Trans-Lunar Trajectory Optimization - SNOPT/MICE versions
Version 1.2.0 (58,2 Mo) par
David Eagle
SNOPT version of the tlto_matlab script used to design preliminary lunar missions from Earth park orbit to B-plane encounter.
This submission is a MATLAB script named tlto_matlab that can be used to design preliminary lunar missions from Earth park orbit to B-plane encounter at the moon. The software assumes trans-lunar injection (TLI) occurs impulsively from a circular Earth park orbit. The B-plane coordinates used for targeting the final conditions at the moon are expressed in a moon-centered (selenocentric) mean equator and IAU node of epoch coordinate system. The results from this scientific simulation can be used as an initial guess for a finite-burn trajectory optimization program.
Citation pour cette source
David Eagle (2024). Trans-Lunar Trajectory Optimization - SNOPT/MICE versions (https://www.mathworks.com/matlabcentral/fileexchange/74321-trans-lunar-trajectory-optimization-snopt-mice-versions), MATLAB Central File Exchange. Récupéré le .
Compatibilité avec les versions de MATLAB
Créé avec
R2019b
Compatible avec toutes les versions
Plateformes compatibles
Windows macOS LinuxCatégories
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Version | Publié le | Notes de version | |
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1.2.0 | Distribution now includes a version (tlto_mice_snopt.zip) that uses JPL MICE routines to evaluate the de430.bsp ephemerides. |
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1.1.0 | Added node/apsis alignment targeting. Updated documentation. |
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1.0.0 |