Path: Orbit/OrbitSim
% Interstellar mission simulation with a sun gravity assist. The spacecraft is put into an elliptical orbit with a near sun perigee. Near perigee a high-power plasma thruster performs a delta-V. The delta-V is amplified by the sun's gravity well. Since version 2. ------------------------------------------------------------------------ See also Constant, TextS, TitleS, XLabelS, YLabelS, RK4, RARP2A, Period, VOrbit, FHel ------------------------------------------------------------------------ % --------------------------------------------------------------------------- Copyright 1998 Princeton Satellite Systems, Inc. All rights reserved. ---------------------------------------------------------------------------
AC: ACData/ACTConstants Orbit: OrbitCoord/RARP2A Orbit: RHSOrbit/FHel SC: BasicOrbit/Period 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/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TextS Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Math: Integration/RK4 Math: Linear/DupVect
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