.022822681</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 tank reference point in z-direction.">
+ <value>4.939499866</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="X component of the unit vector.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </x>
+ <y description="Y component of the unit vector.">
+ <value>1</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </y>
+ <z description="Z component of the unit vector.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </z>
+ </direction>
+ <mass_properties description="Mass properties of one tank.">
+ <mass description="Total dry mass of one tank.">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia of one tank with regard to its center of gravity.">
+ <j_xx description="Inertia of the 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 the 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 the 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>0.0</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>0.0</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>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ <centroid description="Centroid of one tank.">
+ <x description="Centroid in x-direction with regard to the local reference point.">
+ <value>0.695636688</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Centroid in y-direction with regard to the local reference point.">
+ <value>-5.232975698</value>
+ <unit>m</unit>
+ <lower_boundary>-40</lower_boundary>
+ <upper_boundary>40</upper_boundary>
+ </y>
+ <z description="Centroid in z-direction with regard to the local reference point.">
+ <value>0.234777382</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </centroid>
+ </mass_properties>
+ <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+ <value>1.319256243e+11</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </maximum_energy_capacity>
+ <geometry description="Geometrical description of one tank.">
+ <cross_section ID="0" description="Geometrical description of one tank cross section.">
+ <name description="Name of tank cross section.">
+ <value>tank_section_0</value>
+ </name>
+ <position description="Position of tank cross section with regard to the local reference point.">
+ <x description="Distance between the tank cross section and the local reference point in x-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-80</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the tank cross section and the local reference point in y-direction.">
+ <value>0.0</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 local reference point in z-direction.">
+ <value>0.0</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>0.51586832583</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>1.5284987431999997</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </width>
+ <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </length>
+ </cross_section>
+ <cross_section ID="1" description="Geometrical description of one tank cross section.">
+ <name description="Name of tank cross section.">
+ <value>tank_section_1</value>
+ </name>
+ <position description="Position of tank cross section with regard to the local reference point.">
+ <x description="Distance between the tank cross section and the local reference point in x-direction.">
+ <value>6.4287401</value>
+ <unit>m</unit>
+ <lower_boundary>-80</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the tank cross section and the local reference point in y-direction.">
+ <value>0.328341364</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 local reference point in z-direction.">
+ <value>-18.569499866</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>0.22406712114432425</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>0.6639025811683681</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </width>
+ <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </length>
+ </cross_section>
+ </geometry>
+ </tank>
+ <tank ID="2" description="Description of one tank.">
+ <name description="Name of the tank.">
+ <value>tank_2</value>
+ </name>
+ <designator description="Designator of the tank.">
+ <value>wing_inner_right</value>
+ </designator>
+ <position description="Local reference point, position of one tank wrt. the tank reference point.">
+ <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-80</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+ <value>1.124519831</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 tank reference point in z-direction.">
+ <value>-1.983993414</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="X component of the unit vector.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </x>
+ <y description="Y component of the unit vector.">
+ <value>1</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </y>
+ <z description="Z component of the unit vector.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </z>
+ </direction>
+ <mass_properties description="Mass properties of one tank.">
+ <mass description="Total dry mass of one tank.">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia of one tank with regard to its center of gravity.">
+ <j_xx description="Inertia of the 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 the 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 the 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>0.0</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>0.0</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>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ <centroid description="Centroid of one tank.">
+ <x description="Centroid in x-direction with regard to the local reference point.">
+ <value>1.010691405</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Centroid in y-direction with regard to the local reference point.">
+ <value>-2.452697049</value>
+ <unit>m</unit>
+ <lower_boundary>-40</lower_boundary>
+ <upper_boundary>40</upper_boundary>
+ </y>
+ <z description="Centroid in z-direction with regard to the local reference point.">
+ <value>0.341108349</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </centroid>
+ </mass_properties>
+ <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+ <value>1.19652444e+11</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </maximum_energy_capacity>
+ <geometry description="Geometrical description of one tank.">
+ <cross_section ID="0" description="Geometrical description of one tank cross section.">
+ <name description="Name of tank cross section.">
+ <value>tank_section_0</value>
+ </name>
+ <position description="Position of tank cross section with regard to the local reference point.">
+ <x description="Distance between the tank cross section and the local reference point in x-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-80</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the tank cross section and the local reference point in y-direction.">
+ <value>0.0</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 local reference point in z-direction.">
+ <value>0.0</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>0.759050885655</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>2.2490396612</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </width>
+ <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </length>
+ </cross_section>
+ <cross_section ID="1" description="Geometrical description of one tank cross section.">
+ <name description="Name of tank cross section.">
+ <value>tank_section_1</value>
+ </name>
+ <position description="Position of tank cross section with regard to the local reference point.">
+ <x description="Distance between the tank cross section and the local reference point in x-direction.">
+ <value>1.956243826</value>
+ <unit>m</unit>
+ <lower_boundary>-80</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the tank cross section and the local reference point in y-direction.">
+ <value>-0.101697149</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 local reference point in z-direction.">
+ <value>-2.955506452</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>0.51586832583</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>1.5284987431999997</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </width>
+ <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </length>
+ </cross_section>
+ </geometry>
+ </tank>
+ <tank ID="3" description="Description of one tank.">
+ <name description="Name of the tank.">
+ <value>tank_3</value>
+ </name>
+ <designator description="Designator of the tank.">
+ <value>wing_outer_right</value>
+ </designator>
+ <position description="Local reference point, position of one tank wrt. the tank reference point.">
+ <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+ <value>1.956243826</value>
+ <unit>m</unit>
+ <lower_boundary>-80</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+ <value>1.022822681</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 tank reference point in z-direction.">
+ <value>-4.939499866</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="X component of the unit vector.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </x>
+ <y description="Y component of the unit vector.">
+ <value>1</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </y>
+ <z description="Z component of the unit vector.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </z>
+ </direction>
+ <mass_properties description="Mass properties of one tank.">
+ <mass description="Total dry mass of one tank.">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia of one tank with regard to its center of gravity.">
+ <j_xx description="Inertia of the 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 the 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 the 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>0.0</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>0.0</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>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ <centroid description="Centroid of one tank.">
+ <x description="Centroid in x-direction with regard to the local reference point.">
+ <value>0.695636688</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Centroid in y-direction with regard to the local reference point.">
+ <value>5.232975698</value>
+ <unit>m</unit>
+ <lower_boundary>-40</lower_boundary>
+ <upper_boundary>40</upper_boundary>
+ </y>
+ <z description="Centroid in z-direction with regard to the local reference point.">
+ <value>0.234777382</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </centroid>
+ </mass_properties>
+ <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+ <value>1.319256243e+11</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </maximum_energy_capacity>
+ <geometry description="Geometrical description of one tank.">
+ <cross_section ID="0" description="Geometrical description of one tank cross section.">
+ <name description="Name of tank cross section.">
+ <value>tank_section_0</value>
+ </name>
+ <position description="Position of tank cross section with regard to the local reference point.">
+ <x description="Distance between the tank cross section and the local reference point in x-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-80</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the tank cross section and the local reference point in y-direction.">
+ <value>0.0</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 local reference point in z-direction.">
+ <value>0.0</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>0.51586832583</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>1.5284987431999997</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </width>
+ <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </length>
+ </cross_section>
+ <cross_section ID="1" description="Geometrical description of one tank cross section.">
+ <name description="Name of tank cross section.">
+ <value>tank_section_1</value>
+ </name>
+ <position description="Position of tank cross section with regard to the local reference point.">
+ <x description="Distance between the tank cross section and the local reference point in x-direction.">
+ <value>6.4287401</value>
+ <unit>m</unit>
+ <lower_boundary>-80</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the tank cross section and the local reference point in y-direction.">
+ <value>0.328341364</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 local reference point in z-direction.">
+ <value>18.569499866</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>0.22406712114432425</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>0.6639025811683681</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </width>
+ <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </length>
+ </cross_section>
+ </geometry>
+ </tank>
+ <tank ID="4" description="Description of one tank.">
+ <name description="Name of the tank.">
+ <value>tank_4</value>
+ </name>
+ <designator description="Designator of the tank.">
+ <value>wing_center</value>
+ </designator>
+ <position description="Local reference point, position of one tank wrt. the tank reference point.">
+ <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-80</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+ <value>1.124519831</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 tank reference point in z-direction.">
+ <value>0.0</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="X component of the unit vector.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </x>
+ <y description="Y component of the unit vector.">
+ <value>1</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </y>
+ <z description="Z component of the unit vector.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </z>
+ </direction>
+ <mass_properties description="Mass properties of one tank.">
+ <mass description="Total dry mass of one tank.">
+ <value>0.0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia of one tank with regard to its center of gravity.">
+ <j_xx description="Inertia of the 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 the 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 the 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>0.0</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>0.0</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>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </center_of_gravity>
+ <centroid description="Centroid of one tank.">
+ <x description="Centroid in x-direction with regard to the local reference point.">
+ <value>1.124519831</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Centroid in y-direction with regard to the local reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-40</lower_boundary>
+ <upper_boundary>40</upper_boundary>
+ </y>
+ <z description="Centroid in z-direction with regard to the local reference point.">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-5</lower_boundary>
+ <upper_boundary>5</upper_boundary>
+ </z>
+ </centroid>
+ </mass_properties>
+ <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+ <value>2.167864117e+11</value>
+ <unit>J</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </maximum_energy_capacity>
+ <geometry description="Geometrical description of one tank.">
+ <cross_section ID="0" description="Geometrical description of one tank cross section.">
+ <name description="Name of tank cross section.">
+ <value>tank_section_0</value>
+ </name>
+ <position description="Position of tank cross section with regard to the local reference point.">
+ <x description="Distance between the tank cross section and the local reference point in x-direction.">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-80</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the tank cross section and the local reference point in y-direction.">
+ <value>-0.0</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 local reference point in z-direction.">
+ <value>-0.98207674</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>0.759050885655</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>2.2490396612</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </width>
+ <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </length>
+ </cross_section>
+ <cross_section ID="1" description="Geometrical description of one tank cross section.">
+ <name description="Name of tank cross section.">
+ <value>tank_section_1</value>
+ </name>
+ <position description="Position of tank cross section with regard to the local reference point.">
+ <x description="Distance between the tank cross section and the local reference point in x-direction.">
+ <value>-0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-80</lower_boundary>
+ <upper_boundary>80</upper_boundary>
+ </x>
+ <y description="Distance between the tank cross section and the local reference point in y-direction.">
+ <value>0.0</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 local reference point in z-direction.">
+ <value>0.98207674</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>0.759050885655</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </height>
+ <width description="Width of the cross section.">
+ <value>2.2490396612</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </width>
+ <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </length>
+ </cross_section>
+ </geometry>
+ </tank>
+ </specific>
+ </tank>
+ <propulsion>
+ <position description="Reference position of the propulsion assembly">
+ <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>
+ </position>
+ <mass_properties description="Mass properties of the propulsion assembly">
+ <mass description="mass of the of the component">
+ <value>8163.723809</value>
+ <unit>kg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia of the component in respect to the CG">
+ <j_xx description="inertia of the component">
+ <value>291227.1488</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia of the component">
+ <value>9415.034095</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia of the component">
+ <value>293993.4407</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia of the component">
+ <value>-9.734017667</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia of the component">
+ <value>1640.24539</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia of the component">
+ <value>-9.734017667</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia of the component">
+ <value>-10.88764113</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia of the component">
+ <value>1640.24539</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia of the component">
+ <value>-10.88764113</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+ <x description="x coordinate of the center of gravity">
+ <value>14.88163757</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </x>
+ <y description="y coordinate of the center of gravity">
+ <value>0.00753679453</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </y>
+ <z description="z coordinate of the center of gravity">
+ <value>-2.361935723</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <specific>
+ <propulsion ID="0" description="Description of one propulsion">
