Propagating Interplanetary Trajectories from Earth to Mars

Version 1.2.0.0 (15,9 Mo) par David Eagle
Numerically integrate the orbital equations of motion of an Earth to Mars interplanetary trajectory.
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Mise à jour 6 mars 2023

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PDF document and a MATLAB script called pprop_e2m that can be used to numerically integrate the geocentric and heliocentric orbital equations of motion of an Earth to Mars interplanetary trajectory. This scientific simulation begins at a user-defined epoch and state vector somewhere within the Earth’s sphere-of-influence (SOI) and ends at (1) closest approach to Mars, (2) a user-defined Mars-centered (areocentric) distance, or (3) at a user-defined final epoch.

Citation pour cette source

David Eagle (2024). Propagating Interplanetary Trajectories from Earth to Mars (https://www.mathworks.com/matlabcentral/fileexchange/41356-propagating-interplanetary-trajectories-from-earth-to-mars), MATLAB Central File Exchange. Récupéré le .

Compatibilité avec les versions de MATLAB
Créé avec R2019b
Compatible avec toutes les versions
Plateformes compatibles
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Version Publié le Notes de version
1.2.0.0

Trajectory now initialized and results displayed in the Earth mean equator and equinox of J2000 (EME2000) coordinate system. Code clean up.
1.1.0.0

Updated ephemeris to use DE421.bsp data file. Geocentric and heliocentric orbits displayed in Earth true-of-date coordinate system. Updated PDF documentation.
1.0.0.0