Parametric Analysis of Ballistic Earth-to-Mars Trajectories
Versión 1.1.0 (16,1 MB) por
David Eagle
perform a parametric “sweep” of ballistic interplanetary trajectories from a user-defined Earth park orbit to encounter at Mars
PDF user's manual and MATLAB script named e2m_sweep that can be used to perform a parametric “sweep” of ballistic interplanetary trajectories from a user-defined Earth park orbit to encounter at Mars. The user defines the initial departure calendar date, the sweep duration and the step size to use during the analysis. The software assumes that interplanetary injection occurs impulsively from a circular Earth park orbit. The software also assumes the arrival date of each sweep trajectory is fixed to the value provided by the user. The user can also select either the ascending or descending hyperbolic injection for the sweep.
Citar como
David Eagle (2024). Parametric Analysis of Ballistic Earth-to-Mars Trajectories (https://www.mathworks.com/matlabcentral/fileexchange/74254-parametric-analysis-of-ballistic-earth-to-mars-trajectories), 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
- Aerospace > Aerospace Blockset > Visualization >
- Sciences > Earth, Ocean, and Atmospheric Sciences > Earth and Planetary Science >
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Versión | Publicado | Notas de la versión | |
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1.1.0 | Updated script to use NAIF bsp ephemeris files available at https://naif.jpl.nasa.gov/naif/ |
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1.0.0 |