+ <nacelle ID="0" description="Nacelle of the propulsion assembly">
+ <position description="Origin of the nacelle RELATIVE to the engine position.">
+ <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>
+ </position>
+ <normal description="Normal direction of the nacelle in the global aircraft coordinate system">
+ <x description="x direction of unit vector">
+ <value>1</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>0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </normal>
+ <sections description="Geometrical description 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>2.117450668</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>2.117450668</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>nacelle</value>
+ </profile>
+ </section>
+ <section ID="1">
+ <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>0.8175031883</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>2.646813335</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>2.646813335</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>nacelle</value>
+ </profile>
+ </section>
+ <section ID="2">
+ <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>2.452509565</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>2.646813335</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>2.646813335</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>nacelle</value>
+ </profile>
+ </section>
+ <section ID="3">
+ <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>3.270012753</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>2.117450668</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>2.117450668</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>nacelle</value>
+ </profile>
+ </section>
+ </sections>
+ <mass_properties description="Mass properties of the nacelle">
+ <mass description="mass of the of the component">
+ <value>1021.17164</value>
+ <unit>kg</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </mass>
+ <inertia description="Inertia of the component in respect to the CG">
+ <j_xx description="inertia of the component">
+ <value>41.37265694</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia of the component">
+ <value>42.89384826</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia of the component">
+ <value>42.93889432</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia of the component">
+ <value>-8.648443839e-05</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia of the component">
+ <value>-0.01261898096</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia of the component">
+ <value>-8.648443839e-05</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia of the component">
+ <value>-0.005393592727</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia of the component">
+ <value>-0.01261898096</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia of the component">
+ <value>-0.005393592727</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+ <x description="x coordinate of the center of gravity">
+ <value>14.72478543</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </x>
+ <y description="y coordinate of the center of gravity">
+ <value>-5.893109505</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </y>
+ <z description="z coordinate of the center of gravity">
+ <value>-2.538575351</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </nacelle>
+ <pylon ID="0" description="pylon of the propulsion assembly">
+ <position description="Position of the pylon RELATIVE to the engine position.">
+ <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>
+ </position>
+ <normal description="unit vector according to aircraft 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>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>-1.058725334</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </normal>
+ <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>1.296564592e-16</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>-1.058725334</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>3.270012753</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>pylon</value>
+ </profile>
+ </section>
+ <section ID="1">
+ <origin description="origin of chord (local)">
+ <x description="x coordinate of point">
+ <value>2.585343883</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>2.268988035e-16</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>-1.852769335</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>3.270012753</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>pylon</value>
+ </profile>
+ </section>
+ </sections>
+ <mass_properties description="Mass properties of the pylon">
+ <mass description="mass of the of the component">
+ <value>495.2910093</value>
+ <unit>kg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia of the component in respect to the CG">
+ <j_xx description="inertia of the component">
+ <value>0.4759428482</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia of the component">
+ <value>10.28599176</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia of the component">
+ <value>10.0164363</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia of the component">
+ <value>-0.04149876619</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia of the component">
+ <value>1.188151703</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia of the component">
+ <value>-0.04149876619</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia of the component">
+ <value>-0.00425818292</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia of the component">
+ <value>1.188151703</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia of the component">
+ <value>-0.00425818292</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+ <x description="x coordinate of the center of gravity">
+ <value>16.01745737</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y coordinate of the center of gravity">
+ <value>-5.923235836</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z coordinate of the center of gravity">
+ <value>-1.082828016</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </pylon>
+ <engine>
+ <model description="Name of selected engine model">
+ <value>PW1127G-JM</value>
+ </model>
+ <position description="Position of the engine in the global coordinate system">
+ <x description="x coordinate of point">
+ <value>13.08977905</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>-5.923235836</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>-2.538575351</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </position>
+ <mass_properties description="Mass properties of the engine">
+ <mass description="mass of the of the component">
+ <value>2565.399255</value>
+ <unit>kg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia of the component in respect to the CG">
+ <j_xx description="inertia of the component">
+ <value>1437.777157</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia of the component">
+ <value>3004.86955</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia of the component">
+ <value>3004.86955</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia of the component">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia of the component">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia of the component">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia of the component">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia of the component">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia of the component">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+ <x description="x coordinate of the center of gravity">
+ <value>14.72478543</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y coordinate of the center of gravity">
+ <value>-5.923235836</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z coordinate of the center of gravity">
+ <value>-2.538575351</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <SLST description="Sea level static thrust of the engine">
+ <value>109167.0872</value>
+ <unit>N</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </SLST>
+ <scale_factor description="Scale factor of the engine">
+ <value>0.9064775155</value>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </scale_factor>
+ <bucket_point description="Bucket point of the engine at initial cruise flight phase">
+ <thrust description="Thrust of the engine at the bucket point">
+ <value>18391.6134</value>
+ <unit>N</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </thrust>
+ <tsfc description="Thrust specific fuel consumption of the engine at the bucket point">
+ <value>1.407077304e-05</value>
+ <unit>kg/Ns</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </tsfc>
+ </bucket_point>
+ </engine>
+ </propulsion>
+ <propulsion ID="1" description="Description of one propulsion">
+ <nacelle ID="0" description="Nacelle of the propulsion assembly">
+ <position description="Origin of the nacelle RELATIVE to the engine position.">
+ <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>
+ </position>
+ <normal description="Normal direction of the nacelle in the global aircraft coordinate system">
+ <x description="x direction of unit vector">
+ <value>1</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>0</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </normal>
+ <sections description="Geometrical description 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>2.117450668</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>2.117450668</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>nacelle</value>
+ </profile>
+ </section>
+ <section ID="1">
+ <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>0.8175031883</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>2.646813335</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>2.646813335</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>nacelle</value>
+ </profile>
+ </section>
+ <section ID="2">
+ <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>2.452509565</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>2.646813335</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>2.646813335</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>nacelle</value>
+ </profile>
+ </section>
+ <section ID="3">
+ <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>3.270012753</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>2.117450668</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>2.117450668</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>nacelle</value>
+ </profile>
+ </section>
+ </sections>
+ <mass_properties description="Mass properties of the nacelle">
+ <mass description="mass of the of the component">
+ <value>1021.17164</value>
+ <unit>kg</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </mass>
+ <inertia description="Inertia of the component in respect to the CG">
+ <j_xx description="inertia of the component">
+ <value>41.37265694</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia of the component">
+ <value>42.89384826</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia of the component">
+ <value>42.93889432</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia of the component">
+ <value>-8.648443839e-05</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia of the component">
+ <value>-0.01261898096</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia of the component">
+ <value>-8.648443839e-05</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia of the component">
+ <value>-0.005393592727</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia of the component">
+ <value>-0.01261898096</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia of the component">
+ <value>-0.005393592727</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+ <x description="x coordinate of the center of gravity">
+ <value>14.72478543</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </x>
+ <y description="y coordinate of the center of gravity">
+ <value>5.953362166</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </y>
+ <z description="z coordinate of the center of gravity">
+ <value>-2.538575351</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </nacelle>
+ <pylon ID="0" description="pylon of the propulsion assembly">
+ <position description="Position of the pylon RELATIVE to the engine position.">
+ <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>
+ </position>
+ <normal description="unit vector according to aircraft 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>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>-1.058725334</value>
+ <unit>1</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </normal>
+ <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>1.296564592e-16</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>-1.058725334</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>3.270012753</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>pylon</value>
+ </profile>
+ </section>
+ <section ID="1">
+ <origin description="origin of chord (local)">
+ <x description="x coordinate of point">
+ <value>2.585343883</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>2.268988035e-16</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>-1.852769335</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>3.270012753</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>pylon</value>
+ </profile>
+ </section>
+ </sections>
+ <mass_properties description="Mass properties of the pylon">
+ <mass description="mass of the of the component">
+ <value>495.2910093</value>
+ <unit>kg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia of the component in respect to the CG">
+ <j_xx description="inertia of the component">
+ <value>0.4759428482</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia of the component">
+ <value>10.28599176</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia of the component">
+ <value>10.0164363</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia of the component">
+ <value>-0.04149876619</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia of the component">
+ <value>1.188151703</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia of the component">
+ <value>-0.04149876619</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia of the component">
+ <value>-0.00425818292</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia of the component">
+ <value>1.188151703</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia of the component">
+ <value>-0.00425818292</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+ <x description="x coordinate of the center of gravity">
+ <value>16.01745737</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y coordinate of the center of gravity">
+ <value>5.923235836</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z coordinate of the center of gravity">
+ <value>-1.082828016</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </pylon>
+ <engine>
+ <model description="Name of selected engine model">
+ <value>PW1127G-JM</value>
+ </model>
+ <position description="Position of the engine in the global coordinate system">
+ <x description="x coordinate of point">
+ <value>13.08977905</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>5.923235836</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>-2.538575351</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </position>
+ <mass_properties description="Mass properties of the engine">
+ <mass description="mass of the of the component">
+ <value>2565.399255</value>
+ <unit>kg</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia of the component in respect to the CG">
+ <j_xx description="inertia of the component">
+ <value>1437.777157</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xx>
+ <j_yy description="inertia of the component">
+ <value>3004.86955</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yy>
+ <j_zz description="inertia of the component">
+ <value>3004.86955</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zz>
+ <j_xy description="inertia of the component">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xy>
+ <j_xz description="inertia of the component">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xz>
+ <j_yx description="inertia of the component">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yx>
+ <j_yz description="inertia of the component">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yz>
+ <j_zx description="inertia of the component">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zx>
+ <j_zy description="inertia of the component">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+ <x description="x coordinate of the center of gravity">
+ <value>14.72478543</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </x>
+ <y description="y coordinate of the center of gravity">
+ <value>5.923235836</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </y>
+ <z description="z coordinate of the center of gravity">
+ <value>-2.538575351</value>
+ <unit>m</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <SLST description="Sea level static thrust of the engine">
+ <value>109167.0872</value>
+ <unit>N</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </SLST>
+ <scale_factor description="Scale factor of the engine">
+ <value>0.9064775155</value>
+ <unit>1</unit>
+ <lower_boundary>-inf</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </scale_factor>
+ <bucket_point description="Bucket point of the engine at initial cruise flight phase">
+ <thrust description="Thrust of the engine at the bucket point">
+ <value>18391.6134</value>
+ <unit>N</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </thrust>
+ <tsfc description="Thrust specific fuel consumption of the engine at the bucket point">
+ <value>1.407077304e-05</value>
+ <unit>kg/Ns</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </tsfc>
+ </bucket_point>
+ </engine>
+ </propulsion>
+ </specific>
+ </propulsion>
+ <landing_gear description="Geometric description of the aircraft undercarriage." tool_level="1">
+ <position description="Position of the total undercarriage arrangement with regard to the global reference point.">
+ <x description="Distance in x direction with regard to the global reference point. (total undercarriage arrangement)">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the global reference point. (total undercarriage arrangement)">
+ <value>0.0</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. (total undercarriage arrangement)">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </position>
+ <mass_properties description="Mass properties of the total undercarriage arrangement.">
+ <mass description="Mass of the total undercarriage arrangement.">
+ <value>2558.0104</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </mass>
+ <inertia description="Inertia of the total undercarriage arrangement with regard to the total center of gravity.">
