Path: Orbit/OrbitSim
% Simulates a spacecraft in earth orbit with spherical harmonics. The gravity model is the GEM-T1 model which is 36 by 36 (zonal and tesseral harmonics) All control is done through the vector aExt. Since version 8. ------------------------------------------------------------------------- See also FOrbCartH, Constant, Plot2D, TimeGUI, TimeLabl, RK4, Date2JD, LoadGEM, El2RV, Period ------------------------------------------------------------------------- % ------------------------------------------------------------------------------- Copyright (c) 2009 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------------
AC: ACData/ACTConstants Orbit: GravityModels/LoadGEM SC: BasicOrbit/CP2I SC: BasicOrbit/E2Nu SC: BasicOrbit/El2RV SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: BasicOrbit/Period 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/CloseIfHandle Common: General/DeBlankLT Common: General/DeleteCell Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/DTSToDTA Common: Time/Date2JD Math: Integration/RK4 Math: Linear/DupVect Math: Linear/Factorl
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