Equations of Satellite Relative Motion in Low Earth Orbit under Lunar Perturbation

被引：0
|
作者：
Xu, Guangyan [1 ]
Luo, Jianfu [1 ]
Li, Zheng [1 ]
Chen, Xia [1 ]
机构：
[1] Shenyang Aerosp Univ, Sch Automat, Shenyang 110136, Peoples R China
来源：
2014 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2014年
关键词：
Satellite Relative Motion; Third-body Perturbation; Reference Satellite Variable;
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
Aimed at the low earth satellites under lunar perturbation, this paper derived two sets of dynamic equations based on the Reference Satellite Variable (RSV). One is for orbital motion of the reference satellite and another one is for relative motion between satellites. Both sets of equations are simple and accurate and expressed explicitly. Because of clear physical meaning of the selected Reference Satellite Variables, the equations are also suitable to analyze the effect of satellite motion under lunar perturbation qualitatively.
引用
收藏
页码：2204 / 2209
页数：6
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