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作 者:Luo Yazhong Zhang Jin Tang Guojin
机构地区:[1]College of Aerospace Science and Technology,National University of Defense Technology
出 处:《Chinese Journal of Aeronautics》2014年第1期1-11,共11页中国航空学报(英文版)
基 金:co-supported by the National Natural Science Foundation of China (Nos.10902121 and 11222215);National Basic Research Program of China (No.2013CB733100);the Foundation for the Author of National Excellent Doctoral Dissertation of China (No.201171)
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 rendez- vous, 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.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 rendez- vous, 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.
关 键 词:Automated control Relative dynamics equationRelative navigation Space rendezvous SURVEY Trajectory optimization
分 类 号:V412.41[航空宇航科学与技术—航空宇航推进理论与工程] V448.234
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