+ <j_xx description="Inertia of the total undercarriage arrangement 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 arrangement 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 arrangement 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 arrangement 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 arrangement 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 arrangement 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 arrangement 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 arrangement 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 arrangement 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 arrangement.">
+ <x description="Center of gravity in x-direction with regard to the global reference point. (total undercarriage arrangement)">
+ <value>18.9592</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Center of gravity in y-direction with regard to the global reference point. (total undercarriage arrangement)">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Center of gravity in z-direction with regard to the global reference point. (total undercarriage arrangement)">
+ <value>-1.5956</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <aircraft_classification_number description="Aircraft classification number for the total undercarriage arrangement. (CBR = [3, 6, 10, 15])">
+ <value>[45.9, 40.2, 36.7, 35.3]</value>
+ </aircraft_classification_number>
+ <specific description="Landing gear specific output parameter.">
+ <geometry description="Geometry description of the entire landing gear.">
+ <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_assembly</value>
+ </name>
+ <position description="Position of one entire landing gear leg with regard to the landing gear global position.">
+ <x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)">
+ <value>5.8</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the landing gear global position. (center line of the landing gear leg)">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the landing gear global position. (center line of the landing gear leg)">
+ <value>-1.4712</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</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>393.4109</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 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 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 landing gear center of gravity position. (entire landing gear leg)">
+ <value>-13.8761</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Center of gravity in x-direction with regard to the global landing gear enter of gravity position. (entire landing gear leg)">
+ <value>0.0</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+ <value>0.1244</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <assembly_components description="Geometrical description of the assembly components of one landing gear strut.">
+ <strut_diameter description="Diameter of the landing gear strut">
+ <value>0.2248</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </strut_diameter>
+ <strut_length description="Length of the landing gear strut">
+ <value>1.4339</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </strut_length>
+ <tire_description ID="0" description="Description of one tire of the wheel group.">
+ <name description="Name of the tire type.">
+ <value>APS01203</value>
+ </name>
+ <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+ <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+ <value>0.0</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 landing gear strut position. (center line of the landing gear strut">
+ <value>-0.3372</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+ <value>-1.4339</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </position>
+ <tire_diameter description="Diameter of one tire of the wheel group.">
+ <value>0.7699</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>2</upper_boundary>
+ </tire_diameter>
+ <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+ <value>0.2248</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </tire_section_width>
+ </tire_description>
+ <tire_description ID="1" description="Description of one tire of the wheel group.">
+ <name description="Name of the tire type.">
+ <value>APS01203</value>
+ </name>
+ <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+ <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+ <value>0.0</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 landing gear strut position. (center line of the landing gear strut">
+ <value>0.3372</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+ <value>-1.4339</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </position>
+ <tire_diameter description="Diameter of one tire of the wheel group.">
+ <value>0.7699</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>2</upper_boundary>
+ </tire_diameter>
+ <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+ <value>0.2248</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </tire_section_width>
+ </tire_description>
+ </assembly_components>
+ </landing_gear_assembly>
+ <landing_gear_assembly ID="1" description="Geometrical description of one entire landing gear leg.">
+ <name description="Name of the landing gear leg.">
+ <value>right_main_gear_outer_strut</value>
+ </name>
+ <position description="Position of one entire landing gear leg with regard to the landing gear global position.">
+ <x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)">
+ <value>21.4812</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the landing gear global position. (center line of the landing gear leg)">
+ <value>3.6161</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the landing gear global position. (center line of the landing gear leg)">
+ <value>-0.906</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</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>1082.2998</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 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 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 landing gear center of gravity position. (entire landing gear leg)">
+ <value>1.5224</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Center of gravity in x-direction with regard to the global landing gear enter of gravity position. (entire landing gear leg)">
+ <value>3.6161</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+ <value>0.2491</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <assembly_components description="Geometrical description of the assembly components of one landing gear strut.">
+ <strut_diameter description="Diameter of the landing gear strut">
+ <value>0.2322</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </strut_diameter>
+ <strut_length description="Length of the landing gear strut">
+ <value>1.9991</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </strut_length>
+ <tire_description ID="0" description="Description of one tire of the wheel group.">
+ <name description="Name of the tire type.">
+ <value>APS01347-A</value>
+ </name>
+ <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+ <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+ <value>0.0</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 landing gear strut position. (center line of the landing gear strut">
+ <value>-0.4635</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+ <value>-1.9991</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </position>
+ <tire_diameter description="Diameter of one tire of the wheel group.">
+ <value>1.1493</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>2</upper_boundary>
+ </tire_diameter>
+ <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+ <value>0.4064</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </tire_section_width>
+ </tire_description>
+ <tire_description ID="1" description="Description of one tire of the wheel group.">
+ <name description="Name of the tire type.">
+ <value>APS01347-A</value>
+ </name>
+ <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+ <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+ <value>0.0</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 landing gear strut position. (center line of the landing gear strut">
+ <value>0.4635</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+ <value>-1.9991</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </position>
+ <tire_diameter description="Diameter of one tire of the wheel group.">
+ <value>1.1493</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>2</upper_boundary>
+ </tire_diameter>
+ <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+ <value>0.4064</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </tire_section_width>
+ </tire_description>
+ </assembly_components>
+ </landing_gear_assembly>
+ <landing_gear_assembly ID="2" description="Geometrical description of one entire landing gear leg.">
+ <name description="Name of the landing gear leg.">
+ <value>left_main_gear_outer_strut</value>
+ </name>
+ <position description="Position of one entire landing gear leg with regard to the landing gear global position.">
+ <x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)">
+ <value>21.4812</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Distance in y direction with regard to the landing gear global position. (center line of the landing gear leg)">
+ <value>-3.6161</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the landing gear global position. (center line of the landing gear leg)">
+ <value>-0.906</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</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>1082.2998</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 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 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 landing gear center of gravity position. (entire landing gear leg)">
+ <value>1.5224</value>
+ <unit>m</unit>
+ <lower_boundary>-100</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </x>
+ <y description="Center of gravity in x-direction with regard to the global landing gear enter of gravity position. (entire landing gear leg)">
+ <value>3.6161</value>
+ <unit>m</unit>
+ <lower_boundary>-50</lower_boundary>
+ <upper_boundary>50</upper_boundary>
+ </y>
+ <z description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+ <value>0.2491</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <assembly_components description="Geometrical description of the assembly components of one landing gear strut.">
+ <strut_diameter description="Diameter of the landing gear strut">
+ <value>0.2322</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.0</upper_boundary>
+ </strut_diameter>
+ <strut_length description="Length of the landing gear strut">
+ <value>1.9991</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </strut_length>
+ <tire_description ID="0" description="Description of one tire of the wheel group.">
+ <name description="Name of the tire type.">
+ <value>APS01347-A</value>
+ </name>
+ <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+ <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+ <value>0.0</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 landing gear strut position. (center line of the landing gear strut">
+ <value>-0.4635</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+ <value>-1.9991</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </position>
+ <tire_diameter description="Diameter of one tire of the wheel group.">
+ <value>1.1493</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>2</upper_boundary>
+ </tire_diameter>
+ <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+ <value>0.4064</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </tire_section_width>
+ </tire_description>
+ <tire_description ID="1" description="Description of one tire of the wheel group.">
+ <name description="Name of the tire type.">
+ <value>APS01347-A</value>
+ </name>
+ <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+ <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+ <value>0.0</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 landing gear strut position. (center line of the landing gear strut">
+ <value>0.4635</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </y>
+ <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+ <value>-1.9991</value>
+ <unit>m</unit>
+ <lower_boundary>-10</lower_boundary>
+ <upper_boundary>10</upper_boundary>
+ </z>
+ </position>
+ <tire_diameter description="Diameter of one tire of the wheel group.">
+ <value>1.1493</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>2</upper_boundary>
+ </tire_diameter>
+ <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+ <value>0.4064</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </tire_section_width>
+ </tire_description>
+ </assembly_components>
+ </landing_gear_assembly>
+ </geometry>
+ </specific>
+ </landing_gear>
+ <systems>
+ <mass_properties description="mass_properties of component systems">
+ <mass description="component mass">
+ <value>4825.986695</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </mass>
+ <inertia description="component inertia referred to local center of gravity">
+ <j_xx description="systems inertia in x">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xx>
+ <j_yy description="systems inertia in y">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yy>
+ <j_zz description="systems inertia in z">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zz>
+ <j_xy description="systems inertia in xy">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xy>
+ <j_xz description="systems inertia in xz">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xz>
+ <j_yx description="systems inertia in yx">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yx>
+ <j_yz description="systems inertia in yz">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yz>
+ <j_zx description="systems inertia in zx">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zx>
+ <j_zy description="systems inertia in zy">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="component center of gravity with respect to global coordinate system">
+ <x description="x position of center of gravity">
+ <value>7.051442313</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </x>
+ <y description="y position of center of gravity">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </y>
+ <z description="z position of center of gravity">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ <operator_items>
+ <operator_item ID="0">
+ <name description="name of the operator item">
+ <value>water_and_toilet_chemicals</value>
+ </name>
+ <mass_properties description="mass_properties of component water and toilet chemicals">
+ <mass description="component mass">
+ <value>220.32</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </mass>
+ <inertia description="component inertia referred to local center of gravity">
+ <j_xx description="water and toilet chemicals inertia in x">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xx>
+ <j_yy description="water and toilet chemicals inertia in y">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yy>
+ <j_zz description="water and toilet chemicals inertia in z">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zz>
+ <j_xy description="water and toilet chemicals inertia in xy">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xy>
+ <j_xz description="water and toilet chemicals inertia in xz">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xz>
+ <j_yx description="water and toilet chemicals inertia in yx">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yx>
+ <j_yz description="water and toilet chemicals inertia in yz">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yz>
+ <j_zx description="water and toilet chemicals inertia in zx">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zx>
+ <j_zy description="water and toilet chemicals inertia in zy">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="component center of gravity with respect to global coordinate system">
+ <x description="x position of center of gravity">
+ <value>2.811299577</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </x>
+ <y description="y position of center of gravity">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </y>
+ <z description="z position of center of gravity">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </operator_item>
+ <operator_item ID="1">
+ <name description="name of the operator item">
+ <value>residual_oil_and_fuel</value>
+ </name>
+ <mass_properties description="mass_properties of component water and toilet chemicals">
+ <mass description="component mass">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </mass>
+ <inertia description="component inertia referred to local center of gravity">
+ <j_xx description="water and toilet chemicals inertia in x">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xx>
+ <j_yy description="water and toilet chemicals inertia in y">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yy>
+ <j_zz description="water and toilet chemicals inertia in z">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zz>
+ <j_xy description="water and toilet chemicals inertia in xy">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xy>
+ <j_xz description="water and toilet chemicals inertia in xz">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_xz>
+ <j_yx description="water and toilet chemicals inertia in yx">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yx>
+ <j_yz description="water and toilet chemicals inertia in yz">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_yz>
+ <j_zx description="water and toilet chemicals inertia in zx">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zx>
+ <j_zy description="water and toilet chemicals inertia in zy">
+ <value>0</value>
+ <unit>kgm^2</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </j_zy>
+ </inertia>
+ <center_of_gravity description="component center of gravity with respect to global coordinate system">
+ <x description="x position of center of gravity">
+ <value>16.97777054</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </x>
+ <y description="y position of center of gravity">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </y>
+ <z description="z position of center of gravity">
+ <value>0</value>
+ <unit>m</unit>
+ <lower_boundary>-1.797693135e+308</lower_boundary>
+ <upper_boundary>1.797693135e+308</upper_boundary>
+ </z>
+ </center_of_gravity>
+ </mass_properties>
+ </operator_item>
+ </operator_items>
+ <specific>
+ <geometry>
+ <mass_properties>
+ <fuel_system description="mass of ATA-28">
+ <value>0</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </fuel_system>
+ <de_icing description="mass of ATA-30">
+ <value>31.34460331</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </de_icing>
+ <lighting description="mass of ATA-33">
+ <value>198.0485566</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </lighting>
+ <fire_protection description="mass of ATA-26">
+ <value>68.59844962</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </fire_protection>
+ <oxygen_system description="mass of ATA-35">
+ <value>91.34304</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </oxygen_system>
+ <flight_controls description="mass of ATA-27">
