Satellite Ephemeris to LLA (eph2LLA.m)

Versión 1.0.0.0 (1,52 KB) por Jonathon Cheah
This function provides a quick calculation of a satellite LLA from Kepler elements
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Actualizado 29 feb 2016

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Calculation of longitude, latitude and height of a satellite from its ephemeris data is often cumbersome, even with all the necessary functions available. This function does the calculation in a straight forward and self contained manner. It is useful to compute the variations of the satellite position when looking at the daily ephemeris updates of a satellite such as those published by IntelSat.

Citar como

Jonathon Cheah (2025). Satellite Ephemeris to LLA (eph2LLA.m) (https://es.mathworks.com/matlabcentral/fileexchange/55698-satellite-ephemeris-to-lla-eph2lla-m), MATLAB Central File Exchange. Recuperado .

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Se creó con R2013a
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Versión Publicado Notas de la versión
1.0.0.0