A MATLAB Script for Predicting the Evolution of Lunar Orbits

Version 1.1.0.0 (17,5 Mo) par David Eagle
Script for propagating spacecraft lunar orbits subject to non-spherical lunar gravity and third-body gravity.
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Mise à jour 23 jan. 2022

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PDF document and MATLAB script named lprop_matlab which can be used to predict the long-term evolution of lunar orbits. The software integrates the selenocentric or moon-centered Cartesian equations of motion using a variable step size Runge-Kutta-Fehlberg 7(8) numerical method. The selenocentric equations of motion include the non-spherical gravity of the moon and (optionally) the point-mass gravity of the earth and sun. The ephemeris source for this script is JPL DE421 and the default lunar gravity model is LP150q.

Citation pour cette source

David Eagle (2024). A MATLAB Script for Predicting the Evolution of Lunar Orbits (https://www.mathworks.com/matlabcentral/fileexchange/40485-a-matlab-script-for-predicting-the-evolution-of-lunar-orbits), MATLAB Central File Exchange. Récupéré le .

Compatibilité avec les versions de MATLAB
Créé avec R2019b
Compatible avec toutes les versions
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Version Publié le Notes de version
1.1.0.0

Updated to use JPL DE421.bsp ephemeris and MICE routines.
1.0.0.0