CoordinateTransform:

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

--------------------------------------------------------------------------
   Form:
   x = CoordinateTransform( from, to, x, jD )
--------------------------------------------------------------------------

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

   -------
   Outputs
   -------
   xT        (3,:)   Vectors transformed

--------------------------------------------------------------------------

Children:

AerospaceUtils: Coord/ECIToEF
AerospaceUtils: Coord/EFToLatLonAlt
AerospaceUtils: Coord/LatLonAltToEF
Common: Time/JD2T
OrbitMiniToolbox: Support/TruEarth

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