A MATLAB script for Earth-to-Mars Mission Design - SNOPT
Versión 1.2.0 (16,1 MB) por
David Eagle
Design and optimize end-to-end Earth-to-Mars ballistic trajectories from Earth park orbit to Mars B-plane encounter.
PDF document and a MATLAB script named e2m_matlab_snopt.m that can be used to design and optimize ballistic interplanetary missions from Earth park orbit to encounter at Mars. The software assumes that interplanetary injection occurs impulsively from a circular Earth park orbit. The B-plane coordinates are expressed in a Mars-centered (areocentric) mean equator and IAU node of epoch coordinate system. B-plane targets are enforced using either a combination of periapsis radius and orbital inclination, individual B-plane coordinates of the arrival hyperbola, or entry interface (EI) conditions at Mars. The type of targeting and the target values are defined by the user.
Citar como
David Eagle (2024). A MATLAB script for Earth-to-Mars Mission Design - SNOPT (https://www.mathworks.com/matlabcentral/fileexchange/74671-a-matlab-script-for-earth-to-mars-mission-design-snopt), MATLAB Central File Exchange. Recuperado .
Compatibilidad con la versión de MATLAB
Se creó con
R2019b
Compatible con cualquier versión
Compatibilidad con las plataformas
Windows macOS LinuxCategorías
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