Halo Orbit Design Using Differential Correction

Version 1.0.0 (8,76 ko) par David Eagle
Script for creating "re-fined" initial conditions for Halo orbits in the Earth-Moon circular-restricted, three-body problem.
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Mise à jour 21 fév. 2022

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This MATLAB demonstrates halo orbit design in the Earth-Moon system using differential correction (dc). The code is "hard-wired" with the astrodynamic constants for the Earth-Moon circular-restricted, three-body problem and a Class I halo orbit about the L2 libration point.
script features
(1) initial guess using Richardson's algorithm
(2) solve system of nonlinear equations using fsolve
(3) graphics display of dc-refined halo orbit
The only input required from the user is the desired z-amplitude of the halo orbit in kilometers.

Citation pour cette source

David Eagle (2024). Halo Orbit Design Using Differential Correction (https://www.mathworks.com/matlabcentral/fileexchange/107045-halo-orbit-design-using-differential-correction), MATLAB Central File Exchange. Extrait(e) le .

Compatibilité avec les versions de MATLAB
Créé avec R2019b
Compatible avec toutes les versions
Plateformes compatibles
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Version Publié le Notes de version
1.0.0