Halo Orbit Design Using Differential Correction
Script for creating "re-fined" initial conditions for Halo orbits in the Earth-Moon circular-restricted, three-body problem.
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.
引用格式
David Eagle (2026). Halo Orbit Design Using Differential Correction (https://ww2.mathworks.cn/matlabcentral/fileexchange/107045-halo-orbit-design-using-differential-correction), MATLAB Central File Exchange. 检索时间: .
| 版本 | 已发布 | 发行说明 | Action |
|---|---|---|---|
| 1.0.0 |
