Propagating Interplanetary Trajectories from Earth to Mars

版本 1.2.0.0 (15.9 MB) 作者: David Eagle
Numerically integrate the orbital equations of motion of an Earth to Mars interplanetary trajectory.
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更新时间 2023/3/6

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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.

引用格式

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. 检索来源 .

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版本 已发布 发行说明
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