+ <value>1132.081306</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </flight_controls>
+ <instruments description="mass of ATA31">
+ <value>67.91403844</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </instruments>
+ <automatic_flight_system description="mass of ATA22">
+ <value>110.3603125</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </automatic_flight_system>
+ <navigation description="mass of ATA34">
+ <value>449.9305047</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </navigation>
+ <communication description="mass of ATA23">
+ <value>220.7206249</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </communication>
+ <bleed_air_system description="mass of ATA-36">
+ <value>170.9024353</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </bleed_air_system>
+ <hydraulic_generation description="mass of ATA-29">
+ <value>133.6948041</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </hydraulic_generation>
+ <hydraulic_distribution description="mass of ATA-29">
+ <value>506.8091903</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </hydraulic_distribution>
+ <electrical_generation description="mass of ATA-24">
+ <value>517.834438</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </electrical_generation>
+ <electrical_distribution description="mass of ATA-24">
+ <value>437.5675573</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </electrical_distribution>
+ <auxiliary_power_unit description="mass of ATA-49">
+ <value>164.6397078</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </auxiliary_power_unit>
+ <air_conditioning description="mass of ATA-21">
+ <value>303.8771255</value>
+ <unit>kg</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </air_conditioning>
+ </mass_properties>
+ </geometry>
+ <maximium_power_demand description="maximum power (hydraulic + electric) demand">
+ <value>249540.7594</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>1.971020666</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>55719.8203</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">
+ <value>0.9372327978</value>
+ <unit>W</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>100</upper_boundary>
+ </average_bleed_air_demand>
+ </specific>
+ </systems>
+ </component_design>
+ <sizing_point>
+ <thrust_to_weight description="Total thrust (kN) divided by maximum aircraft weight (kN)">
+ <value>0.341170989</value>
+ <unit>1</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>1</upper_boundary>
+ </thrust_to_weight>
+ <wing_loading description="Maximum takeoff mass (MTOM) divided by wing area (Sref)">
+ <value>619.8444758</value>
+ <unit>kg/m^2</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>inf</upper_boundary>
+ </wing_loading>
+ </sizing_point>
+ <assessment description="Assessment data">
+ <performance description="Assessment of performance values">
+ <takeoff>
+ <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>1714.684647</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5000</upper_boundary>
+ </takeoff_distance_normal_safety>
+ </takeoff>
+ <landing>
+ <needed_runway_length description="Needed runway length with all engines operating and maximum landing mass">
+ <value>1293.066314</value>
+ <unit>m</unit>
+ <lower_boundary>0</lower_boundary>
+ <upper_boundary>5000</upper_boundary>
+ </needed_runway_length>
+ </landing>
+ </performance>
+ </assessment>
+</aircraft_exchange_file>
\ No newline at end of file
diff --git a/UnicadoGUI/Frontend/package-lock.json b/UnicadoGUI/Frontend/package-lock.json
index b61a62dfb623a39504399af85db6b03a59e72e21..a576d6f81054845b41e24a8a59bf3022e9a83253 100644
--- a/UnicadoGUI/Frontend/package-lock.json
+++ b/UnicadoGUI/Frontend/package-lock.json
@@ -10,6 +10,7 @@
"dependencies": {
"@rollup/plugin-dsv": "^3.0.2",
"@sveltestrap/sveltestrap": "^6.2.4",
+ "jszip": "^3.10.1",
"layercake": "^8.0.2",
"svelte-chartjs": "^3.1.5",
"svelte-drag-and-drop-actions": "^1.0.2",
@@ -999,6 +1000,12 @@
"node": ">= 0.6"
}
},
+ "node_modules/core-util-is": {
+ "version": "1.0.3",
+ "resolved": "https://registry.npmjs.org/core-util-is/-/core-util-is-1.0.3.tgz",
+ "integrity": "sha512-ZQBvi1DcpJ4GDqanjucZ2Hj3wEO5pZDS89BWbkcrvdxksJorwUDDZamX9ldFkp9aw2lmBDLgkObEA4DWNJ9FYQ==",
+ "license": "MIT"
+ },
"node_modules/css-tree": {
"version": "2.3.1",
"resolved": "https://registry.npmjs.org/css-tree/-/css-tree-2.3.1.tgz",
@@ -1356,6 +1363,12 @@
"node": ">=0.10.0"
}
},
+ "node_modules/immediate": {
+ "version": "3.0.6",
+ "resolved": "https://registry.npmjs.org/immediate/-/immediate-3.0.6.tgz",
+ "integrity": "sha512-XXOFtyqDjNDAQxVfYxuF7g9Il/IbWmmlQg2MYKOH8ExIT1qg6xc4zyS3HaEEATgs1btfzxq15ciUiY7gjSXRGQ==",
+ "license": "MIT"
+ },
"node_modules/import-fresh": {
"version": "3.3.0",
"resolved": "https://registry.npmjs.org/import-fresh/-/import-fresh-3.3.0.tgz",
@@ -1395,8 +1408,7 @@
"node_modules/inherits": {
"version": "2.0.4",
"resolved": "https://registry.npmjs.org/inherits/-/inherits-2.0.4.tgz",
- "integrity": "sha512-k/vGaX4/Yla3WzyMCvTQOXYeIHvqOKtnqBduzTHpzpQZzAskKMhZ2K+EnBiSM9zGSoIFeMpXKxa4dYeZIQqewQ==",
- "dev": true
+ "integrity": "sha512-k/vGaX4/Yla3WzyMCvTQOXYeIHvqOKtnqBduzTHpzpQZzAskKMhZ2K+EnBiSM9zGSoIFeMpXKxa4dYeZIQqewQ=="
},
"node_modules/internmap": {
"version": "2.0.3",
@@ -1456,11 +1468,29 @@
"@types/estree": "*"
}
},
+ "node_modules/isarray": {
+ "version": "1.0.0",
+ "resolved": "https://registry.npmjs.org/isarray/-/isarray-1.0.0.tgz",
+ "integrity": "sha512-VLghIWNM6ELQzo7zwmcg0NmTVyWKYjvIeM83yjp0wRDTmUnrM678fQbcKBo6n2CJEF0szoG//ytg+TKla89ALQ==",
+ "license": "MIT"
+ },
"node_modules/javascript-interface-library": {
"version": "0.1.14",
"resolved": "https://registry.npmjs.org/javascript-interface-library/-/javascript-interface-library-0.1.14.tgz",
"integrity": "sha512-TSdQbLKqq6PcFk9M9Qk+l45rjqWfTMhSkvZVcByy1tKsDYDH+kblKu/FcVk4lWkeYXvcczX8NtPGdeyrZYEBrw=="
},
+ "node_modules/jszip": {
+ "version": "3.10.1",
+ "resolved": "https://registry.npmjs.org/jszip/-/jszip-3.10.1.tgz",
+ "integrity": "sha512-xXDvecyTpGLrqFrvkrUSoxxfJI5AH7U8zxxtVclpsUtMCq4JQ290LY8AW5c7Ggnr/Y/oK+bQMbqK2qmtk3pN4g==",
+ "license": "(MIT OR GPL-3.0-or-later)",
+ "dependencies": {
+ "lie": "~3.3.0",
+ "pako": "~1.0.2",
+ "readable-stream": "~2.3.6",
+ "setimmediate": "^1.0.5"
+ }
+ },
"node_modules/kleur": {
"version": "4.1.5",
"resolved": "https://registry.npmjs.org/kleur/-/kleur-4.1.5.tgz",
@@ -1485,6 +1515,15 @@
"typescript": "^5.0.2"
}
},
+ "node_modules/lie": {
+ "version": "3.3.0",
+ "resolved": "https://registry.npmjs.org/lie/-/lie-3.3.0.tgz",
+ "integrity": "sha512-UaiMJzeWRlEujzAuw5LokY1L5ecNQYZKfmyZ9L7wDHb/p5etKaxXhohBcrw0EYby+G/NA52vRSN4N39dxHAIwQ==",
+ "license": "MIT",
+ "dependencies": {
+ "immediate": "~3.0.5"
+ }
+ },
"node_modules/locally-unique-id-generator": {
"version": "0.1.5",
"resolved": "https://registry.npmjs.org/locally-unique-id-generator/-/locally-unique-id-generator-0.1.5.tgz",
@@ -1635,6 +1674,12 @@
"wrappy": "1"
}
},
+ "node_modules/pako": {
+ "version": "1.0.11",
+ "resolved": "https://registry.npmjs.org/pako/-/pako-1.0.11.tgz",
+ "integrity": "sha512-4hLB8Py4zZce5s4yd9XzopqwVv/yGNhV1Bl8NTmCq1763HeK2+EwVTv+leGeL13Dnh2wfbqowVPXCIO0z4taYw==",
+ "license": "(MIT AND Zlib)"
+ },
"node_modules/parent-module": {
"version": "1.0.1",
"resolved": "https://registry.npmjs.org/parent-module/-/parent-module-1.0.1.tgz",
@@ -1711,6 +1756,12 @@
"node": "^10 || ^12 || >=14"
}
},
+ "node_modules/process-nextick-args": {
+ "version": "2.0.1",
+ "resolved": "https://registry.npmjs.org/process-nextick-args/-/process-nextick-args-2.0.1.tgz",
+ "integrity": "sha512-3ouUOpQhtgrbOa17J7+uxOTpITYWaGP7/AhoR3+A+/1e9skrzelGi/dXzEYyvbxubEF6Wn2ypscTKiKJFFn1ag==",
+ "license": "MIT"
+ },
"node_modules/queue-microtask": {
"version": "1.2.3",
"resolved": "https://registry.npmjs.org/queue-microtask/-/queue-microtask-1.2.3.tgz",
@@ -1731,6 +1782,21 @@
}
]
},
+ "node_modules/readable-stream": {
+ "version": "2.3.8",
+ "resolved": "https://registry.npmjs.org/readable-stream/-/readable-stream-2.3.8.tgz",
+ "integrity": "sha512-8p0AUk4XODgIewSi0l8Epjs+EVnWiK7NoDIEGU0HhE7+ZyY8D1IMY7odu5lRrFXGg71L15KG8QrPmum45RTtdA==",
+ "license": "MIT",
+ "dependencies": {
+ "core-util-is": "~1.0.0",
+ "inherits": "~2.0.3",
+ "isarray": "~1.0.0",
+ "process-nextick-args": "~2.0.0",
+ "safe-buffer": "~5.1.1",
+ "string_decoder": "~1.1.1",
+ "util-deprecate": "~1.0.1"
+ }
+ },
"node_modules/readdirp": {
"version": "3.6.0",
"resolved": "https://registry.npmjs.org/readdirp/-/readdirp-3.6.0.tgz",
@@ -1846,6 +1912,12 @@
"node": ">=6"
}
},
+ "node_modules/safe-buffer": {
+ "version": "5.1.2",
+ "resolved": "https://registry.npmjs.org/safe-buffer/-/safe-buffer-5.1.2.tgz",
+ "integrity": "sha512-Gd2UZBJDkXlY7GbJxfsE8/nvKkUEU1G38c1siN6QP6a9PT9MmHB8GnpscSmMJSoF8LOIrt8ud/wPtojys4G6+g==",
+ "license": "MIT"
+ },
"node_modules/safer-buffer": {
"version": "2.1.2",
"resolved": "https://registry.npmjs.org/safer-buffer/-/safer-buffer-2.1.2.tgz",
@@ -1869,6 +1941,12 @@
"integrity": "sha512-RVnVQxTXuerk653XfuliOxBP81Sf0+qfQE73LIYKcyMYHG94AuH0kgrQpRDuTZnSmjpysHmzxJXKNfa6PjFhyQ==",
"dev": true
},
+ "node_modules/setimmediate": {
+ "version": "1.0.5",
+ "resolved": "https://registry.npmjs.org/setimmediate/-/setimmediate-1.0.5.tgz",
+ "integrity": "sha512-MATJdZp8sLqDl/68LfQmbP8zKPLQNV6BIZoIgrscFDQ+RsvK/BxeDQOgyxKKoh0y/8h3BqVFnCqQ/gd+reiIXA==",
+ "license": "MIT"
+ },
"node_modules/sirv": {
"version": "2.0.4",
"resolved": "https://registry.npmjs.org/sirv/-/sirv-2.0.4.tgz",
@@ -1906,6 +1984,15 @@
"node": ">=0.10.0"
}
},
+ "node_modules/string_decoder": {
+ "version": "1.1.1",
+ "resolved": "https://registry.npmjs.org/string_decoder/-/string_decoder-1.1.1.tgz",
+ "integrity": "sha512-n/ShnvDi6FHbbVfviro+WojiFzv+s8MPMHBczVePfUpDJLwoLT0ht1l4YwBCbi8pJAveEEdnkHyPyTP/mzRfwg==",
+ "license": "MIT",
+ "dependencies": {
+ "safe-buffer": "~5.1.0"
+ }
+ },
"node_modules/strip-indent": {
"version": "3.0.0",
"resolved": "https://registry.npmjs.org/strip-indent/-/strip-indent-3.0.0.tgz",
@@ -2165,6 +2252,12 @@
"node": ">=14.17"
}
},
+ "node_modules/util-deprecate": {
+ "version": "1.0.2",
+ "resolved": "https://registry.npmjs.org/util-deprecate/-/util-deprecate-1.0.2.tgz",
+ "integrity": "sha512-EPD5q1uXyFxJpCrLnCc1nHnq3gOa6DZBocAIiI2TaSCA7VCJ1UJDMagCzIkXNsUYfD1daK//LTEQ8xiIbrHtcw==",
+ "license": "MIT"
+ },
"node_modules/vite": {
"version": "5.1.1",
"resolved": "https://registry.npmjs.org/vite/-/vite-5.1.1.tgz",
diff --git a/UnicadoGUI/Frontend/package.json b/UnicadoGUI/Frontend/package.json
index af5e6bb049aa64430eff081859c084e7b8dc7d89..68b770077f79eaf0c22c107feafd2e5a2ec26d76 100644
--- a/UnicadoGUI/Frontend/package.json
+++ b/UnicadoGUI/Frontend/package.json
@@ -23,6 +23,7 @@
"dependencies": {
"@rollup/plugin-dsv": "^3.0.2",
"@sveltestrap/sveltestrap": "^6.2.4",
+ "jszip": "^3.10.1",
"layercake": "^8.0.2",
"svelte-chartjs": "^3.1.5",
"svelte-drag-and-drop-actions": "^1.0.2",
diff --git a/UnicadoGUI/Frontend/src/lib/components/Buttons/BaseButton.svelte b/UnicadoGUI/Frontend/src/lib/components/Buttons/BaseButton.svelte
new file mode 100644
index 0000000000000000000000000000000000000000..ba58bbe99edcd0d1066fd9ecd47ef864739a73ed
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/lib/components/Buttons/BaseButton.svelte
@@ -0,0 +1,17 @@
+<script>
+ import { Button, Icon } from "@sveltestrap/sveltestrap";
+
+ export let color = "primary";
+ export let outline = false;
+ export let iconName = "";
+ export let text = "";
+ export let onClick = () => {};
+
+</script>
+
+<Button {color} {outline} on:click={onClick}>
+ {#if iconName}
+ <Icon name={iconName} />{' '}
+ {/if}
+ {text}
+</Button>
diff --git a/UnicadoGUI/Frontend/src/lib/components/Buttons/DeleteProjectByIdButton.svelte b/UnicadoGUI/Frontend/src/lib/components/Buttons/DeleteProjectByIdButton.svelte
new file mode 100644
index 0000000000000000000000000000000000000000..7ff8e9d75a8c2f622af69e4481f971a28fcd9083
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/lib/components/Buttons/DeleteProjectByIdButton.svelte
@@ -0,0 +1,41 @@
+<script lang="ts">
+ import { Modal, ModalHeader, ModalBody, ModalFooter, Button, Icon } from "@sveltestrap/sveltestrap";
+ import { removeProjectById, getProjectNameById } from '../../../stores/projects';
+ import { createEventDispatcher } from 'svelte';
+
+ export let projectId : number;
+ const dispatch = createEventDispatcher();
+ let isModalOpen = false;
+
+ function openModal() {
+ isModalOpen = true;
+ dispatch('openModal');
+ }
+
+ function closeModal() {
+ isModalOpen = false;
+ dispatch('closeModal');
+ }
+
+ function handleDeleteProject() {
+ if (projectId) {
+ removeProjectById(projectId);
+ closeModal();
+ }
+ }
+</script>
+
+<Button color="danger" outline on:click={openModal} style="fit-content">
+ <Icon name="trash" />
+</Button>
+
+<Modal isOpen={isModalOpen} toggle={closeModal}>
+ <ModalHeader toggle={closeModal}>Remove Project</ModalHeader>
+ <ModalBody>
+ <p>Are you sure you want to remove the project with the name: <strong>{getProjectNameById(projectId)}</strong>?</p>
+ </ModalBody>
+ <ModalFooter>
+ <Button color="danger" on:click={handleDeleteProject}>Remove Project</Button>
+ <Button color="secondary" on:click={closeModal}>Cancel</Button>
+ </ModalFooter>
+</Modal>
\ No newline at end of file
diff --git a/UnicadoGUI/Frontend/src/lib/components/Buttons/DeleteProjectByNameButton.svelte b/UnicadoGUI/Frontend/src/lib/components/Buttons/DeleteProjectByNameButton.svelte
new file mode 100644
index 0000000000000000000000000000000000000000..77a0e943098ec7dbef489eef6749e57879ae12e9
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/lib/components/Buttons/DeleteProjectByNameButton.svelte
@@ -0,0 +1,73 @@
+<script lang="ts">
+ import {
+ Modal,
+ ModalHeader,
+ ModalBody,
+ ModalFooter,
+ Button,
+ Icon,
+ } from "@sveltestrap/sveltestrap";
+ import { userProjects, removeProject } from "../../../stores/projects";
+ import { onDestroy, createEventDispatcher } from "svelte";
+ let projects: any = [];
+ export let projectToRemove = "";
+
+ const unsubscribe = userProjects.subscribe((value) => {
+ projects = value;
+ });
+
+ const dispatch = createEventDispatcher();
+ let isModalOpen = false;
+
+ function openModal() {
+ isModalOpen = true;
+ dispatch("openModal");
+ }
+
+ function closeModal() {
+ isModalOpen = false;
+ dispatch("closeModal");
+ }
+
+ function handleDeleteProject() {
+ if (projectToRemove.trim() !== "") {
+ if (
+ confirm(
+ `Are you sure you want to delete the project "${projectToRemove}"?`,
+ )
+ ) {
+ removeProject(projectToRemove);
+ projectToRemove = "";
+ closeModal();
+ }
+ }
+ }
+
+ onDestroy(() => {
+ unsubscribe();
+ });
+</script>
+
+<!-- Button zum Öffnen des Modals -->
+<Button color="danger" outline on:click={openModal}>
+ <Icon name="trash" /> Remove Project
+</Button>
+
+<!-- Modal zum Löschen eines Projekts -->
+<Modal isOpen={isModalOpen} toggle={closeModal}>
+ <ModalHeader toggle={closeModal}>Remove Project</ModalHeader>
+ <ModalBody>
+ <select bind:value={projectToRemove} class="form-control">
+ <option value="" disabled>Select a project to remove...</option>
+ {#each projects as project}
+ <option value={project.name}>{project.name}</option>
+ {/each}
+ </select>
+ </ModalBody>
+ <ModalFooter>
+ <Button color="danger" on:click={handleDeleteProject}
+ >Remove Project</Button
+ >
+ <Button color="secondary" on:click={closeModal}>Cancel</Button>
+ </ModalFooter>
+</Modal>
diff --git a/UnicadoGUI/Frontend/src/lib/components/Buttons/LoadProjectsFromServerButton.svelte b/UnicadoGUI/Frontend/src/lib/components/Buttons/LoadProjectsFromServerButton.svelte
new file mode 100644
index 0000000000000000000000000000000000000000..6c894919b757525582e7f16d57a0af6a8d5af1f0
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/lib/components/Buttons/LoadProjectsFromServerButton.svelte
@@ -0,0 +1,24 @@
+<script>
+ import { Button, Icon } from "@sveltestrap/sveltestrap";
+ import { loadProjectsFromServer } from "../../../stores/projects.js";
+
+ const triggerFileDownload = async () => {
+ try {
+ if (
+ confirm(
+ `Are you sure you want to load the project list from the server?`,
+ )
+ ) {
+ await loadProjectsFromServer();
+ console.log("Project list Loaded successfully");
+ }
+ } catch (error) {
+ console.error("Error while trying to load the project list", error);
+ }
+ };
+</script>
+
+<Button on:click={triggerFileDownload}>
+ <Icon name="cloud-upload" />
+ Load project Liste from the server
+</Button>
diff --git a/UnicadoGUI/Frontend/src/lib/components/Buttons/LoadProjectsFromZipButton.svelte b/UnicadoGUI/Frontend/src/lib/components/Buttons/LoadProjectsFromZipButton.svelte
new file mode 100644
index 0000000000000000000000000000000000000000..ef71200874aab6ab06e93a46e427f06edf22e81f
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/lib/components/Buttons/LoadProjectsFromZipButton.svelte
@@ -0,0 +1,41 @@
+<script lang="ts">
+ import { Button, Icon } from "@sveltestrap/sveltestrap";
+ import { loadProjectsFromZip } from "../../../stores/projects";
+
+ function handleFileUpload(event: Event) {
+ const target = event.target as HTMLInputElement;
+ const selectedFile = target.files ? target.files[0] : null;
+
+ if (selectedFile) {
+ if (
+ confirm(
+ `Are you sure you want to load the project list from "${selectedFile?.name}"?`,
+ )
+ ) {
+ loadProjectsFromZip(selectedFile);
+ }
+ }
+ }
+
+ function triggerFileInput() {
+ const fileInput = document.getElementById("file-input");
+ if (fileInput) {
+ fileInput.click();
+ } else {
+ console.error("file-input not found");
+ }
+ }
+</script>
+
+<input
+ type="file"
+ accept=".zip"
+ id="file-input"
+ on:change={handleFileUpload}
+ style="display: none;"
+/>
+
+<Button on:click={triggerFileInput}>
+ <Icon name="cloud-upload" />
+ Load project Liste von zip-file
+</Button>
diff --git a/UnicadoGUI/Frontend/src/lib/components/Buttons/NewProjectButton.svelte b/UnicadoGUI/Frontend/src/lib/components/Buttons/NewProjectButton.svelte
new file mode 100644
index 0000000000000000000000000000000000000000..7bf9299777d6ab4b426ce354eb570f9ac0556626
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/lib/components/Buttons/NewProjectButton.svelte
@@ -0,0 +1,61 @@
+<script>
+ import {
+ Modal,
+ ModalHeader,
+ ModalBody,
+ ModalFooter,
+ Button,
+ Icon,
+ } from "@sveltestrap/sveltestrap";
+ import { addProject } from "../../../stores/projects.js";
+ import { createEventDispatcher } from "svelte";
+
+ export let projectName = "";
+ const dispatch = createEventDispatcher();
+ let isModalOpen = false;
+
+ function openModal() {
+ isModalOpen = true;
+ dispatch("openModal");
+ }
+
+ function closeModal() {
+ isModalOpen = false;
+ dispatch("closeModal");
+ }
+
+ function handleAddProject() {
+ if (projectName.trim() !== "") {
+ addProject(projectName);
+ projectName = "";
+ closeModal();
+ }
+ }
+
+ function handleKeyDown(/** @type KeyboardEvent **/ event) {
+ if (event.key === "Enter") {
+ handleAddProject();
+ }
+ }
+</script>
+
+<Button color="success" outline on:click={openModal}>
+ <Icon name="window-plus" /> New Project
+</Button>
+
+<Modal isOpen={isModalOpen} toggle={closeModal}>
+ <ModalHeader toggle={closeModal}>Add New Project</ModalHeader>
+ <ModalBody>
+ <input
+ type="text"
+ bind:value={projectName}
+ placeholder="Enter project name..."
