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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
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lat (1,1) Latitude (rad)
lon (1,1) Longitude (rad)
OR
r (3,1) Earth fixed position
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Outputs
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T (3,3) ENU to ECEF rotation matrix
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