A MATLAB script for Earth-to-Mars Mission Design - OTB

Versión 1.3.0 (16,1 MB) por David Eagle
Optimization Toolbox version of the e2m_matlab script that performs Earth-to-Mars mission analysis and design.
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PDF document and a MATLAB script named e2m_matlab_otb.m that can be used to design and optimize end-to-end 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.

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David Eagle (2024). A MATLAB script for Earth-to-Mars Mission Design - OTB (https://www.mathworks.com/matlabcentral/fileexchange/73646-a-matlab-script-for-earth-to-mars-mission-design-otb), MATLAB Central File Exchange. Recuperado .

Compatibilidad con la versión de MATLAB
Se creó con R2019b
Compatible con cualquier versión
Compatibilidad con las plataformas
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Versión Publicado Notas de la versión
1.3.0

Updated script to use the *.bsp ephemeris files. Minor updates to the source code.
1.2.0

Added trajectory verification calculations and updated documentation
1.1.0

Added node/apse targeting. Added additional examples. Updated PDF document.
1.0.1

added "verify optimal solution" calculations
1.0.0