Parametric Analysis of Ballistic Earth-to-Mars Trajectories

Version 1.1.0 (16,1 Mo) par David Eagle
perform a parametric “sweep” of ballistic interplanetary trajectories from a user-defined Earth park orbit to encounter at Mars
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Mise à jour 3 août 2021

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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.

Citation pour cette source

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. Récupéré le .

Compatibilité avec les versions de MATLAB
Créé avec R2019b
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Version Publié le Notes de version
1.1.0

Updated script to use NAIF bsp ephemeris files available at https://naif.jpl.nasa.gov/naif/
1.0.0