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
   c = HelioToPlanet( jD, planet, kEarth )	

   jD         (1,1)  Julian date
   planet     (1,:)  Name of the planet
   kEarth     (1,1)  If 0 use TruEarth, if 1 is TruEarth with eofe

   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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