Satellite Ephemeris to LLA (eph2LLA.m)
版本 1.0.0.0 (1.5 KB) 作者:
Jonathon Cheah
This function provides a quick calculation of a satellite LLA from Kepler elements
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.
引用格式
Jonathon Cheah (2024). Satellite Ephemeris to LLA (eph2LLA.m) (https://www.mathworks.com/matlabcentral/fileexchange/55698-satellite-ephemeris-to-lla-eph2lla-m), MATLAB Central File Exchange. 检索时间: .
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R2013a
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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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1.0.0.0 |