Path: Orbit/OrbitPropagator
% Computes the engine force vector in the ECI frame.
The input is in the LVLH frame.
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Form:
x = FEngine( action, modifier, u, t )
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Inputs
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action (1,:) Action 'initialize', 'update'
modifier (1,:) Modifier to the action or data structure if initialization
u (7,1) [r;v;m]
t (1,1) Time
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Outputs
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x (1,1) The tag if action is 'initialize'
If the action is update
x.f (3,1) Force vector in the ECI frame
x.mDot (1,1) Mass derivative
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AC: ACData/ACTConstants AerospaceUtils: AtmosphericCalculations/AtmDens1 AerospaceUtils: AtmosphericCalculations/AtmDens2 AerospaceUtils: AtmosphericCalculations/AtmDensTitan AerospaceUtils: AtmosphericCalculations/NeptuneDensity AerospaceUtils: Coord/ECIToEF AerospaceUtils: Coord/EFToLatLonAlt AerospaceUtils: Coord/QLVLH AerospaceUtils: Coord/R2LatLon Orbit: GravityModels/LoadGEM Orbit: GravityModels/LoadGravityModel Orbit: GravityModels/NormalizationMatrix Orbit: GravityModels/UnnormalizeGravity Orbit: OrbitCoord/RV2AE Orbit: OrbitCoord/SLR Orbit: OrbitMechanics/AGravity Orbit: OrbitMechanics/AGravityC Orbit: OrbitMechanics/APlanet Orbit: OrbitMechanics/Energy Orbit: OrbitMechanics/FlightPathAngle Orbit: OrbitMechanics/OrbitJacobian Orbit: OrbitMechanics/PlanetaryAccelerations Orbit: OrbitMechanics/RVOrbGen Orbit: OrbitPropagator/FOrbHFOP Orbit: OrbitPropagator/PropagateOrbitPlugIn Orbit: OrbitPropagator/StoppingConditions Orbit: OrbitPropagator/StoppingPlugIn Orbit: RHSOrbit/FOrbHF2 SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/El2RV SC: BasicOrbit/FOrbCart SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/Period SC: BasicOrbit/RV2El SC: Environs/MolWt2R SC: Ephem/ECIToPlanet SC: Ephem/EOfE SC: Ephem/EarthNut SC: Ephem/EarthPre SC: Ephem/EarthRot SC: Ephem/EarthRte SC: Ephem/GMSTime SC: Ephem/MSidDay SC: Ephem/MoonRot SC: Ephem/MoonV1 SC: Ephem/Moons SC: Ephem/NutDelta SC: Ephem/ObOfE SC: Ephem/S2HMS SC: Ephem/SunV1 SC: Ephem/TruEarth SC: GUIPlugIn/ElementsPlugIn SC: Help/HelpSystem SC: SCData/sCTConstants SC: SCMat/GEMT1 Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: GUIs/TimeGUI Common: General/CellToMat Common: General/CloseFigure Common: General/CloseIfHandle Common: General/DeBlankLT Common: General/DeleteCell Common: General/DispWithTitle Common: General/GetCurrentGUIObject Common: General/GetListString Common: General/IsVersionAfter Common: General/MatToCell Common: General/RadioButtons Common: General/SaveStructure Common: General/SetUIElement Common: General/StringMatch Common: General/StringToTokens Common: General/StructToCell2D Common: General/UIElement Common: General/ValidTime Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/Ellipsd Common: Graphics/Map Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PlotDoubleYAxis Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Plugins/TimePlugIn Common: Quaternion/Mat2Q Common: Quaternion/QTForm Common: Time/DN2Date Common: Time/DNString2Date Common: Time/DTAToDTS Common: Time/DTSToDTA Common: Time/Date2DN Common: Time/Date2JD Common: Time/FindSolsticeOrEquinox Common: Time/JD2000 Common: Time/JD2Date Common: Time/JD2T Common: Time/JDToMidnight Common: Time/T2JD Common: Transform/RPhiTheta2Cart Math: Analysis/JacobianODE Math: Analysis/PDAL Math: Analysis/SCHarm Math: Linear/Cross Math: Linear/Dot Math: Linear/DupVect Math: Linear/Factorl Math: Linear/Mag Math: Linear/Skew Math: Linear/SkewSq Math: Linear/Unit Math: MathUtils/R2P5 Math: Probability/CovarianceRHS Math: Trigonometry/CosD Math: Trigonometry/SinD
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