Path: Missions/LunarMission
% Lunar transfer simulation Demonstrates an elliptical transfer orbit to the moon and orbit insertion. The moon's orbit is approximated as circular and the transfer orbit is in the plane of the moon's orbit. The insertion is computed and the orbit around the moon simulated. ------------------------------------------------------------------------ See also RPRA2AE, OrbMnvrInsertion, RVOrbGen, Constant, Plot2D, TimeLabl, Period, RV2El, RK4 ------------------------------------------------------------------------ % -------------------------------------------------------------------------- Copyright (c) 2014 Princeton Satellite Systems All Rights Reserved. --------------------------------------------------------------------------
AC: ACData/ACTConstants Orbit: OrbitCoord/RPRA2AE Orbit: OrbitCoord/SLR Orbit: OrbitManeuver/OrbMnvrInsertion Orbit: OrbitMechanics/RVOrbGen SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/Period SC: BasicOrbit/RV2El SC: BasicOrbit/RVFromKepler SC: BasicOrbit/VOrbit SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeBlankLT Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/Plot3D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Quaternion/QForm Math: Integration/RK4 Math: Linear/Cross Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit
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