+ class="form-control"
+ on:keydown={handleKeyDown}
+ />
+ </ModalBody>
+ <ModalFooter>
+ <Button color="primary" on:click={handleAddProject}>Add Project</Button>
+ <Button color="secondary" on:click={closeModal}>Cancel</Button>
+ </ModalFooter>
+</Modal>
diff --git a/UnicadoGUI/Frontend/src/lib/components/Buttons/NotSavedWarningButton.svelte b/UnicadoGUI/Frontend/src/lib/components/Buttons/NotSavedWarningButton.svelte
new file mode 100644
index 0000000000000000000000000000000000000000..9e8874e8924e3c34d3822659ab41ff001362b372
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/lib/components/Buttons/NotSavedWarningButton.svelte
@@ -0,0 +1,43 @@
+<script lang="ts">
+ import {
+ Modal,
+ ModalHeader,
+ ModalBody,
+ ModalFooter,
+ Button,
+ Icon,
+ } from "@sveltestrap/sveltestrap";
+ import SaveProjectsToZipButton from "$lib/components/Buttons/SaveProjectsToZipButton.svelte";
+ import SaveProjectsToServerButton from "$lib/components/Buttons/SaveProjectsToServerButton.svelte";
+ import { isSavePending } from "../../../stores/projects";
+ let isModalOpen = false;
+
+ $: buttonColor = $isSavePending ? "danger" : "secondary";
+ $: buttonText = $isSavePending
+ ? "Project List not saved"
+ : "Save Project List";
+
+ function openModal() {
+ isModalOpen = true;
+ }
+
+ function closeModal() {
+ isModalOpen = false;
+ }
+</script>
+
+<Button color={buttonColor} on:click={openModal}>
+ <Icon name="cloud-upload" />
+ {buttonText}
+</Button>
+
+<Modal isOpen={isModalOpen} toggle={closeModal}>
+ <ModalHeader toggle={closeModal}>Save Project List Project</ModalHeader>
+ <ModalBody>
+ <SaveProjectsToZipButton />
+ <SaveProjectsToServerButton />
+ </ModalBody>
+ <ModalFooter>
+ <Button color="secondary" on:click={closeModal}>Cancel</Button>
+ </ModalFooter>
+</Modal>
diff --git a/UnicadoGUI/Frontend/src/lib/components/Buttons/SaveProjectsToServerButton.svelte b/UnicadoGUI/Frontend/src/lib/components/Buttons/SaveProjectsToServerButton.svelte
new file mode 100644
index 0000000000000000000000000000000000000000..6f4fca94f3a4fbfdf38fcee1e3cb4613b6146f31
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/lib/components/Buttons/SaveProjectsToServerButton.svelte
@@ -0,0 +1,24 @@
+<script>
+ import { Button, Icon } from "@sveltestrap/sveltestrap";
+ import { saveProjectsOnServer } from "../../../stores/projects.js";
+
+ const triggerFileUpload = async () => {
+ try {
+ if (
+ confirm(
+ `Are you sure you want to save the project list on the server?`,
+ )
+ ) {
+ await saveProjectsOnServer();
+ console.log("Project list saved successfully");
+ }
+ } catch (error) {
+ console.error("Error while trying to save the project list", error);
+ }
+ };
+</script>
+
+<Button on:click={triggerFileUpload}>
+ <Icon name="cloud-upload" />
+ Save projects list on the server
+</Button>
diff --git a/UnicadoGUI/Frontend/src/lib/components/Buttons/SaveProjectsToZipButton.svelte b/UnicadoGUI/Frontend/src/lib/components/Buttons/SaveProjectsToZipButton.svelte
new file mode 100644
index 0000000000000000000000000000000000000000..982e32cc13d88840fc63b365cbf20120fc9e44e4
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/lib/components/Buttons/SaveProjectsToZipButton.svelte
@@ -0,0 +1,27 @@
+<script lang="ts">
+ import { Button, Icon } from "@sveltestrap/sveltestrap";
+ import { saveProjectsAsZip } from '../../../stores/projects';
+
+ const handleSave = async () => {
+ try {
+ if (
+ confirm(
+ `Are you sure you want to save the project list?`,
+ )
+ ) {
+ await saveProjectsAsZip();
+ console.log("Projects saved successfully");
+ }
+ } catch (error) {
+ console.error("Error while trying to save the project list", error);
+
+ }
+ }
+</script>
+
+
+
+<Button on:click={handleSave}>
+ <Icon name="cloud-download"/>
+ Save Project list to a zip-file
+</Button>
\ No newline at end of file
diff --git a/UnicadoGUI/Frontend/src/lib/components/ConfigView.svelte b/UnicadoGUI/Frontend/src/lib/components/ConfigView.svelte
new file mode 100644
index 0000000000000000000000000000000000000000..11d4ed7d3af5efe0f7c7dc2610bd52ed02ae84a4
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/lib/components/ConfigView.svelte
@@ -0,0 +1,114 @@
+<script lang="ts">
+ import { Input, Styles, Tooltip } from "@sveltestrap/sveltestrap";
+ import {
+ calcStepSize,
+ formatLabel,
+ } from "$lib/utilities/utilities";
+ import { createEventDispatcher } from 'svelte';
+
+ export let data:any;
+ const dispatch = createEventDispatcher();
+
+ function checkModalChanged() {
+ data.changed = true;
+ dispatch('update', {data})
+ }
+
+ function validateNumber(index: number) {
+ console.log("validateNumber");
+ if (data.html[index].bind.value < data.html[index].min) {
+ data.html[index].bind.value = data.html[index].min;
+ } else if (
+ data.html[index].bind.value > data.html[index].max
+ ) {
+ data.html[index].bind.value = data.html[index].max;
+ }
+ }
+</script>
+
+{#each data.html as element, index}
+ {#if element.type == "switch"}
+ <Input
+ id="uiElement{index}"
+ type="switch"
+ label={formatLabel(element.label)}
+ bind:checked={element.bind.value}
+ on:change={() => checkModalChanged()}
+ />
+ <Tooltip target="uiElement{index}" placement="left">
+ {element.description}
+ </Tooltip>
+ {:else if element.type == "label"}
+ <h3>{formatLabel(element.label)}</h3>
+ {:else if element.type == "selector"}
+ <h6>{formatLabel(element.label)}</h6>
+ <Input
+ id="uiElement{index}"
+ type="select"
+ bind:value={element.bind.value}
+ on:change={() => checkModalChanged()}
+ >
+ {#each element.options as option}
+ <option>{option}</option>
+ {/each}
+ </Input>
+ <Tooltip target="uiElement{index}" placement="left">
+ {element.description}
+ </Tooltip>
+ {:else if element.type == "textfield"}
+ <h7>{formatLabel(element.label)}</h7>
+ <Input
+ id="uiElement{index}"
+ type="text"
+ bind:value={element.bind.value}
+ on:change={() => checkModalChanged()}
+ />
+ <Tooltip target="uiElement{index}" placement="left">
+ {element.description}
+ </Tooltip>
+ {:else if element.type == "numberfield"}
+ {#if element.unit != "1" && element.unit != "-" && element.unit != "count"}
+ <h7>{formatLabel(element.label)} (in {element.unit})</h7>
+ {:else}
+ <h7>{formatLabel(element.label)}</h7>
+ {/if}
+ {#if element.max != Number.POSITIVE_INFINITY && element.min != Number.NEGATIVE_INFINITY}
+ <Input
+ type="range"
+ min={element.min}
+ max={element.max}
+ step="0.01"
+ bind:value={element.bind.value}
+ placeholder="range placeholder"
+ on:change={() => checkModalChanged()}
+ />
+ <Input
+ id="uiElement{index}"
+ type="number"
+ min={element.min}
+ max={element.max}
+ step="0.01"
+ bind:value={element.bind.value}
+ on:change={() => checkModalChanged()}
+ on:blur={() => validateNumber(index)}
+ />
+ {:else}
+ <Input
+ id="uiElement{index}"
+ type="number"
+ min={element.min}
+ max={element.max}
+ step={calcStepSize(element.bind.value)}
+ bind:value={element.bind.value}
+ on:change={() => checkModalChanged()}
+ on:blur={() => validateNumber(index)}
+ />
+ {/if}
+
+ <Tooltip target="uiElement{index}" placement="left">
+ {element.description}
+ </Tooltip>
+ {/if}
+{/each}
+
+<Styles />
diff --git a/UnicadoGUI/Frontend/src/lib/components/InPlaceEdit.svelte b/UnicadoGUI/Frontend/src/lib/components/InPlaceEdit.svelte
new file mode 100644
index 0000000000000000000000000000000000000000..95b0b20685b569cea99d487c01adf1d058eeb752
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/lib/components/InPlaceEdit.svelte
@@ -0,0 +1,58 @@
+<script>
+ import { createEventDispatcher, onMount } from 'svelte'
+
+ export let value, required = true
+
+ const dispatch = createEventDispatcher()
+ let editing = false, original
+
+ onMount(() => {
+ original = value
+ })
+
+ function edit() {
+ editing = true
+ }
+
+ function submit() {
+ if (value != original) {
+ dispatch('submit', value)
+ }
+
+ editing = false
+ }
+
+ function keydown(event) {
+ if (event.key == 'Escape') {
+ event.preventDefault()
+ value = original
+ editing = false
+ }
+ }
+
+ function focus(element) {
+ element.focus()
+ }
+</script>
+
+{#if editing}
+ <form on:submit|preventDefault={submit} on:keydown={keydown}>
+ <input bind:value on:blur={submit} {required} use:focus/>
+ </form>
+{:else}
+ <div on:click={edit}>
+ {value}
+ </div>
+{/if}
+
+<style>
+ input {
+ border: none;
+ background: none;
+ font-size: inherit;
+ color: inherit;
+ font-weight: inherit;
+ text-align: inherit;
+ box-shadow: none;
+ }
+</style>
\ No newline at end of file
diff --git a/UnicadoGUI/Frontend/src/lib/components/TabComponent.svelte b/UnicadoGUI/Frontend/src/lib/components/TabComponent.svelte
new file mode 100644
index 0000000000000000000000000000000000000000..e013c6327386ff1ce536eb0aa4582aaf948930b5
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/lib/components/TabComponent.svelte
@@ -0,0 +1,35 @@
+<script lang="ts">
+ import { Styles} from "@sveltestrap/sveltestrap";
+ import { onMount } from "svelte";
+ import {
+ generateHTML
+ } from "$lib/utilities/utilities";
+ import ConfigView from "$lib/components/ConfigView.svelte";
+
+ export let data;
+
+ type dictionary = {
+ [key: string]: any;
+ };
+
+ let modalModule: dictionary = {
+ name: "",
+ response: {},
+ html: [],
+ changed: false,
+ };
+
+ onMount(async () => {
+ console.log(data);
+ generateHTML(data,modalModule.html);
+ modalModule.html = [...modalModule.html];
+ });
+ function handleUpdate(event:any){
+ modalModule = event.detail.data;
+ modalModule = modalModule;
+ }
+</script>
+
+<ConfigView data={modalModule} on:update={handleUpdate}/>
+
+<Styles />
diff --git a/UnicadoGUI/Frontend/src/lib/index.ts b/UnicadoGUI/Frontend/src/lib/index.ts
index 856f2b6c38aec1085db88189bcf492dbb49a1c45..0d7c663c49ab824aef78132f6d082f072f6bec79 100644
--- a/UnicadoGUI/Frontend/src/lib/index.ts
+++ b/UnicadoGUI/Frontend/src/lib/index.ts
@@ -1 +1,2 @@
// place files you want to import through the `$lib` alias in this folder.
+
diff --git a/UnicadoGUI/Frontend/src/lib/settings/SettingsUi.ts b/UnicadoGUI/Frontend/src/lib/settings/SettingsUi.ts
new file mode 100644
index 0000000000000000000000000000000000000000..a75057970d440a395fb1ab949e3620216894bcf2
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/lib/settings/SettingsUi.ts
@@ -0,0 +1,100 @@
+//Interface for Ui-elements in module settings and it's implementations
+export interface SettingsUi {
+ type: string;
+ label: string;
+ description: string;
+ bind: string;
+}
+
+export class SettingsSwitch implements SettingsUi {
+ readonly type = "switch";
+ label: string;
+ description: string;
+ bind: string;
+
+ constructor(label: string, description: string, bind: string) {
+ this.bind = bind;
+ this.label = label;
+ this.description = description;
+ }
+}
+
+export class SettingsSelector implements SettingsUi {
+ readonly type = "selector";
+ label: string;
+ description: string;
+ bind: string;
+ options: string[];
+
+ constructor(
+ label: string,
+ description: string,
+ bind: string,
+ options: string[],
+ ) {
+ this.bind = bind;
+ this.label = label;
+ this.description = description;
+ this.options = options;
+ }
+}
+
+export class SettingsTextfield implements SettingsUi {
+ readonly type = "textfield";
+ label: string;
+ description: string;
+ bind: string;
+ input: string;
+
+ constructor(
+ label: string,
+ description: string,
+ bind: string,
+ input: string,
+ ) {
+ this.bind = bind;
+ this.label = label;
+ this.description = description;
+ this.input = input;
+ }
+}
+
+export class SettingsNumberfield implements SettingsUi {
+ readonly type = "numberfield";
+ label: string;
+ description: string;
+ bind: string;
+ unit: string = "-";
+ max: number = Number.POSITIVE_INFINITY;
+ min: number = Number.NEGATIVE_INFINITY;
+
+ constructor(label: string, description: string, bind: string) {
+ this.bind = bind;
+ this.label = label;
+ this.description = description;
+ }
+ setMax(max: number) {
+ this.max = max;
+ }
+ setMin(min: number) {
+ this.min = min;
+ }
+ setUnit(unit: string) {
+ this.unit = unit;
+ }
+}
+
+export class SettingsLabel implements SettingsUi{
+ readonly type = "label";
+ label: string;
+ bind: string;
+ description: string;
+
+ constructor(label: string,description: string, bind: string) {
+ this.label = label;
+ this.description = description;
+ this.bind = bind;
+ }
+
+
+}
diff --git a/UnicadoGUI/Frontend/src/lib/utilities/utilities.ts b/UnicadoGUI/Frontend/src/lib/utilities/utilities.ts
new file mode 100644
index 0000000000000000000000000000000000000000..6012b8dacd7811b805edb37d174a0da57e01ffc0
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/lib/utilities/utilities.ts
@@ -0,0 +1,77 @@
+import {
+ SettingsLabel,
+ SettingsNumberfield,
+ SettingsSelector,
+ SettingsSwitch,
+ SettingsTextfield, type SettingsUi
+} from "$lib/settings/SettingsUi";
+
+//template for datatype of dictionaries, only to avoid errors in Typescript
+export type dictionary = {
+ [key: string]: any
+}
+
+//Test if the string includes a number
+export function isNumber(n: string) {
+ return !isNaN(parseFloat(n)) && isFinite(parseFloat(n));
+}
+
+
+//Calculate Stepsize of number inputs from current value
+export function calcStepSize(value: number) {
+ const numberString = value.toString();
+ if (!numberString.includes(".")) {
+ return 1;
+ } else {
+ const decimalPart = numberString.split(".")[1];
+ return Math.pow(10, -decimalPart.length);
+ }
+}
+//Replacing underscores to space
+export function formatLabel(label: string) {
+ return label.replaceAll("_", " ");
+}
+
+/*Parse json response to matching SettingsUi-Elements
+ * to portray it later in the DOM
+ * recursive Function
+ * */
+export function generateHTML(json: dictionary, html : SettingsUi[]) {
+ Object.entries(json).forEach(([key, value]) => {
+ if (value == null) {
+ return
+ }
+ if (value.hasOwnProperty("value")) {
+ if (value["@description"] && value["@description"].toLowerCase().includes("switch")) {
+ value.value = (value.value === 'true' || value.value === "1") //transform string input to boolean for easier binding
+ html.push(new SettingsSwitch(key, value["@description"], value))
+ }else if(value["@description"] && (value["@description"].toLowerCase().includes("selector:")||value["@description"].toLowerCase().startsWith("selector"))){
+ let options = []
+ if(value["@description"].includes("mode_" )){
+ options = value["@description"].match(/mode_\d+/g)
+ }else{
+ let selectorString = value["@description"].split("Selector:")[1]
+ options=selectorString.split(" / ")
+ }
+ html.push(new SettingsSelector(key, value["@description"], value, options))
+ }else if(isNumber(value.value)){
+ value.value=parseFloat(value.value);
+ let numberField = new SettingsNumberfield(key, value["@description"], value)
+ if(value.hasOwnProperty('lower_boundary')&&isNumber(value['lower_boundary'])){numberField.setMin(value['lower_boundary'])}
+ if(value.hasOwnProperty('upper_boundary')&&isNumber(value['upper_boundary'])){numberField.setMax(value['upper_boundary'])}
+ if(value.hasOwnProperty("@unit")){numberField.setUnit(value["@unit"])}//spaeter entweder unit oder Unit in XML
+ if(value.hasOwnProperty("@Unit")){numberField.setUnit(value["@Unit"])}
+ if(value.hasOwnProperty("unit")){numberField.setUnit(value["unit"])}
+ if(value.hasOwnProperty("Unit")){numberField.setUnit(value["Unit"])}
+ html.push(numberField);
+ } else {
+ html.push(new SettingsTextfield(key, value["@description"], value, key))
+ }
+ } else if (typeof value === "object") {
+ html.push(new SettingsLabel(key,'',''))
