Path: Orbit/LowEnergyManeuver
% Transfer a CRTBP LET to the restricted 3 body, non-planar problem.
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Form:
[elementsNew,dV1EphNew] = Targeting3BP2(elements,dV1Eph,dt,et,muMoon)
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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
dt (1,1) Transfer time
et (1,1) Seconds after the Epoch at which the transfer
is initiated
muMoon (1,1) Gravitational parameter of the Moon
jDate (1,1) Julian date
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Outputs
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elementsNew (1,6) Converged ecliptic orbital elements
dV1EphNew (1,1) Converged maneuver magnitude
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AC: ACData/ACTConstants Orbit: LowEnergyManeuver/CheckForOptimizationToolbox Orbit: LowEnergyManeuver/J20002RotPuls Orbit: LowEnergyManeuver/PlotLET3BP Orbit: LowEnergyManeuver/Propagate3BP 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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