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.
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Form:
c = ECIToPlanet( jD, planet, kEarth )
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Inputs
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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)
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Outputs
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c (3,3) Matrix from Mean of 2000.0 to planet fixed
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References: Seidelmann, ed. The Explanatory Supplement to the
Astronomical Almanac, University Science Books, 1992,
p. 705.
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AC: ACData/ACTConstants SC: Ephem/EOfE SC: Ephem/EarthNut SC: Ephem/EarthPre SC: Ephem/EarthRot SC: Ephem/GMSTime SC: Ephem/MSidDay SC: Ephem/MoonRot SC: Ephem/Moons SC: Ephem/NutDelta SC: Ephem/ObOfE SC: Ephem/TruEarth SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2T Common: Time/JDToMidnight Common: Time/T2JD Math: MathUtils/R2P5 Math: Trigonometry/CosD Math: Trigonometry/SinD
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