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example_LEO_sim.xml
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example_LEO_sim.xml
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<?xml version="1.0" encoding="ISO-8859-1"?>
<LEOSimulation version="2.5.0">
<STELAVersion>2.5.1</STELAVersion>
<SpaceObject>
<mass unit="kg">1470.0</mass>
<dragArea>15.0</dragArea>
<reflectingArea>15.0</reflectingArea>
<reflectivityCoefficient>1.5</reflectivityCoefficient>
<orbitType>LEO</orbitType>
<VariableDragCoef/>
<name>EXAMPLE space object</name>
</SpaceObject>
<EphemerisManager version="2.5.0">
<initState>
<bulletin version="2.5.0">
<date>2009-07-29T00:00:00.000</date>
<Type2PosVel>
<frame>CELESTIAL_MEAN_OF_DATE</frame>
<nature>MEAN</nature>
<semiMajorAxis unit="m">7062500.0</semiMajorAxis>
<eccentricity>0.0159292035</eccentricity>
<inclination unit="rad">1.7207201095412095</inclination>
<rAAN unit="rad">4.843520977607705</rAAN>
<argOfPerigee unit="rad">0.0</argOfPerigee>
<meanAnomaly unit="rad">0.0</meanAnomaly>
</Type2PosVel>
</bulletin>
</initState>
<finalState>
<bulletin version="2.5.0">
<date>2036-10-16T20:59:08.938</date>
<Type2PosVel>
<frame>CELESTIAL_MEAN_OF_DATE</frame>
<nature>MEAN</nature>
<longitudeTFE>0.0</longitudeTFE>
<epochTFE>2011-05-12T13:09:03.724</epochTFE>
<semiMajorAxis unit="m">6518883.301409532</semiMajorAxis>
<eccentricity>3.065067844123603E-4</eccentricity>
<inclination unit="rad">1.7200551075580324</inclination>
<rAAN unit="rad">3.2602684552180676</rAAN>
<argOfPerigee unit="rad">4.687680003722658</argOfPerigee>
<meanAnomaly unit="rad">1.6122434925375835</meanAnomaly>
</Type2PosVel>
</bulletin>
</finalState>
</EphemerisManager>
<author>CNES</author>
<comment>LEO example simulation</comment>
<simulationDuration unit="years">100.0</simulationDuration>
<ephemerisStep unit="s">86400.0</ephemerisStep>
<ttMinusUT1 unit="s">67.184</ttMinusUT1>
<srpSwitch>true</srpSwitch>
<sunSwitch>true</sunSwitch>
<moonSwitch>true</moonSwitch>
<warningFlag>false</warningFlag>
<iterativeMode>true</iterativeMode>
<modelType>GTO</modelType>
<atmosModel>NRLMSISE-00</atmosModel>
<VariableSolarActivity>
<solActType>VARIABLE</solActType>
</VariableSolarActivity>
<integrationStep unit="s">86400.0</integrationStep>
<dragSwitch>true</dragSwitch>
<dragQuadPoints>33</dragQuadPoints>
<atmosDragRecomputeStep>1</atmosDragRecomputeStep>
<srpQuadPoints>11</srpQuadPoints>
<reentryAltitude unit="m">120000.0</reentryAltitude>
<iterationData>
<funcValueAccuracy unit="days">10.0</funcValueAccuracy>
<expDuration unit="years">24.75</expDuration>
<simMinusExpDuration unit="years">75.25</simMinusExpDuration>
<iterationMethod>FrozenOrbit</iterationMethod>
</iterationData>
<nbIntegrationStepTesseral>5.0</nbIntegrationStepTesseral>
<zonalOrder>7</zonalOrder>
</LEOSimulation>