Earth-to-Mars Interplanetary TCM Optimization - SNOPT
Version 184.108.40.206 (15.6 MB) by David Eagle
Optimization of interplanetary trajectory correction maneuvers (TCM) during Earth-to-Mars spaceflight.
Updated 28 Jan 2022
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.
David Eagle (2023). 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. Retrieved .
MATLAB Release Compatibility
Created with R2019b
Compatible with any release
Platform CompatibilityWindows macOS Linux
- Aerospace > Aerospace Blockset > Visualization >
- Sciences > Earth, Ocean, and Atmospheric Sciences > Earth and Planetary Science >
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