Inertial2Rotating:

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   Converts a coordinates in an inertial reference frame  to coordinates in a 
   rotating reference frame (such as the rotating coordinates typically used in 
   the circular restricted three body problem).  Both frames are 
   centered at the secondary body. The rotating coordinate system has the
   primary body fixed on the x-axis
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   Form:
   stateOut = Inertial2Rotating(stateIn,primary,muPrimary)
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   ------
   Inputs
   ------
   stateIn		(6,1)    State vector in the non-rotating frame
   primary     (6,1)    State vector of the primary body
   muPrimary   (1,1)    Gravitational Parameter of the primary body

   -------
   Outputs
   -------
   stateOut    (6,1)    State vector in the rotating frame

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Children:

Common: Math/Mag
Common: Math/Unit