ECEFToLLA:

Path: AerospaceUtils/Coord

% Compute latitude, longitude, altitude from ECEF position.
 Assumes spherical planet.
--------------------------------------------------------------------------
   Form:
   lla = ECEFToLLA( rECEF, rP );
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   rECEF       (3,:)   ECEF position vector [km]
   rP          (1,1)   Radius of planet (for Earth: 6378.14) [km]
                       

   -------
   Outputs
   -------
   lla         (3,:)   Latitude [rad], longitude [rad], altitude [km]

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

Children:

Math: Linear/Mag

Back to the AerospaceUtils Module page