Ballistic Interplanetary Trajectory Optimization - SNOPT
Citation pour cette source
David Eagle (2024). Ballistic Interplanetary Trajectory Optimization - SNOPT (https://www.mathworks.com/matlabcentral/fileexchange/39446-ballistic-interplanetary-trajectory-optimization-snopt), MATLAB Central File Exchange. Récupéré le .
Compatibilité avec les versions de MATLAB
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- Sciences > Physics > Gravitation, Cosmology & Astrophysics >
- Sciences > Earth, Ocean, and Atmospheric Sciences > Earth and Planetary Science >
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Version | Publié le | Notes de version | |
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1.9.0.0 | Modified to use MICE routines and companion JPL DE421.bsp ephemeris |
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1.8.0.0 | Fixed two bugs related to the mission constraints script option. Updated the PDF user's manual for this option. Verified that the script works with the March 2015 version of SNOPT. |
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1.7.0.0 | Updated to use the September 2014, 64 bit version of SNOPT. |
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1.6.0.0 | Added version of main script (ipto_matlab_64bit.m) that uses the March 17, 2014 version of SNOPT. |
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1.5.0.0 | Added additional features to the heliocentric graphic display. Updated PDF document with additional script example. |
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1.4.0.0 | Updated version includes the option to enforce user-defined mission constraints during the trajectory optimization. PDF document updated to reflect this change. |
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1.3.0.0 | MICE version included in ipto_matlab_mice.zip archive. |
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1.2.0.0 | Minor script changes (ecliptic-to-equatorial transformation, etc.) along with updates to PDF document. |
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1.0.0.0 |