PlotLET3BP:

Path: Orbit/LowEnergyManeuver

% Plot the Low Energy Transfer for a 3 body problem in a Non-Rotating
   Frame as well as in a Sun-Earth Rotating Frame

   Since version 9.
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   Form:
   h = PlotLET3BP(elements,dV1Eph,det,h);
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   ------
   Inputs
   ------
   elements         (1,6)    Eclptic orbital elements of the intial state
   dV1Eph            (1)     Magnitude of the initial burn
   det               (1)     Transfer time
   h                (1,2)    Optional. Figure handles to use for plots.

   -------
   Outputs
   -------
   h                (1,2)    Figure handles used for the plots.
  
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Children:

Common: Database/Constant
Common: Graphics/NewFig
Math: Linear/Unit
Orbit: OrbitCoord/J20002RotPuls
Orbit: OrbitSim/Propagate3BP
SC: BasicOrbit/El2RV
SC: Ephem/PlanetPositionEMBarycenter

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