Path: Orbit/LowEnergyManeuver
% Transfer a LET from the restricted 3BP to the Sun/Planet/Moon 4BP
--------------------------------------------------------------------------
Form:
[elementsNew,dV1EphNew,dtNew,exitflag] = Targeting4BP(elements,dV1Eph,
dtTarg,et,p,jDate,muPlanet)
--------------------------------------------------------------------------
------
Inputs
------
elements (1,6) Ecliptic orbital elements of the initial state
dV1Eph (1,1) Magnitude of the initial burn
dtTarg (1,1) Transfer time
et (1,1) Seconds after the Epoch at which the transfer
is initiated
p (1,1) Distance from the moon to L2
jDate (1,1) Julian date
muMoonMultiplier (1,1) 0 to 1, parameter to ease between 3BP and 4BP
muPlanet (1,1) Gravitational parameter of the planet
-------
Outputs
-------
elementsNew (1,6) Converged ecliptic orbital elements
dV1EphNew (1,1) Converged maneuver magnitude
dtNew (1,1) Converged transfer time
exitflag (1,1) 1 if successful
--------------------------------------------------------------------------
AC: ACData/ACTConstants Orbit: LowEnergyManeuver/CheckForOptimizationToolbox Orbit: LowEnergyManeuver/J20002RotPuls Orbit: LowEnergyManeuver/PlotLET 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
Back to the Orbit Module page