Path: Orbit/OrbitPropagator
% High fidelity orbit model designed to work with ode113.
Called by the OrbitPropagator GUI. Uses AGravityC. Uses ECIToPlanet with
high-fidelity option for the Earth using TruEarth. Selects atmosphere model
based on input.
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Form:
vargout = FOrbHFOP( t, x, flag, d )
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Inputs
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t (1,1) Time
x (6,1) The state vector [x;y;z;dx/dt;dy/dt;dz/dt]
flag (1,:) Event flag for ode113
d (.) Data structure
.planet (1,:) Planet name
.jD (1,1) Julian date
.thrustModelOn (1,1) Thrust function flag
.thrustFunction (*) Thrust function name/handle
.thrustFunctionTag (1,1 Thrust function tag
.solarModelOn (1,1) Solar function flag
.solarFunction (*) Solar function name/handle
.solarFunctionTag (1,1) Solar function tag
.aeroModelOn (1,1) Aero function flag
.atmosphere '' Type of atmosphere model
.densFunction (*) Aero function name/handle
.densFunctionTag (1,1) Aero function tag
.propagateEF (1,1) Propagate earth-fixed flag
.propagateECIR (1,1) Propagate ECIR flag
.stopping (:) Stopping condition data structure
.nTess (1,1) Number of tesseral harmonics
.nZonal (1,1) Number of zonal harmonics
.gravityModel (.) Gravity model
.s (:,:) S terms
.c (:,:) C terms
.j (:) m = 0 terms
.mu (1,1) Gravitational parameter (km^3/sec^2)
.a (1,1) Earth radius
.name (1,1) Planet name
.isNormalized (1,1) Boolean for normalization
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Outputs
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xDot (6,1) The state vector derivative [x;y;z;dx/dt;dy/dt;dz/dt]
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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/R2LatLon Orbit: GravityModels/LoadGEM Orbit: GravityModels/NormalizationMatrix Orbit: OrbitCoord/RV2AE Orbit: OrbitCoord/SLR Orbit: OrbitMechanics/AGravityC Orbit: OrbitMechanics/APlanet Orbit: OrbitMechanics/Energy Orbit: OrbitMechanics/FlightPathAngle Orbit: OrbitMechanics/PlanetaryAccelerations Orbit: OrbitMechanics/RVOrbGen Orbit: OrbitPropagator/StoppingConditions SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu 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/GMSTime SC: Ephem/MSidDay SC: Ephem/MoonRot SC: Ephem/MoonV1 SC: Ephem/Moons SC: Ephem/NutDelta SC: Ephem/ObOfE SC: Ephem/SunV1 SC: Ephem/TruEarth SC: SCData/sCTConstants SC: SCMat/GEMT1 Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeBlankLT Common: General/DeleteCell Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/Axis3D 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: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2T Common: Time/JDToMidnight Common: Time/T2JD Math: Linear/Cross Math: Linear/Dot Math: Linear/DupVect Math: Linear/Factorl Math: Linear/Mag Math: Linear/Unit Math: MathUtils/R2P5 Math: Trigonometry/CosD Math: Trigonometry/SinD
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