ENUToECEF:

Path: Orbit/OrbitCoord

% Compute the transformation matrix that rotates ENU to ECEF coordinates.
   ENU is East-North-Up. Assumes spherical Earth.

   Since version 8.
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   Form:
   T = ENUToECEF( lat, lon )
   T = ENUToECEF( r )
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   ------
   Inputs
   ------
   lat         (1,1)   Latitude (rad)
   lon         (1,1)   Longitude (rad)
         OR
   r           (3,1)   Earth fixed position  

   -------
   Outputs
   -------
   T           (3,3)   ENU to ECEF rotation matrix

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