Survey of orbital dynamics and control of space rendezvous
Survey of orbital dynamics and control of space rendezvous
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DOI：
10.1016/j.cja.2013.07.042
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发表时间：
2014-02-01
影响因子：
5.7
通讯作者：
Tang Guojin
中科院分区：
文献类型：
--
作者：
Luo Yazhong;Zhang Jin;Tang Guojin
交会对接轨道动力学与控制（RODC）是实现空间交会对接任务的关键技术。本文综述了RODC的研究进展。首先介绍了相对动力学基本方程组，并对其改进形式进行了评价。其次，从线性交会、非线性两体交会、摄动约束交会三个方面对交会轨道优化的研究进行了评述。第三，简要回顾了相对导航的研究现状，分析了近距离控制的方法，包括自动控制、手动控制和遥控控制。第四，综述了交会轨道安全性和鲁棒性分析的研究进展，并讨论了它们在轨道优化中的应用。最后，对本文的研究工作进行了总结，并对RODC的研究前景进行了展望。(C)2014由爱思唯尔有限公司代表CSAA和北航制作和主办。
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.