文献详情
Robust adaptive relative position and attitude control for spacecraft autonomous proximity
文献类型期刊
作者Sun, Liang[1];Huo, Wei[2];Jiao, Zongxia[3]
机构
2016
期刊名称ISA TRANSACTIONS影响因子和分区
通讯作者Huo, W (reprint author), Beihang Univ, Sch Automat Sci & Elect Engn, Sci & Technol Aircraft Control Lab, Res Div 7, Xueyuan Rd 37, Beijing 100191, Peoples R China.
63
来源信息年:2016  卷:63  页码范围:11-19  
期刊信息ISA TRANSACTIONS影响因子和分区  ISSN:0019-0578
页码范围11-19
关键词Spacecraft control; Close proximity operations; Kinematic couplings; Thrust misalignment; Adaptive control; Robust control
增刊正刊
摘要This paper provides new results of the dynamical modeling and controller designing for autonomous close proximity phase during rendezvous and docking in the presence of kinematic couplings and model uncertainties. A globally defined relative motion mechanical model for close proximity operations is introduced firstly. Then, in spite of the kinematic couplings and thrust misalignment between relative rotation and relative translation, robust adaptive relative position and relative attitude controllers are designed successively. Finally, stability of the overall system is proved that the relative position and relative attitude are uniformly ultimately bounded, and the size of the ultimate bound can be regulated small enough by control system parameters. Performance of the controlled overall system is demonstrated via a representative numerical example. (C) 2016 ISA. Published by Elsevier Ltd. All rights reserved.
收录情况SCIE(WOS:000381164700002)  EI(20161202134167)  PubMed(26993103)  
所属部门自动化科学与电气工程学院
DOI10.1016/j.isatra.2016.02.022
学科自动化与控制系统;工程:综合;仪器仪表
百度学术Robust adaptive relative position and attitude control for spacecraft autonomous proximity
语言外文
ISSN0019-0578
被引频次3
人气指数29
浏览次数29
基金National Science Foundation of China [61134005, 61327807]; National Key Basic Research Program of China [2012CB821204]
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