Satellite Ephemeris to LLA (eph2LLA.m)
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.
Cita come
Jonathon Cheah (2025). Satellite Ephemeris to LLA (eph2LLA.m) (https://it.mathworks.com/matlabcentral/fileexchange/55698-satellite-ephemeris-to-lla-eph2lla-m), MATLAB Central File Exchange. Recuperato .
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- Industries > Aerospace and Defense > CubeSat and Satellites >
- Simulink > Applications > Aerospace Applications >
- Industries > Aerospace and Defense >
- Aerospace and Defense > Aerospace Blockset > Reference Applications >
- Engineering > Aerospace Engineering > Satellite and Orbital Mechanics >
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| Versione | Pubblicato | Note della release | |
|---|---|---|---|
| 1.0.0.0 |
