Propagating Interplanetary Trajectories from Earth to Mars
バージョン 1.2.0.0 (15.9 MB) 作成者:
David Eagle
Numerically integrate the orbital equations of motion of an Earth to Mars interplanetary trajectory.
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.
引用
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. に取得済み.
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Start Hunting!バージョン | 公開済み | リリース ノート | |
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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. |
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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. |
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1.0.0.0 |