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
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jD (1,1) Julian Date
type (1,4) 'mean' or 'true'
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Outputs
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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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