Halo Orbit Design Using Differential Correction

Versión 1.0.0 (8,76 KB) por David Eagle
Script for creating "re-fined" initial conditions for Halo orbits in the Earth-Moon circular-restricted, three-body problem.
4.0
(1)
435 Descargas
Actualizado 21 feb 2022

Ver licencia

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.

Citar como

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. Recuperado .

Compatibilidad con la versión de MATLAB
Se creó con R2019b
Compatible con cualquier versión
Compatibilidad con las plataformas
Windows macOS Linux

Community Treasure Hunt

Find the treasures in MATLAB Central and discover how the community can help you!

Start Hunting!

Versión Publicado Notas de la versión
1.0.0