Path: AerospaceUtils/Coord
% Compute ECEF position from latitude, longitude, altitude.
Assumes spherical planet.
--------------------------------------------------------------------------
Form:
rECEF = LLAToECEF( lla, rP )
--------------------------------------------------------------------------
------
Inputs
------
lla (3,:) Latitude [rad], longitude [rad], altitude [km]
rP (1,1) Radius of planet (for Earth: 6378.14) [km]
-------
Outputs
-------
rECEF (3,1) ECEF position vector [km]
--------------------------------------------------------------------------
Back to the AerospaceUtils Module page