Earth-to-Mars Interplanetary TCM Optimization - OTB
Version 1.1.0 (15,6 MB) von
David Eagle
Optimization Toolbox version of the MATLAB script that determines optimal Earth-to-Mars TCM maneuvers.
PDF document and a MATLAB script called e2m_tcm which can be used to solve the classic one impulse, Earth-to-Mars interplanetary trajectory correction maneuver (TCM) optimization problem. The software implements a simple shooting method that attempts to minimize the TCM delta-v while numerically integrating the n-body heliocentric equations of motion and solving for user-defined final orbit conditions at Mars.
Zitieren als
David Eagle (2024). Earth-to-Mars Interplanetary TCM Optimization - OTB (https://www.mathworks.com/matlabcentral/fileexchange/73775-earth-to-mars-interplanetary-tcm-optimization-otb), MATLAB Central File Exchange. Abgerufen .
Kompatibilität der MATLAB-Version
Erstellt mit
R2019b
Kompatibel mit allen Versionen
Plattform-Kompatibilität
Windows macOS LinuxKategorien
- Aerospace > Aerospace Blockset > Visualization >
- Sciences > Earth, Ocean, and Atmospheric Sciences > Earth and Planetary Science >
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Version | Veröffentlicht | Versionshinweise | |
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1.1.0 | Updated to use DE421.bsp JPL ephemeris (included in the zip distribution file) and MICE routines. |
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1.0.0 |