Survey of orbital dynamics and control of space rendezvous

被引：89
作者：
Luo Yazhong [1 ]
Zhang Jin [1 ]
Tang Guojin [1 ]
机构：
[1] Natl Univ Def Technol, Coll Aerosp Sci & Technol, Changsha 410073, Hunan, Peoples R China
来源：
CHINESE JOURNAL OF AERONAUTICS | 2014年 / 27卷 / 01期
基金：
中国国家自然科学基金;
关键词：
Automated control; Relative dynamics equation; Relative navigation; Space rendezvous; Survey; Trajectory optimization; STATE TRANSITION MATRIX; RELATIVE-MOTION; TRAJECTORY OPTIMIZATION; MULTIPLE-REVOLUTION; SUFFICIENT CONDITIONS; PRIMER VECTOR; SATELLITE; IMPULSE; DOCKING; NAVIGATION;
D O I：
10.1016/j.cja.2013.07.042
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Rendezvous orbital dynamics and control (RODC) is a key technology for operating space rendezvous and docking missions. This paper surveys the studies on RODC. Firstly, the basic relative dynamics equation set is introduced and its improved versions are evaluated. Secondly, studies on rendezvous trajectory optimization are commented from three aspects: the linear rendezvous, the nonlinear two-body rendezvous, and the perturbed and constrained rendezvous. Thirdly, studies on relative navigation are briefly reviewed, and then close-range control methods including automated control, manual control, and telecontrol are analyzed. Fourthly, advances in rendezvous trajectory safety and robust analysis are surveyed, and their applications in trajectory optimization are discussed. Finally, conclusions are drawn and prospects of studies on RODC are presented. (C) 2014 Production and hosting by Elsevier Ltd. on behalf of CSAA & BUAA.
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页码：1 / 11
页数：11
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