Earth-to-Mars Interplanetary TCM Optimization - SNOPT

Versión 1.1.0.0 (15,6 MB) por David Eagle
Optimization of interplanetary trajectory correction maneuvers (TCM) during Earth-to-Mars spaceflight.
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Actualizado 28 ene 2022

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PDF document and a MATLAB script called e2m_tcm_snopt 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.

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David Eagle (2024). Earth-to-Mars Interplanetary TCM Optimization - SNOPT (https://www.mathworks.com/matlabcentral/fileexchange/48690-earth-to-mars-interplanetary-tcm-optimization-snopt), MATLAB Central File Exchange. Recuperado .

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Se creó con R2019b
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Versión Publicado Notas de la versión
1.1.0.0

Updated to use JPL DE421.bsp ephemeris (included in zip file) and MICE routines.
1.0.0.0