Rotating2Inertial:

--------------------------------------------------------------------------
   Converts a coordinates in a rotating reference frame (such as the 
   rotating coordinates typically used in the circular restricted three body 
   problem)  to coordinates in an inertial reference frame.  Both frames are 
   centered at the secondary body. The rotating coordinate system has the
   primary body fixed on the x-axis
--------------------------------------------------------------------------
   Form:
   stateOut = Rotating2Inertial(stateIn,primary,muPrimary)
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   stateIn		(6,1)    State vector in the 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 non-rotating frame

--------------------------------------------------------------------------

Children:

Common: Math/Mag
Common: Math/Unit