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
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.
2016
期刊名称ISA TRANSACTIONS影响因子和分区
来源信息年:2016  卷:63  页码范围:11-19  
63
期刊信息ISA TRANSACTIONS影响因子和分区  ISSN:0019-0578
关键词Spacecraft control; Close proximity operations; Kinematic couplings; Thrust misalignment; Adaptive control; Robust control
页码范围11-19
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
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33
人气指数32
浏览次数32
基金National Science Foundation of China [61134005, 61327807]; National Key Basic Research Program of China [2012CB821204]
全部评论(0 条评论)
作者其他论文

Singularity-free backstepping controller for model helicopters.

Zou, Yao;Huo, Wei.ISA TRANSACTIONS.2016,65,133-142.

Research on Aircraft Attack Angle Control Considering Servo-Loop Dynamics.

Liu, Xiaodong;Wang, Yan;Huang, Wanwei,等.INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING.2015.

Adaptive Trajectory Linearization Control for a model-scaled helicopter with uncertain inertial parameters.

Zhu, Bing;Huo, Wei.31st Chinese Control Conference, CCC 2012.2012,4389-4395.

Compensation control for the supply pressure fluctuation in electro-hydraulic load simulator.

Han, Songshan;Jiao, Zongxia;Shang, Yaoxing,等.2011 International Conference on Fluid Power and Mechatronics, FPM 2011.2011,914-919.

The application of multipoint rotate-vector optimization method on the On-line Identification based Optimal Control (OIOC.

Zhang, Boya;Jiao, Zongxia;Kang, Rongjie,等.2011 International Conference on Fluid Power and Mechatronics, FPM 2011.2011,926-929.

登录