Path: AerospaceUtils/Coord

% Transform between selected coordinate frames and representations.
 The frames are:

 ECI      Earth centered inertial
 ECR/EF   Earth fixed
 LLR      Geodetic latitude, longitude and altitude

   x = CoordinateTransform( from, to, x, jD )

   from      (1,:)   From (ECI, EF/ECR, LLR)
   to        (1,:)   To (ECI, EF/ECR, LLR)
   x         (3,:)   Vectors
   jD        (3,1)   Julian date

   xT        (3,:)   Vectors transformed



AC: ACData/ACTConstants
AerospaceUtils: Coord/ECIToEF
AerospaceUtils: Coord/EFToLatLonAlt
AerospaceUtils: Coord/LatLonAltToEF
SC: Ephem/EOfE
SC: Ephem/EarthNut
SC: Ephem/EarthPre
SC: Ephem/EarthRot
SC: Ephem/GMSTime
SC: Ephem/MSidDay
SC: Ephem/NutDelta
SC: Ephem/ObOfE
SC: Ephem/TruEarth
SC: SCData/sCTConstants
Common: CommonData/Constants
Common: CommonData/xSplashSmall
Common: Database/Constant
Common: General/DeleteCell
Common: Time/DTSToDTA
Common: Time/Date2JD
Common: Time/JD2000
Common: Time/JD2T
Common: Time/JDToMidnight
Common: Time/T2JD
Math: Linear/Mag
Math: Linear/Unit
Math: MathUtils/R2P5
Math: Trigonometry/CosD
Math: Trigonometry/SinD

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