+ generateHTML(json[key],html)
+ } else {
+ return;
+ }
+ })
+}
diff --git a/UnicadoGUI/Frontend/src/routes/+layout.svelte b/UnicadoGUI/Frontend/src/routes/+layout.svelte
index 924aa6c03f6dbdee82153f782784dd572b9cc350..e70addb2cc2e5357ada17480ba3132daeff4eb77 100644
--- a/UnicadoGUI/Frontend/src/routes/+layout.svelte
+++ b/UnicadoGUI/Frontend/src/routes/+layout.svelte
@@ -1,54 +1,165 @@
<script lang="ts">
- import {Container, Image, Row, Styles, Col, Nav, NavItem, NavLink, Icon} from '@sveltestrap/sveltestrap';
+ import {
+ Container,
+ Image,
+ Row,
+ Styles,
+ Col,
+ Nav,
+ NavItem,
+ NavLink,
+ Icon
+ } from "@sveltestrap/sveltestrap";
+ import { userProjects } from "../stores/projects";
+ import { onMount } from "svelte";
+ import DeleteProjectByIdButton from "$lib/components/Buttons/DeleteProjectByIdButton.svelte";
+ import NotSavedWarningButton from "$lib/components/Buttons/NotSavedWarningButton.svelte";
+ let projects: any[] = [];
+
+ onMount(() => {
+ const unsubscribe = userProjects.subscribe((value) => {
+ projects = value;
+ });
+ return () => unsubscribe();
+ });
+
+ let openProjectIndex: any = null;
+
+ function toggleSubItems(index: number) {
+ if (openProjectIndex === index) {
+ openProjectIndex = null;
+ } else {
+ openProjectIndex = index;
+ }
+ }
</script>
+
<Container fluid>
<Row class="flex-nowrap">
- <Col class="auto col-md-3 col-xl-2 px-sm-2 px-0 bg-dark" style="position: fixed">
- <div class="d-flex flex-column align-items-center align-items-sm-start px-3 pt-2 text-white min-vh-100">
- <a href="/" class="d-flex align-items-center pb-3 mb-md-0 me-md-auto text-white text-decoration-none">
- <Image fluid alt="" src="./favicon.png" style="max-width:20%;padding-right: 10px"/>
+ <Col
+ class="auto col-md-3 col-xl-2 px-sm-2 px-0 bg-dark"
+ style="position: fixed"
+ >
+ <div
+ class="d-flex flex-column align-items-center align-items-sm-start px-3 pt-2 text-white min-vh-100"
+ >
+ <a
+ href="/"
+ class="d-flex align-items-center pb-3 mb-md-0 me-md-auto text-white text-decoration-none"
+ >
+ <Image
+ fluid
+ alt=""
+ src="./favicon.png"
+ style="max-width:20%;padding-right: 10px"
+ />
<span class="fs-2 d-none d-sm-inline">Unicado</span>
</a>
- <Nav class="nav-pills flex-column mb-sm-auto mb-0 align-items-center align-items-sm-start " id="menu">
+ <Nav
+ class="nav-pills flex-column mb-sm-auto mb-0 align-items-center align-items-sm-start "
+ id="menu"
+ >
<NavItem>
<NavLink href="/" class="align-middle px-0 text-light">
<Icon name="house"></Icon>
<span class="ms-1 d-none d-sm-inline">Home</span>
</NavLink>
</NavItem>
- <NavItem>
- <NavLink href="/model" class="align-middle px-0 text-light">
- <Icon name="airplane"></Icon>
- <span class="ms-1 d-none d-sm-inline">Aircraft Projects</span>
- </NavLink>
- </NavItem>
- <NavItem>
- <NavLink href="/graphs" class="align-middle px-0 text-light">
- <Icon name="graph-down"></Icon>
- <span class="ms-1 d-none d-sm-inline">Graphs</span>
- </NavLink>
- </NavItem>
- <NavItem>
- <NavLink href="/reports" class="align-middle px-0 text-light">
- <Icon name="journal-richtext"></Icon>
- <span class="ms-1 d-none d-sm-inline">Reports</span>
- </NavLink>
- </NavItem>
- <NavItem>
- <NavLink href="/logs" class="align-middle px-0 text-light">
- <Icon name="card-text"></Icon>
- <span class="ms-1 d-none d-sm-inline">Logs</span>
- </NavLink>
- </NavItem>
- <NavItem>
- <NavLink href="/settings" class="align-middle px-0 text-light">
- <Icon name="gear"></Icon>
- <span class="ms-1 d-none d-sm-inline">Settings</span>
- </NavLink>
- </NavItem>
+
+ {#each projects as project, index}
+ <NavItem>
+ <NavLink
+ class="align-middle px-0 text-light"
+ on:click={() => toggleSubItems(index)}
+ >
+ <div class="d-flex justify-content-between align-items-center w-100">
+ <div class="d-flex align-items-center">
+ <Icon name="airplane"></Icon>
+ <span class="ms-1 d-none d-sm-inline"
+ >{project.name}</span
+ >
+ </div>
+ <DeleteProjectByIdButton projectId={project.id} />
+ </div>
+ </NavLink>
+
+ {#if openProjectIndex === index}
+ <ul class="sub-menu">
+ <NavItem>
+ <NavLink
+ href="/model"
+ class="align-middle px-0 text-light"
+ >
+ <Icon name="airplane"></Icon>
+ <span
+ class="ms-1 d-none d-sm-inline"
+ >Simulationsmodel</span
+ >
+ </NavLink>
+ </NavItem>
+ <NavItem>
+ <NavLink
+ href="/graphs/{project.id}"
+ class="align-middle px-0 text-light"
+ >
+ <Icon name="graph-down"></Icon>
+ <span
+ class="ms-1 d-none d-sm-inline"
+ >Graphs</span
+ >
+ </NavLink>
+ </NavItem>
+ <NavItem>
+ <NavLink
+ href="/reports/{project.id}"
+ class="align-middle px-0 text-light"
+ >
+ <Icon name="journal-richtext"
+ ></Icon>
+ <span
+ class="ms-1 d-none d-sm-inline"
+ >Reports</span
+ >
+ </NavLink>
+ </NavItem>
+ <NavItem>
+ <NavLink
+ href="/logs/{project.id}"
+ class="align-middle px-0 text-light"
+ >
+ <Icon name="card-text"></Icon>
+ <span
+ class="ms-1 d-none d-sm-inline"
+ >Logs</span
+ >
+ </NavLink>
+ </NavItem>
+ <NavItem>
+ <NavLink
+ href="/settings"
+ class="align-middle px-0 text-light"
+ >
+ <Icon name="gear"></Icon>
+ <span
+ class="ms-1 d-none d-sm-inline"
+ >Settings</span
+ >
+ </NavLink>
+ </NavItem>
+ </ul>
+ {/if}
+ </NavItem>
+ {/each}
+ <NavItem></NavItem>
</Nav>
- <hr>
- <Nav class="pb-4" style="width: 100%; display: flex; justify-content: space-between">
+ <hr />
+ <Nav
+ class="pb-4"
+ style="width: 100%; display: flex; justify-content: space-between"
+ >
+ <NavItem>
+ <NotSavedWarningButton />
+ </NavItem>
<NavItem>
<NavLink href="/" class="align-middle text-light">
<Icon name="box-arrow-in-right"></Icon>
@@ -70,4 +181,4 @@
</Row>
</Container>
-<Styles/>
+<Styles />
diff --git a/UnicadoGUI/Frontend/src/routes/+page.svelte b/UnicadoGUI/Frontend/src/routes/+page.svelte
index d10b46043e814d51bee0f12af497d2e126bde361..8b852b9c5d560d48b3a106ff40c35acd228384db 100644
--- a/UnicadoGUI/Frontend/src/routes/+page.svelte
+++ b/UnicadoGUI/Frontend/src/routes/+page.svelte
@@ -1,8 +1,25 @@
<script>
- import {Styles} from "@sveltestrap/sveltestrap";
+ import { Styles } from "@sveltestrap/sveltestrap";
+
+ let projectName = "";
+ let projectToRemove = "";
+
+ import NewProjectButton from "$lib/components/Buttons/NewProjectButton.svelte";
+ import DeleteProjectButton from "$lib/components/Buttons/DeleteProjectByNameButton.svelte";
+ import SaveProjectsToZipButton from "$lib/components/Buttons/SaveProjectsToZipButton.svelte";
+ import LoadProjectsFromZipButton from "$lib/components/Buttons/LoadProjectsFromZipButton.svelte";
+ import LoadProjectFromServerButton from "$lib/components/Buttons/LoadProjectsFromServerButton.svelte";
+ import SaveProjectsToServerButton from "$lib/components/Buttons/SaveProjectsToServerButton.svelte";
</script>
+
<h1>Welcome to the UNICADO WebApp</h1>
-<p>Create new Project....<br>Open existing Project...</p>
+<NewProjectButton bind:projectName />
+<DeleteProjectButton bind:projectToRemove />
+<SaveProjectsToZipButton />
+<LoadProjectsFromZipButton />
+
+<LoadProjectFromServerButton />
+<SaveProjectsToServerButton />
-<Styles/>
\ No newline at end of file
+<Styles />
diff --git a/UnicadoGUI/Frontend/src/routes/model/+page.svelte b/UnicadoGUI/Frontend/src/routes/model/+page.svelte
index 3cae5d93f62130ecab5f2d8e4a6aef4b372c5caf..93ec7737b3f9902a526c77ef6786f7c3d0686c2b 100644
--- a/UnicadoGUI/Frontend/src/routes/model/+page.svelte
+++ b/UnicadoGUI/Frontend/src/routes/model/+page.svelte
@@ -14,97 +14,13 @@
Styles, Tooltip
} from "@sveltestrap/sveltestrap";
import {onMount} from "svelte";
- import InPlaceEdit from './InPlaceEdit.svelte';
-
- //Interface for Ui-elements in module settings and it's implementations
- interface SettingsUi {
- type: string;
- label: string;
- description: string;
- bind: string;
- }
-
- class SettingsSwitch implements SettingsUi {
- readonly type = "switch";
- label: string;
- description: string;
- bind: string;
-
- constructor(label: string, description: string, bind: string) {
- this.bind = bind;
- this.label = label;
- this.description = description;
- }
- }
-
- class SettingsSelector implements SettingsUi {
- readonly type = "selector";
- label: string;
- description: string;
- bind: string;
- options: string[];
-
- constructor(label: string, description: string, bind: string, options: string[]) {
- this.bind = bind;
- this.label = label;
- this.description = description;
- this.options = options;
- }
- }
-
- class SettingsTextfield implements SettingsUi {
- readonly type = "textfield";
- label: string;
- description: string;
- bind: string;
- input: string;
-
- constructor(label: string, description: string, bind: string, input: string) {
- this.bind = bind;
- this.label = label;
- this.description = description;
- this.input = input;
- }
- }
-
- class SettingsNumberfield implements SettingsUi {
- readonly type = "numberfield";
- label: string;
- description: string;
- bind: string;
- unit: string = '-';
- max: number = Number.POSITIVE_INFINITY;
- min: number = Number.NEGATIVE_INFINITY;
-
- constructor(label: string, description: string, bind: string) {
- this.bind = bind;
- this.label = label;
- this.description = description;
- }
- setMax(max:number){
- this.max=max;
- }
- setMin(min:number){
- this.min=min;
- }
- setUnit(unit:string){
- this.unit=unit;
- }
- }
-
- class SettingsLabel {
- readonly type = "label";
- label: string;
-
- constructor(label: string) {
- this.label = label;
- }
- }
-
- //template for datatype of dictionaries, only to avoid errors in Typescript
- type dictionary = {
- [key: string]: any
- }
+ import InPlaceEdit from '$lib/components/InPlaceEdit.svelte';
+ import {
+ generateHTML,
+ formatLabel,
+ } from "$lib/utilities/utilities.js";
+ import type {dictionary} from "$lib/utilities/utilities.js";
+ import ConfigView from "$lib/components/ConfigView.svelte";
/* Dictionary with information of the module
* including the json response and the settings elements it needs to implement in the dom
@@ -112,7 +28,8 @@
let modalModule: dictionary = {
name: '',
response: {},
- html: []
+ html: [],
+ changed: false
}
//Class for a group of modules
@@ -137,9 +54,6 @@
//Flag for Alarm which is invoked by changes
let saveAlert = false;
- //Flag for changes in settings modal by the user
- let modalChanged: boolean = false;
-
//Array of all the groups of the model
let groups: group[] = [];
@@ -162,8 +76,6 @@
//Function for loading list of available modules from server
async function loadAvailableModules() {
- //transitionally reading from convergenceloop_conf.xml
- //TO-DO: replace with something more recent
const res = await fetch("http://127.0.0.1:8000/modules/selection");
const data = await res.json();
modules = data['availableModules'];
@@ -212,19 +124,19 @@
modalModule.response = JSON.parse(data);
modalModule.html = [];
modalModule = modalModule;
- generateHTML(modalModule.response);
- modalChanged = false;
- modalChanged = modalChanged;
+ generateHTML(modalModule.response,modalModule.html);
+ modalModule.changed = false;
+ modalModule.changed = modalModule.changed;
modalModule = modalModule;
+
} catch (error) {
console.error(error);
modalModule.name = "no";
modalModule.response = {};
- modalModule.html = [];
- modalModule.html.push(new SettingsLabel("No config found!"));
}
}
+
//Wrapper to give Click-Event handler a synchronous Output
function getModuleConfClickWrapper(item: string) {
getModuleConf(item).catch(console.error);
@@ -235,50 +147,6 @@
};
}
- /*Parse json response to matching SettingsUi-Elements
- * to portray it later in the DOM
- * recursive Function
- * */
- function generateHTML(json: dictionary) {
- Object.entries(json).forEach(([key, value]) => {
- if (value == null) {
- return
- }
- if (value.hasOwnProperty("value")) {
- if (value["@description"] && value["@description"].toLowerCase().includes("switch")) {
- value.value = (value.value === 'true' || value.value === "1") //transform string input to boolean for easier binding
- modalModule.html.push(new SettingsSwitch(key, value["@description"], value))
- }else if(value["@description"] && (value["@description"].toLowerCase().includes("selector:")||value["@description"].toLowerCase().startsWith("selector"))){
- let options = []
- if(value["@description"].includes("mode_" )){
- options = value["@description"].match(/mode_\d+/g)
- }else{
- let selectorString = value["@description"].split("Selector:")[1]
- options=selectorString.split(" / ")
- }
- modalModule.html.push(new SettingsSelector(key, value["@description"], value, options))
- }else if(isNumber(value.value)){
- value.value=parseFloat(value.value);
- let numberField = new SettingsNumberfield(key, value["@description"], value)
- if(value.hasOwnProperty('lower_boundary')&&isNumber(value['lower_boundary'])){numberField.setMin(value['lower_boundary'])}
- if(value.hasOwnProperty('upper_boundary')&&isNumber(value['upper_boundary'])){numberField.setMax(value['upper_boundary'])}
- if(value.hasOwnProperty("@unit")){numberField.setUnit(value["@unit"])}//spaeter entweder unit oder Unit in XML
- if(value.hasOwnProperty("@Unit")){numberField.setUnit(value["@Unit"])}
- if(value.hasOwnProperty("unit")){numberField.setUnit(value["unit"])}
- if(value.hasOwnProperty("Unit")){numberField.setUnit(value["Unit"])}
- modalModule.html.push(numberField);
- } else {
- modalModule.html.push(new SettingsTextfield(key, value["@description"], value, key))
- }
- } else if (typeof value === "object") {
- modalModule.html.push(new SettingsLabel(key))
- generateHTML(json[key])
- } else {
- return;
- }
- })
- }
-
//Save Settings of Module to Server
async function uploadModuleConf() {
const response = await fetch('http://127.0.0.1:8000/modules/config/update', {
@@ -289,19 +157,8 @@
}
})
.then(response => response.json())
- modalChanged = false;
- modalChanged = modalChanged;
- }
-
- //Replacing underscores to space
- function formatLabel(label: string) {
- return label.replaceAll("_", " ")
- }
-
- //check if the settings modal of a module changed
- function checkModalChanged() {
- modalChanged = true;
- modalChanged = modalChanged;
+ modalModule.changed = false;
+ modalModule.changed = modalModule.changed;
}
//reset settings of an module
@@ -346,6 +203,11 @@
changed = changed;
}
+ function handleUpdate(event:any){
+ modalModule = event.detail.data;
+ modalModule = modalModule;
+ }
+
//Makes new group and adding it to groups
function addGroup() {
groups.push(new group("group " + groups.length, 1))
@@ -391,33 +253,9 @@
updateAll()
}
- //Calculate Stepsize of number inputs from current value
- function calcStepSize(value:number){
- const numberString = value.toString()
- if (!numberString.includes('.')) {
- return 1;
- } else {
- const decimalPart = numberString.split('.')[1];
- return Math.pow(10, -decimalPart.length);
- }
- }
- //check if string is a number
- function isNumber(n:string){
- return!isNaN(parseFloat(n))&&isFinite(parseFloat(n))
- }
- //check if number is in boundry
- function validateNumber(index:number){
- console.log("validateNumber")
- if(modalModule.html[index].bind.value<modalModule.html[index].min){
- modalModule.html[index].bind.value=modalModule.html[index].min;
- }else if(modalModule.html[index].bind.value>modalModule.html[index].max){
- modalModule.html[index].bind.value=modalModule.html[index].max;
- }
- }
-
</script>
<Container>
- <h2>Simulationsmodel</h2>
+ <h2>Simulationsmodel12</h2>
<Alert color="primary" isOpen={saveAlert} toggle={() => (saveAlert = false)}>
Changes in Model please save or reload before starting!.
