Ballistic Interplanetary Trajectory Optimization - OTB
Optimization Toolbox version of a MATLAB script that solves the two impulse, patched-conic interplanetary trajectory problem.
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Cite As
David Eagle (2026). Ballistic Interplanetary Trajectory Optimization - OTB (https://in.mathworks.com/matlabcentral/fileexchange/73513-ballistic-interplanetary-trajectory-optimization-otb), MATLAB Central File Exchange. Retrieved .
General Information
- Version 1.7.0 (111 MB)
MATLAB Release Compatibility
- Compatible with R2019b
Platform Compatibility
- Windows
- macOS
- Linux
| Version | Published | Release Notes | Action |
|---|---|---|---|
| 1.7.0 | Added option to include a Deep Space Maneuver (DSM) |
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| 1.6.0 | Updated several algorithms, graphics displays and PDF documentation. |
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| 1.5.0 | Changed fmincon algorithm to interior-point. Updated several MATLAB functions and PDF documentation. |
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| 1.4.0 | Minor tweaks to the MATLAB source code, graphics updates and updated PDF user's guide. |
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| 1.3.0 | Bug fix for comet/asteroid bodies |
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| 1.2.0 | DE421 ephemeris |
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| 1.1.0 | Updated to use the DE440s JPL ephemeris and MICE routines |
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| 1.0.0 |
