Halo Orbit Design Using Differential Correction

版本 1.0.0 (8.8 KB) 作者: 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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更新时间 2022/2/21

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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.

引用格式

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. 检索来源 .

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创建方式 R2019b
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版本 已发布 发行说明
1.0.0