Path: SC/Ephem
% Computes the matrix from mean of Aries 2000 to planet fixed frame. Includes all of the planets and many of the moons. Returns the identity matrix if the moon is unknown. For the Earth's moon it returns the true rotation matrix. -------------------------------------------------------------------------- Form: c = ECIToPlanet( jD, planet, kEarth ) -------------------------------------------------------------------------- ------ Inputs ------ jD (1,1) Julian date planet (1,:) Name of the planet kEarth (1,1) If 0 use TruEarth, if 1 is TruEarth with eofe, if <0 use Montenbruck (see also ECIToEF) ------- Outputs ------- c (3,3) Matrix from Mean of 2000.0 to planet fixed -------------------------------------------------------------------------- References: Seidelmann, ed. The Explanatory Supplement to the Astronomical Almanac, University Science Books, 1992, p. 705. --------------------------------------------------------------------------
Common: Database/Constant Common: Graphics/Plot2D Common: Time/Date2JD Common: Time/JD2T Common: Time/T2JD OrbitMiniToolbox: Support/TruEarth SC: Ephem/MoonRot SC: Ephem/Moons
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