Rotating2Inertial:

Path: AerospaceUtils/Coord

% Converts a coordinates in a rotating reference frame to inertial.
 For example, convert 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.
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   Form:
   stateOut = Rotating2Inertial(stateIn,primary,muPrimary)
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   ------
   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

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Children:

Math: Linear/Mag

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