Earth-to-Mars Interplanetary TCM Optimization - SNOPT
Optimization of interplanetary trajectory correction maneuvers (TCM) during Earth-to-Mars spaceflight using the SNOPT algorithm.
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Cite As
David Eagle (2026). Earth-to-Mars Interplanetary TCM Optimization - SNOPT (https://in.mathworks.com/matlabcentral/fileexchange/48690-earth-to-mars-interplanetary-tcm-optimization-snopt), MATLAB Central File Exchange. Retrieved .
General Information
- Version 1.3.0 (111 MB)
MATLAB Release Compatibility
- Compatible with any release
Platform Compatibility
- Windows
- macOS
- Linux
| Version | Published | Release Notes | Action |
|---|---|---|---|
| 1.3.0 | Updated algorithms, graphics and PDF documentation. |
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| 1.2.0 | Updated several MATLAB functions and PDF documentation. Added areocentric (Mars-centered) graphic of the approach trajectory. |
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| 1.1.0 | Updated to use JPL DE421.bsp ephemeris (included in zip file) and MICE routines. |
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| 1.0.0 |
