J20002RotPuls:

Path: Orbit/OrbitCoord

% Transform from J2000 to rotating-pulsating
 Transform a state vector from the J2000 reference frame to a
 rotating-pulsating reference frame centered on the secondary body.
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   Form:
   stateOut = J20002RotPuls(stateIn,primaryEph,muPrimary);
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   ------
   InputsP
   ------
   stateIn     (6,1)   Initial state vector
   primaryEph  (6,1)   State vector of Primary
   muPrimary    (1)    Gravitational Parameter the Primary
   
   -------
   Outputs
   -------
   stateOut    (6,1)   Output state vector

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Children:

Math: Linear/Mag
Math: Linear/Unit

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