Gooding's State Vector-to-Orbital Elements Algorithm

版本 1.0.0.0 (4.3 KB) 作者: David Eagle
MATLAB demo script and function that implements Gooding's method.
5.0
(1)
827.0 次下载
更新时间 2014/11/27

查看许可证

A MATLAB implementation of R. H. Gooding's method for converting an ECI state vector to classical orbital elements. Valid for elliptical and hyperbolic orbits. Reference: R. H. Gooding, "On Universal Elements, and Conversion Procedures To and From Position and Velocity", Celestial Mechanics 44 (1988), 283-298

引用格式

David Eagle (2024). Gooding's State Vector-to-Orbital Elements Algorithm (https://www.mathworks.com/matlabcentral/fileexchange/48590-gooding-s-state-vector-to-orbital-elements-algorithm), MATLAB Central File Exchange. 检索来源 .

MATLAB 版本兼容性
创建方式 R2012b
兼容任何版本
平台兼容性
Windows macOS Linux
类别
在 Help Center 和 MATLAB Answers 中查找有关 Gravitation, Cosmology & Astrophysics 的更多信息
标签 添加标签

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
1.0.0.0