CP2I:

Path: SC/BasicOrbit

% Transformation matrix from the perifocal frame to the inertial frame.

   Since version 1.
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   Form:
   c = CP2I( i, L, w )
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   ------
   Inputs
   ------
   i               (3,1) Inclination (rad)
   L               (3,1) Longitude of the ascending node (rad)
   w               (3,1) Argument of perigee (rad)

   -------
   Outputs
   -------
   c               (3,3) Transformation matrix

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   References: Bate, Roger R., Fundamentals of Astrodynamics, Dover 
               Publications, Inc., New York, 1971, pp. 82-83.
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