Path: AerospaceUtils/Coord
% Computes the matrix from mean of Aries 2000 to the earth fixed frame. Accounts for Earth rotation, nutation, and precession. -------------------------------------------------------------------------- Form: c = ECIToEF( T ) -------------------------------------------------------------------------- ------ Inputs ------ T (1,1) Julian century ------- Outputs ------- c (3,3) Matrix from Mean of 2000.0 to planet fixed -------------------------------------------------------------------------- References: Seidelmann, The Explanatory Supplement to the Astronomical Almanac, University Science Books, 1992, p. 705. Montenbruck, O., Pfleger, T., "Astronomy on the Personal Computer, Second Edition." --------------------------------------------------------------------------
Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2T Common: Time/T2JD
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