Path: Orbit/LowEnergyManeuver

% Minimize the keplerian energy of the final state of a transfer orbit
 The default bodies are the Earth and the Moon.
   [elementsNew,dV1EphNew,dtNew,f,jTraj,jL2,dV2EphNew,tM2New] =

   elements       (1,6)  Ecliptic orbital elements of the initial state
   dV1Eph          (1)   Magnitude of the initial maneuver
   dtTarg          (1)   Transfer time
   et              (1)   Seconds after the epoch at which the orbit begins
   muMoon          (1)   Gravitational Parameter of the moon
   p               (1)   L2 distance from the moon

   elementsNew     (1)   Optimized ecliptic elements
   dV1EphNew       (1)   Optimized initial maneuver magnitude
   dtNew           (1)   Optimized transfer time
   f               (1)   Final energy with resepect to the moon
   jTraj           (1)   Jacobi constant of the final state
   jL2             (1)   Jacobi constant of the L2 point



AC: ACData/ACTConstants
Orbit: LowEnergyManeuver/CRTBPJacobiConstant
Orbit: LowEnergyManeuver/EnergyWRTMoon
Orbit: LowEnergyManeuver/J20002RotPulsPlanetMoon
Orbit: LowEnergyManeuver/Kms2CRTBP
Orbit: LowEnergyManeuver/Propagate4BP
Orbit: LowEnergyManeuverData/f16Ref
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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