Path: Interplanetary/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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Interplanetary: Ephemeris/PlanetPositionEMBarycenter Interplanetary: LowEnergyManeuver/J20002RotPuls Interplanetary: LowEnergyManeuver/Propagate4BP SC: BasicOrbit/El2RV Common: Database/Constant Common: Graphics/NewFig Math: Linear/Unit
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