MarsRot:

Path: SC/Ephem

% Computes the matrix that transforms from ECI to areographic axes.
   If two arguments are entered it will add secular components.
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   Form:
   g = MarsRot( jD, useSec )
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   ------
   Inputs
   ------
   jD           Julian Date
   useSec       Add secular variations

   -------
   Outputs
   -------
   g            ECI To Areographic matrix

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	References:   Escobal, P. R., Methods of Orbit Determination, Krieger, 
               pp. 419-421.
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Children:

Common: Time/DTAToDTS
Common: Time/DTSToDTA
Common: Time/Date2JD
Common: Time/JD2Date
Math: MathUtils/R2P5

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