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