EnergyWRTMoon:

Path: Orbit/LowEnergyManeuver

% Keplerian Energy with respect to the Moon

   Since version 9.
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   Form:
   e = EnergyWRTMoon(t,y,moon,planet,muMoon);
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   ------
   InputsP
   ------
   t          (1)   Seconds after epoch 
   y          (1)   State vector in Earth/Moon Barycentered frame
   muMoon     (1)   Gravitational Parameter of the moon
   
   -------
   Outputs
   -------
   e          (1)   Keplerian energy 

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Children:

Math: Linear/Mag
SC: Ephem/PlanetPositionEMBarycenter

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