RHSCRTBP:

Path: Orbit/LowEnergyManeuver

% Compute the RHS of the CRTBP equations of motion.
   For arbitrary 'mu' parameter - smaller mass divided by total mass of system.

   Since version 9.
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   Form:
   yDot = RHSCRTBP( t, y, mu )
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   ------
   Inputs
   ------
   t              (1,1)    Time (not used)
   y              (6,1)    State vector [r;v]
   mu             (1,1)    CRTBP mass ratio

   -------
   Outputs
   -------
   yDot           (6,1) 	Time derivative of the state vector
  
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Children:

Orbit: LowEnergyManeuverData/f16pRef

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