</Alert>
@@ -498,59 +336,12 @@
<Modal isOpen={open} toggle={toggle} scrollable>
<ModalHeader toggle={toggle}>{formatLabel(modalModule.name)} settings</ModalHeader>
<ModalBody>
- {#each modalModule.html as element, index}
- {#if element.type == "switch"}
- <Input id="uiElement{index}" type="switch" label="{formatLabel(element.label)}"
- bind:checked={element.bind.value} on:change={()=>checkModalChanged()}/>
- <Tooltip target="uiElement{index}" placement="left">
- {element.description}
- </Tooltip>
- {:else if element.type == "label"}
- <h3>{formatLabel(element.label)}</h3>
- {:else if element.type == "selector"}
- <h6>{formatLabel(element.label)}</h6>
- <Input id="uiElement{index}" type="select" bind:value={element.bind.value}
- on:change={()=>checkModalChanged()}>
- {#each element.options as option}
- <option>{option}</option>
- {/each}
- </Input>
- <Tooltip target="uiElement{index}" placement="left">
- {element.description}
- </Tooltip>
- {:else if element.type == "textfield"}
- <h7>{formatLabel(element.label)}</h7>
- <Input id="uiElement{index}" type="text" bind:value={element.bind.value}
- on:change={()=>checkModalChanged()}/>
- <Tooltip target="uiElement{index}" placement="left">
- {element.description}
- </Tooltip>
- {:else if element.type == "numberfield"}
- {#if element.unit != "1" && element.unit != "-" && element.unit != "count"}
- <h7>{formatLabel(element.label)} (in {element.unit})</h7>
- {:else}
- <h7>{formatLabel(element.label)}</h7>
- {/if}
- {#if element.max != Number.POSITIVE_INFINITY && element.min != Number.NEGATIVE_INFINITY}
- <Input type="range" min={element.min} max={element.max} step=0.01 bind:value={element.bind.value}
- placeholder="range placeholder" on:change={()=>checkModalChanged()}/>
- <Input id="uiElement{index}" type="number" min={element.min} max={element.max} step=0.01
- bind:value={element.bind.value} on:change={()=>checkModalChanged()} on:blur={()=>validateNumber(index)}/>
- {:else}
- <Input id="uiElement{index}" type="number" min={element.min} max={element.max} step={calcStepSize(element.bind.value)}
- bind:value={element.bind.value} on:change={()=>checkModalChanged()} on:blur={()=>validateNumber(index)}/>
- {/if}
-
- <Tooltip target="uiElement{index}" placement="left">
- {element.description}
- </Tooltip>
- {/if}
- {/each}
+ <ConfigView data={modalModule} on:update={handleUpdate}/>
</ModalBody>
- {#if modalModule.name != "no"}
+ {#if modalModule.name !== "no"}
<ModalFooter>
<ButtonGroup>
- {#if modalChanged}
+ {#if modalModule.changed}
<Button color="primary" on:click={uploadModuleConf}>
<Icon name="floppy"/>
Save
diff --git a/UnicadoGUI/Frontend/src/routes/settings/+page.svelte b/UnicadoGUI/Frontend/src/routes/settings/+page.svelte
index 85503ea5e5cb6c833eddd705d8d942fe5164943b..084adf5af1f5f9a2119d4c8be5b826255841263b 100644
--- a/UnicadoGUI/Frontend/src/routes/settings/+page.svelte
+++ b/UnicadoGUI/Frontend/src/routes/settings/+page.svelte
@@ -1,343 +1,44 @@
<script lang="ts">
- //Testpage to show possible look of a settingspage
-
- import {
- Button,
- ButtonGroup,
- Form,
- FormGroup,
- Icon,
- Input,
- Styles,
- TabContent,
- TabPane
- } from "@sveltestrap/sveltestrap";
- let changed = false;
-
- class EnergyCarrier{
- constructor(value : string, id :number) {
- this.value = value;
- this.id = id;
- }
- }
- class Propulsor{
- constructor(powertrain : string,type : string,position : string ,energycarrier: EnergyCarrier[],thrust_share: string) {
- this.powertrain = powertrain;
- this.type = type;
- this.position = position;
- this.energycarrier = energycarrier;
- this.thrust_share = thrust_share;
- }
+ import { Styles } from "@sveltestrap/sveltestrap";
+ import { onMount } from "svelte";
+ import { settingData, loadTabData } from "../../stores/settings";
+ import TabComponent from "$lib/components/TabComponent.svelte";
+
+ let selectedTab = Object.keys($settingData)[0];
+
+ onMount(async () => {
+ const res = await fetch(
+ `http://127.0.0.1:8000/projects/aircraft_exchange_file/`,
+ );
+ const data = await res.json();
+ await loadTabData(data);
+ selectedTab = Object.keys($settingData)[0];
+ console.log(Object.keys($settingData));
+ });
+
+ function selectTab(tab: string) {
+ selectedTab = tab;
}
- //Energy Carriers
- let kerosin = new EnergyCarrier("kerosin",1);
- let liquid_hydrogen = new EnergyCarrier("liquid_hydrogen",2);
- let battery = new EnergyCarrier("battery",3);
- let saf = new EnergyCarrier("saf",4);
-
-
- let propulsors : Propulsor[]= [];
- let energycarriers : EnergyCarrier[]=[];
-
- let max_load_factor= 2;
- let min_load_factor= -1;
- let maneuver_load_factor= 1.1;
- let passenger_nr= 150;
- let mass_per_passenger=80;
- let luggage_mass_per_passenger=17;
- let additional_cargo_mass= 500;
- let cargo_density =165;
- let thrust_share = 1;
- let thickness = 0.003;
- let maximum_structrual_payload_mass = 30000;
- let takeoff_distance = 2122;
- let landing_field_length = 2387;
- let requirements ={
- general:{
- type: String,
- model: String,
- },
- mission_files: {
- design_mission_file: String,
- study_mission_file: String,
- requirements_mission_file: String,
- },
- design_specification:{
- configuration: {
- configuration_type: String,
- fuselage_type: String,
- mounting: String,
- empennage_type: String,
- undercarriage_definition:{
- main_gear_mounting: String,
- undercarriage_retractability: String,
- },
-
-
-
- },
-
-
- }
- }
-
</script>
-<h1>Aircraftmodelsettings</h1>
-<ButtonGroup style="margin-bottom: 20px">
- <Button color="dark" outline ><Icon name="bootstrap-reboot"/> Reset </Button>
- {#if changed}
- <Button color="danger" outline active><Icon name="cloud-upload" /> Save </Button>
- {:else}
- <Button color="dark" outline ><Icon name="cloud-upload" /> Save </Button>
- {/if}
- <Button color="dark" outline ><Icon name="cloud-download" /> Load </Button>
-</ButtonGroup>
-
-<TabContent vertical pills>
- <TabPane tabId="general" tab="General" active>
- <Form>
- <h5>General aircraft information</h5>
- <FormGroup floating label="Aircraft type">
- <Input placeholder="Enter a value"/>
- </FormGroup>
- <FormGroup floating label="Model - Version">
- <Input placeholder="Enter a value"/>
- </FormGroup>
-
- <h5>Name of xml files which are located in the missionData directory and contain the flight phase data</h5>
- <FormGroup floating label="Name of the study mission xml">
- <Input placeholder="Enter a value"/>
- </FormGroup>
- <FormGroup floating label="Name of the requirements mission xml">
- <Input placeholder="Enter a value"/>
- </FormGroup>
- </Form>
- </TabPane>
- <TabPane tabId="design_specification" tab="Design Specification">
- <Form>
- <h5>Configuration information</h5>
- <FormGroup floating label="Aircraft configuration">
- <Input type="select" placeholder="Enter a value">
- <option value="tube_and_wing">tube and wing</option>
- <option value="blended_wing_body">blended wing body</option>
- </Input>
- </FormGroup>
- <FormGroup floating label="Design description of the fuselage">
- <Input type="select" placeholder="Enter a value">
- <option value="single_aisle">single aisle</option>
- <option value="weight_body">weight body</option>
- </Input>
- </FormGroup>
- <FormGroup floating label="Definitions for wing design">
- <Input type="select" placeholder="Enter a value">
- <option value="low">low</option>
- <option value="mid">mid</option>
- <option value="high">high</option>
- </Input>
- </FormGroup>
- <!-- <FormGroup floating label="Definitions for empennage design">-->
- <!-- <Input type="select" placeholder="Enter a value">-->
- <!-- <option value="low">low</option>-->
- <!-- <option value="mid">mid</option>-->
- <!-- </Input>-->
- <!-- </FormGroup>-->
-
- <h5>Design description of the undercarriage</h5>
- <FormGroup floating label="Mounting position of the main landing gear">
- <Input type="select" placeholder="Enter a value">
- <option value="wing_mounted">wing mounted</option>
- <option value="fuselage_mounted">fuselage mounted</option>
- </Input>
- </FormGroup>
- <FormGroup floating label="Retractability of landing gear">
- <Input type="select" placeholder="Enter a value">
- <option value="retractable">retractable</option>
- <option value="non_retractable">non retractable</option>
- </Input>
- </FormGroup>
-
- <h5> Design Load information</h5>
- <FormGroup floating label="maximum load factor">
- <Input type="number" min={0} max={4} step={0.1} bind:value={max_load_factor} placeholder="number placeholder"/>
- <Input type="range" min={0} max={4} step={0.1} bind:value={max_load_factor} placeholder="range placeholder"/>
- </FormGroup>
- <FormGroup floating label="minimum load factor">
- <Input type="number" min={-2} max={0} step={0.1} bind:value={min_load_factor} placeholder="number placeholder"/>
- <Input type="range" min={-2} max={0} step={0.1} bind:value={min_load_factor} placeholder="range placeholder"/>
- </FormGroup>
- <FormGroup floating label="standard maneuver load factor for e.g. flare">
- <Input type="number" min={0} max={2} step={0.1} bind:value={maneuver_load_factor} placeholder="number placeholder"/>
- <Input type="range" min={0} max={2} step={0.1} bind:value={maneuver_load_factor} placeholder="range placeholder"/>
- </FormGroup>
-
- <h5> Passenger definition</h5>
- <FormGroup floating label="Number of passengers">
- <Input type="number" min={0} step={1} bind:value={passenger_nr} placeholder="number placeholder"/>
- </FormGroup>
- <FormGroup floating label="Design mass of a single passenger WITHOUT luggage in kg">
- <Input type="number" min={50} max={200} step={1} bind:value={mass_per_passenger} placeholder="number placeholder"/>
- <Input type="range" min={50} max={200} step={1} bind:value={mass_per_passenger} placeholder="range placeholder"/>
- </FormGroup>
- <FormGroup floating label="Design mass of a the luggage for a single passenger in kg">
- <Input type="number" min={0} max={25} step={1} bind:value={luggage_mass_per_passenger} placeholder="number placeholder"/>
- <Input type="range" min={0} max={25} step={1} bind:value={luggage_mass_per_passenger} placeholder="range placeholder"/>
- </FormGroup>
- <h6>passenger class distro with bar and 5 classes</h6>
-
- <h5>Cargo definition</h5>
- <FormGroup floating label="Mass of cargo which does not belong to passengers in kg">
- <Input type="number" min={0} max={1000} step={1} bind:value={additional_cargo_mass} placeholder="number placeholder"/>
- <Input type="range" min={0} max={1000} step={1} bind:value={additional_cargo_mass} placeholder="range placeholder"/>
- </FormGroup>
- <FormGroup floating label="Density of cargo which does not belong to passengers in kg/m^3">
- <Input type="number" min={150} max={200} step={1} bind:value={cargo_density} placeholder="number placeholder"/>
- <Input type="range" min={150} max={200} step={1} bind:value={cargo_density} placeholder="range placeholder"/>
- </FormGroup>
- </Form>
- </TabPane>
- <TabPane tabId="requirements" tab="Requirements">
- <Form>
-
- </Form>
- </TabPane>
- <TabPane tabId="assessment_scenario" tab="Assessment Scenario">
- <Form>
-
- </Form>
- </TabPane>
-</TabContent>
-<Form>
- <h2>Requirements and Specifications</h2>
-
-
-
- <h5>Design specification</h5>
-
-
- <h5>Energy carriers information</h5>
- <FormGroup floating label="ID of Energy type: kerosene / liquid_hydrogen / battery / saf (for multifuel engine create new ID)">
- <Input type="number" placeholder="number placeholder"/>
- </FormGroup>
-
- <h5>Propulsion information?</h5>
- <FormGroup floating label="Way the power is generated from the source">
- <Input type="select" placeholder="Enter a value">
- <option value="turbo">turbo</option>
- <option value="electric">electric</option>
- <option value="fuel_cell">fuel_cell</option>
- </Input>
- </FormGroup>
- <FormGroup floating label="Type of main thrust generator">
- <Input type="select" placeholder="Enter a value">
- <option value="fan">fan</option>
- <option value="prop">prop</option>
- </Input>
- </FormGroup>
- <FormGroup floating label="position on component">
- <Input type="select" placeholder="Enter a value">
- <option value="wing">wing</option>
- <option value="fuselage">fuselage</option>
- <option value="empennage">empennage</option>
- </Input>
- </FormGroup>
- <FormGroup floating label="x-position (aircraft coordinate system)">
- <Input type="select" placeholder="Enter a value">
- <option value="front">front</option>
