J20002RotPulsPlanetMoon:

Path: Orbit/OrbitCoord

% Transform a state vector from the J2000 reference frame to a rotating
   pulsating reference frame centered at the barycenter of the secondary
   body's system.

   Since version 9.
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   Form:
   stateOut = J20002RotPulsPlanetMoon(stateIn,primaryEph,muPrimary,secondaryEph);
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   ------
   InputsP
   ------
   stateIn        (6,1)   Initial state vector
   primaryEph     (6,1)   State vector of Primary Object
   muPrimary       (1)    Gravitational Parameter of Object
   secondaryEph   (6,1)   State vector of Secondary Object
   
   -------
   Outputs
   -------
   stateOut       (6,1)   Output state vector

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Children:

Math: Linear/Mag
Math: Linear/Unit

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