Path: Orbit/OrbitCoord
% Computes the transformation matrix from heliocentric 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. See also CEcl2Eq, ECIToPlanet Since version 2014.1 -------------------------------------------------------------------------- Form: c = HelioToPlanet( 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 ------- Outputs ------- c (3,3) Matrix from heliocentric to planet fixed --------------------------------------------------------------------------
AC: ACData/ACTConstants SC: Ephem/CEcl2Eq SC: Ephem/ECIToPlanet 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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