- <option value="back">back</option>
- </Input>
- </FormGroup>
- <FormGroup floating label="y-position (aircraft coordinate system)">
- <Input type="select" placeholder="Enter a value">
- <option value="left">left</option>
- <option value="right">right</option>
- </Input>
- </FormGroup>
- <FormGroup floating label="z-position (aircraft coordinate system)">
- <Input type="select" placeholder="Enter a value">
- <option value="over">over</option>
- <option value="mid">mid</option>
- <option value="under">under</option>
- <option value="in">in</option>
- </Input>
- </FormGroup>
- <FormGroup floating label="see energy carrier specification node">
- <Input type="number" min={0} max={5} step={1} bind:value={energycarriers} placeholder="number placeholder"/>
- <Input type="range" min={0} max={5} step={1} bind:value={energycarriers} placeholder="range placeholder"/>
- </FormGroup>
- <FormGroup floating label="Share of this thrust in relation to required aircraft thrust">
- <Input type="number" min={0} max={1} step={0.1} bind:value={thrust_share} placeholder="number placeholder"/>
- <Input type="range" min={0} max={1} step={0.1} bind:value={thrust_share} placeholder="range placeholder"/>
- </FormGroup>
-
- <h5>Systems information</h5>
- <FormGroup floating label="Way the power is generated from the source">
- <Input type="select" placeholder="Enter a value">
- <option value="propulsor">propulsor</option>
- <option value="turbo">turbo</option>
- <option value="electric">electric</option>
- <option value="fuel_cell">fuel_cell</option>
- </Input>
- </FormGroup>
- <p>dieser bereich ist verwirrend, unterkategorien?</p>
-
- <h5>Skinning Information</h5>
- <FormGroup floating label="Material of skinning">
- <Input placeholder="Enter a value"/>
- </FormGroup>
- <FormGroup floating label="Thickness of skinning">
- <Input type="number" min={0.0001} max={0.1} step={0.0001} bind:value={thickness} placeholder="number placeholder"/>
- <Input type="range" min={0.0001} max={0.1} step={0.0001} bind:value={thickness} placeholder="range placeholder"/>
- </FormGroup>
-
- <h5>Technology</h5>
- <Input type="switch" label="Switch if variable camber is used" />
-
- <h5>Energy tanks information?</h5>
- <p>energiecarrier wieder, machmal bei auswahl zahlen manchmal direkt wörter</p>
- <FormGroup floating label="Component where the tank is located">
- <Input type="select" placeholder="Enter a value">
- <option value="fusalage">fusalage</option>
- <option value="wing">wing</option>
- <option value="horizontal_stabilizer">horizontal_stabilizer</option>
- </Input>
- </FormGroup>
- <FormGroup floating label="Position of tank in location">
- <Input type="select" placeholder="Enter a value">
- <option value="tailcone">tailcone</option>
- <option value="rear">rear</option>
- <option value="front">front</option>
- <option value="top">top</option>
- <option value="bottom">bottom</option>
- <option value="center">center</option>
- <option value="inner_left">inner_left</option>
- <option value="outer_left">outer_left</option>
- <option value="inner_right">inner_right</option>
- <option value="outer_right">outer_right</option>
- <option value="total">total</option>
- </Input>
- </FormGroup>
-
- <h5>Aircraft design requirements</h5>
- <h6>TLAR</h6>
- <FormGroup floating label="Maximum structual payload mass which can be carried by the aircraft (e.g. for short trips) in kg">
- <Input type="number" min={100} max={150000} step={100} bind:value={maximum_structrual_payload_mass} placeholder="number placeholder"/>
- <Input type="range" min={100} max={150000} step={100} bind:value={maximum_structrual_payload_mass} placeholder="range placeholder"/>
- </FormGroup>
- <FormGroup floating label="Design takeoff distance (Balanced Field Length) at Sea Level with maximum takeoff mass (MTOM) and (ISA + deltaISA)-Conditions in m">
- <Input type="number" min={600} max={5000} step={1} bind:value={takeoff_distance} placeholder="number placeholder"/>
- <Input type="range" min={600} max={5000} step={1} bind:value={takeoff_distance} placeholder="range placeholder"/>
- </FormGroup>
- <FormGroup floating label="Needed runway length at Sea Level with maximum landing mass (MLM) and (ISA + deltaISA)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6) in m">
- <Input type="number" min={600} max={5000} step={1} bind:value={landing_field_length} placeholder="number placeholder"/>
- <Input type="range" min={600} max={5000} step={1} bind:value={landing_field_length} placeholder="range placeholder"/>
- </FormGroup>
- <FormGroup floating label="ICAO reference code - code_number 1-4 (field length) + code_letter A-F (wing span limits) + faa ADG code number I-VI (wing span limits + tail height limits) + Aircraft Approach Category letter A-D">
- <Input placeholder="Enter a value"/>
- </FormGroup>
- <p>mit check dass code stimmt?</p>
-
-
-</Form>
+<div class="tabs">
+ {#each Object.keys($settingData) as tab}
+ <button
+ on:click={() => selectTab(tab)}
+ class:selected={selectedTab === tab}
+ >
+ {tab}
+ </button>
+ {/each}
+</div>
+
+<div class="tab-content">
+ <!--TODO: fix the type error, even it doesnt break anything-->
+ {#if $settingData[selectedTab]}
+ {#key selectedTab}
+ <TabComponent data={$settingData[selectedTab]} />
+ {/key}
+ {/if}
+</div>
-<Styles/>
\ No newline at end of file
+<Styles />
diff --git a/UnicadoGUI/Frontend/src/stores/projects.js b/UnicadoGUI/Frontend/src/stores/projects.js
new file mode 100644
index 0000000000000000000000000000000000000000..51b8cc676ad846d25eb06bafebe3d559777742f0
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/stores/projects.js
@@ -0,0 +1,220 @@
+import { writable } from 'svelte/store';
+import JSZip from 'jszip';
+
+
+function getStoredProjects() {
+ if (typeof window !== 'undefined') {
+ const storedProjects = localStorage.getItem('userProjects');
+ return storedProjects ? JSON.parse(storedProjects) : [];
+ }
+ return [];
+}
+
+function toggleIsSavePending() {
+ isSavePending.update(value => !value);
+}
+const initialProjects = getStoredProjects();
+
+export const userProjects = writable(initialProjects);
+export const isSavePending = writable(false);
+
+if (typeof window !== 'undefined') {
+ userProjects.subscribe(projects => {
+ localStorage.setItem('userProjects', JSON.stringify(projects));
+ });
+}
+
+
+/**
+ * @param {string} name
+ */
+export function addProject(name) {
+ userProjects.update(projects => {
+ const maxId = projects.reduce((/** @type {number} */ max, /** @type {{ id: number; }} */ project) => project.id > max ? project.id : max, 0);
+ const newProject = { id: maxId + 1, name };
+ toggleIsSavePending();
+ return [...projects, newProject];
+ });
+}
+
+/**
+ * @param {string} name
+ */
+export function removeProject(name) {
+ toggleIsSavePending();
+ userProjects.update(projects => {
+ return projects.filter((/** @type {{ name: string; }} */ project) => project.name !== name);
+ });
+}
+
+/**
+ * @param {number} id
+ */
+export function removeProjectById(id) {
+ toggleIsSavePending();
+ userProjects.update(projects => {
+ return projects.filter((/** @type {{ id: number; }} */ project) => project.id !== id);
+ });
+}
+
+
+/**
+ * @typedef {Object} Project
+ * @property {string} name - Der Name des Projekts
+ * @property {number} id - Die Projektid
+ * very basic structure for the Projects
+ */
+
+/**
+ * Saves to Projects to a zip file
+ * @returns {Promise<void>}
+ */
+export const saveProjectsAsZip = async () => {
+ toggleIsSavePending();
+
+ /** @type {Project[]} */
+ let projectArray = [];
+ userProjects.subscribe(value => {
+ projectArray = value;
+ })();
+
+ const zipBlob = await createZipFile(projectArray);
+ const url = URL.createObjectURL(zipBlob);
+ const a = document.createElement('a');
+ a.href = url;
+ a.download = 'projects.zip';
+
+ document.body.appendChild(a);
+ a.click();
+
+ document.body.removeChild(a);
+ URL.revokeObjectURL(url);
+};
+
+/**
+ * @param {number} id - Die Projekt-ID
+ * @returns {string | undefined} - Der Name des Projekts oder undefined, wenn nicht gefunden
+ */
+export function getProjectNameById(id) {
+ let projectName;
+ userProjects.subscribe((projects) => {
+ const project = projects.find((/** @type {Project} */ p) => p.id === id);
+ projectName = project ? project.name : undefined;
+ })();
+ return projectName;
+}
+
+
+/**
+* Loads the Project List from a zip file
+*/
+export const loadProjectsFromZip = (/** @type {File} */ file) => {
+ loadProjectList(file);
+ toggleIsSavePending();
+};
+
+const loadProjectList = async (/** @type {File} */ file) => {
+ const zip = new JSZip();
+ zip.loadAsync(file).then(async (zipContent) => {
+ /** @type {Project[]} */
+ const projectArray = [];
+ /** @type {any[]} */
+ const promises = [];
+ zipContent.forEach(async (relativePath, file) => {
+ const folderName = relativePath.split("/")[0];
+ if (file.dir) return;
+
+ const fileName = file.name.split("/")[1];
+ if (fileName === "data.json") {
+ const promise = file.async("text").then(content => {
+ try {
+ const projectData = JSON.parse(content);
+ projectArray.push({ name: folderName, id: projectData.id });
+ } catch (error) {
+ console.error(`Error while trying to load ${folderName}:`, error);
+ }
+ });
+ promises.push(promise);
+ }
+ });
+ await Promise.all(promises);
+ userProjects.set(projectArray);
+ alert("Project list loaded successfully");
+ }).catch(error => {
+ alert("Error while loading the project list from a file");
+ console.error(error);
+ });
+}
+
+/**
+ * helper function that parse the project zip file and loads it into the userProject list
+ */
+export const saveProjectsOnServer = async () => {
+ /** @type {Project[]} */
+ let projectArray = [];
+ userProjects.subscribe(value => {
+ projectArray = value;
+ })();
+
+ const zipBlob = await createZipFile(projectArray);
+ const formData = new FormData();
+ formData.append("file", new Blob([zipBlob]), "projects.zip");
+
+ try {
+ const response = await fetch('http://127.0.0.1:8000/projects/', {
+ method: "POST",
+ body: formData,
+ });
+
+ if (!response.ok) {
+ throw new Error("Failed to upload ZIP file");
+ }
+
+ toggleIsSavePending();
+ console.log("ZIP file uploaded successfully");
+ } catch (error) {
+ console.error("Error uploading file:", error);
+ }
+}
+
+/**
+ * Function to load the project list from the server
+ */
+export const loadProjectsFromServer = async () => {
+ try {
+ const response = await fetch('http://127.0.0.1:8000/projects/', {
+ method: "GET",
+ });
+ if (!response.ok) {
+ throw new Error("Failed to download the project list");
+ }
+ const blob = await response.blob();
+ const file = new File([blob], "projects.zip", { type: blob.type });
+ await loadProjectList(file);
+ toggleIsSavePending();
+ } catch (error) {
+ throw error;
+ }
+}
+
+
+/**
+ * helper function:
+ * generates a zip file with all the project files, every project gets its own directory
+ */
+const createZipFile = async (/** @type {Project[]} */ projects) => {
+ const zip = new JSZip();
+
+ projects.forEach((project) => {
+ const folder = zip.folder(project.name);
+
+ if (folder) {
+ const fileContent = JSON.stringify({ id: project.id }, null, 2);
+ folder.file("data.json", fileContent);
+ } else {
+ console.error(`Could not create folder for project: ${project.name}`);
+ }
+ });
+
+ return await zip.generateAsync({ type: "blob" });
+};
\ No newline at end of file
diff --git a/UnicadoGUI/Frontend/src/stores/settings.js b/UnicadoGUI/Frontend/src/stores/settings.js
new file mode 100644
index 0000000000000000000000000000000000000000..fd01e7c53764ac83938da680396a6499a8c5f914
--- /dev/null
+++ b/UnicadoGUI/Frontend/src/stores/settings.js
@@ -0,0 +1,30 @@
+import { writable } from 'svelte/store';
+
+// Define the type for the entire settings data object
+/**
+ * @typedef {Object<string, string>} SettingsData
+ */
+
+export const settingData = writable({});
+
+
+/**
+ * Load XML data into the tab store dynamically.
+ * @param {string} data - The XML data as a string.
+ * @returns {Promise<void>}
+ */
+async function loadTabData(data) {
+ const parsedXML = JSON.parse(data);
+ const root = parsedXML.aircraft_exchange_file;
+
+ /** @type {SettingsData} */
+ const tabs = {};
+
+ for (const [key, value] of Object.entries(root)) {
+ tabs[key] = value;
+ }
+
+ settingData.set(tabs);
+}
+
+export { loadTabData };
\ No newline at end of file