Propagating Trajectories from the Earth to the Moon
Version 1.2.0.0 (17,6 Mo) par
David Eagle
Integrate n-body trajectories from the Earth to the Moon. Includes non-spherical Earth gravity.
PDF document and a MATLAB script called pprop_lunar that can be used to numerically integrate the geocentric orbital equations of motion of a trajectory from the Earth to the Moon. This scientific simulation begins at a user-defined epoch and geocentric state vector (position and velocity vectors) representing the point of trans-lunar injection (TLI) and ends at (1) closest approach to the Moon, (2) a user-defined Moon-centered (selenocentric) distance, or (3) at a user-defined final epoch.
Citation pour cette source
David Eagle (2024). Propagating Trajectories from the Earth to the Moon (https://www.mathworks.com/matlabcentral/fileexchange/43067-propagating-trajectories-from-the-earth-to-the-moon), MATLAB Central File Exchange. Récupéré le .
Compatibilité avec les versions de MATLAB
Créé avec
R2019b
Compatible avec toutes les versions
Plateformes compatibles
Windows macOS LinuxCatégories
- Aerospace > Aerospace Blockset > Visualization >
- Sciences > Earth, Ocean, and Atmospheric Sciences > Earth and Planetary Science >
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Version | Publié le | Notes de version | |
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1.2.0.0 | Input in true-of-date coordinates. Updated to use JPL *.bsp ephemeris and MICE routines. PDF document updated. |
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1.1.0.0 | Includes new option to model the effect of the Moon on the trajectory using non-spherical lunar gravity. |
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1.0.0.0 |