COMBINED STATION KEEPING OF INCLINATION AND LONGITUDE FOR GEOSTATIONARY SATELLITE WITH ELECTRIC PROPULSION SYSTEM

被引：0
|
作者：
Li, Lincheng [1 ]
Zhang, Jingrui [1 ]
Zhao, Shuge [2 ,3 ]
机构：
[1] Beijing Inst Technol, Sch Aerosp Engn, Zhongguancun South St 5, Beijing 100081, Peoples R China
[2] China Aerosp Sci & Ind Corp, Beijing Inst Elect Syst Engn, Yongdian Rd 52, Beijing 100854, Peoples R China
[3] China Aerosp Sci & Ind Corp, Inst Space Syst Engn, Yongdian Rd 52, Beijing 100854, Peoples R China
来源：
FOURTH IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2018, PTS I-III | 2018年 / 165卷
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Station keeping is a prerequisite for the on-orbit service of geostationary satellites. It can restrain the drift caused by high-orbit perturbations effectively and increase the on-orbit stability. Using electric propulsion to achieve station keeping has the advantage of reduction in the fuel consumption. This paper is to develop a station keeping strategy to solve the combined control for inclination and longitude. High-precision equation of motion described by mean orbital elements is proposed in the first part. Then the fuel-optimal control is applied to indicate the relation among switching time of four thrusters. Thus, the equation between variation of orbital elements and speed increment can be analytically solved. Finally, numerical results are presented to evaluate this technique.
引用
收藏
页码：413 / 426
页数：14
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