Path: Orbit/LowEnergyManeuver
% Plot the Low Energy Transfer
Plot the Low Energy Transfer for a 4 body problem in a Non-Rotating Frame as
well as in a Sun-Earth Rotating Frame. You must initialize the
Barycenter using PlanetPositionEMBarycenter('initialize',[0, 3,10]);
Type PlotLET for a demo.
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Form:
h = PlotLET(elements,dV1Eph,det,jDate,h)
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Inputs
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elements (1,6) Ecliptic orbital elements of the initial state
dV1Eph (1,1) Magnitude of the initial burn
det (1,1) Transfer time
jDate (1,1) Julian date
muMoonMultiplier (1,1) 0 to 1, for the purpose of easing between 3BP and 4BP
h (1,2) Optional. Figure handles to use for plots.
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Outputs
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h (1,2 Figure handles used for the plots.
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AC: ACData/ACTConstants Orbit: LowEnergyManeuver/J20002RotPuls Orbit: LowEnergyManeuver/Propagate4BP 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/RVFromKepler SC: Ephem/CEcl2Eq SC: Ephem/InterpolateState SC: Ephem/PlanetPosJPL SC: Ephem/PlanetPositionEMBarycenter SC: SCData/bin2000 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/DispWithTitle Common: General/MatToCell Common: General/Watermark 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: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit
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