File Exchange

Propagating Trajectories from the Earth to the Moon

版本 1.2.0.0 (17.6 MB) 作者： David Eagle
Integrate n-body trajectories from the Earth to the Moon. Includes non-spherical Earth gravity.
5.0
(2)

1.7K 次下载

更新时间 2022/1/20

查看许可证

PDF document and a MATLAB script called pprop_lunar that can be used to numerically integrate the geocentric orbital equations of motion of a trajectory from the Earth to the Moon. This scientific simulation begins at a user-defined epoch and geocentric state vector (position and velocity vectors) representing the point of trans-lunar injection (TLI) and ends at (1) closest approach to the Moon, (2) a user-defined Moon-centered (selenocentric) distance, or (3) at a user-defined final epoch.

引用格式

David Eagle (2023). Propagating Trajectories from the Earth to the Moon (https://www.mathworks.com/matlabcentral/fileexchange/43067-propagating-trajectories-from-the-earth-to-the-moon), MATLAB Central File Exchange. 检索来源 .

MATLAB 版本兼容性
创建方式 R2019b
兼容任何版本
平台兼容性
Windows macOS Linux

Community Treasure Hunt

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

Start Hunting!

版本 已发布 发行说明
1.2.0.0

Input in true-of-date coordinates. Updated to use JPL *.bsp ephemeris and MICE routines. PDF document updated.
1.1.0.0

Includes new option to model the effect of the Moon on the trajectory using non-spherical lunar gravity.
1.0.0.0