MoonRot:

Path: SC/Ephem

% Computes the matrix that transforms from ECI to selenographic axes.
   mean is the default type.

   Type MoonRot for a demo.

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   Form:
   [g, omega] = MoonRot( jD, type )
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   ------
   Inputs
   ------
   jD      (1,1) Julian Date
   type    (1,4) 'mean' or 'true'

   -------
   Outputs
   -------
   g       (3,3) ECI To Selenographic
   omega   (3,1) ECI Polar rotation vector

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   References:   Escobal, P. R., Methods of Orbit Determination, Krieger, 
                 pp. 413-416.
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