NSSC OpenIR  > 空间技术部
Alternative TitleAnalytical Solutions for Satellite Relative Motion under J_2 Perturbation
周敬; 郑建华; 李明涛
Source Publication航天控制
Keyword相对运动 Cw方程 J_2摄动 解析方程
Other AbstractSatellite's orbital elements can contain secular and periodic components under the J_2 perturbation which results in that the relative motion dynamics model become transcendental equations and the analytical solutions can not be obtained through conventional methods. Under this circumstances,the distance can be averaged among the satellite,the earth center and the orbit inclination so that the relative motion dynamics model can be solved and the analytical relative motion equations can be obtained under J_2 perturbation force when the reference orbit is circular or elliptical with very small eccentricity. Simulations results show that the precision of relative motion can be improved greatly by comparing with CW equations. It demonstrates the effectiveness and veracity of the new method.
Indexed ByCSCD
Citation statistics
Document Type期刊论文
Recommended Citation
GB/T 7714
周敬,郑建华,李明涛. J_2摄动下卫星相对运动解析方程研究[J]. 航天控制,2017,35(2):44-50.
APA 周敬,郑建华,&李明涛.(2017).J_2摄动下卫星相对运动解析方程研究.航天控制,35(2),44-50.
MLA 周敬,et al."J_2摄动下卫星相对运动解析方程研究".航天控制 35.2(2017):44-50.
Files in This Item:
File Name/Size DocType Version Access License
201735244-50.pdf(386KB)期刊论文作者接受稿开放获取CC BY-NC-SAApplication Full Text
Related Services
Recommend this item
Usage statistics
Export to Endnote
Google Scholar
Similar articles in Google Scholar
[周敬]'s Articles
[郑建华]'s Articles
[李明涛]'s Articles
Baidu academic
Similar articles in Baidu academic
[周敬]'s Articles
[郑建华]'s Articles
[李明涛]'s Articles
Bing Scholar
Similar articles in Bing Scholar
[周敬]'s Articles
[郑建华]'s Articles
[李明涛]'s Articles
Terms of Use
No data!
Social Bookmark/Share
All comments (0)
No comment.

Items in the repository are protected by copyright, with all rights reserved, unless otherwise indicated.