南方科技大学知识苑(SUSTech KC): Fully Actuated System Approach for 6DOF Spacecraft Control Based on Extended State Observer

题名	Fully Actuated System Approach for 6DOF Spacecraft Control Based on Extended State Observer
作者	Zhao Qin1 ; Duan Guang-Ren1,2
通讯作者	Zhao Qin
发表日期	2022-04-01
DOI	10.1007/s11424-022-1498-5
发表期刊	Journal of Systems Science & Complexity 影响因子和分区
ISSN	1009-6124
EISSN	1559-7067
卷号	35 期号:2页码:604-622
摘要	This paper deals with the problem of position and attitude tracking control for a rigid spacecraft. A fully actuated system (FAS) model for the six degree-of-freedom (6DOF) spacecraft motion is derived first from the state-space model by variable elimination. Considering the uncertainties from external disturbance, unknown motion information, and uncertain inertia properties, an extended state observer (ESO) is designed to estimate the total disturbance. Then, a tracking controller based on FAS approach is designed, and this makes the closed-loop system a constant linear one with an arbitrarily assignable eigenstructure. The solution to the parameter matrices of the observer and controller is given subsequently. It is proved via the Lyapunov stability theory that the observer errors and tracking errors both converge into the neighborhood of the origin. Finally, numerical simulation demonstrates the effectiveness of the proposed controller.
关键词	Constant linear closed-loop system extended state observer fully actuated system approach relative position and attitude control
相关链接	[来源记录]
收录类别	SCI ; EI
语种	英语
学校署名	第一 ; 通讯
资助项目	Science Center Program of the National Natural Science Foundation of China[62188101] ; Major Program of the National Natural Science Foundation of China[61690210,61690212] ; National Natural Science Foundation of China[62103164,61703437]
WOS研究方向	Mathematics
WOS类目	Mathematics, Interdisciplinary Applications
WOS记录号	WOS:000786419800012
出版者	SPRINGER HEIDELBERG
EI入藏号	20221611982621
EI主题词	Attitude control ; Closed loop control systems ; Controllers ; Degrees of freedom (mechanics) ; Navigation ; State estimation ; Uncertainty analysis
EI分类号	Control Systems:731.1 ; Specific Variables Control:731.3 ; Control Equipment:732.1 ; Mathematics:921 ; Probability Theory:922.1 ; Mechanics:931.1 ; Systems Science:961
来源库	Web of Science
引用统计	被引频次[WOS]：21
成果类型	期刊论文
条目标识符	http://sustech.caswiz.com/handle/2SGJ60CL/333466
专题	南方科技大学
作者单位	1.Southern Univ Sci & Technol, Ctr Control Sci & Technol, Shenzhen 518055, Peoples R China 2.Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Harbin 150001, Peoples R China
第一作者单位	南方科技大学
通讯作者单位	南方科技大学
第一作者的第一单位	南方科技大学
推荐引用方式 GB/T 7714	Zhao Qin,Duan Guang-Ren. Fully Actuated System Approach for 6DOF Spacecraft Control Based on Extended State Observer[J]. Journal of Systems Science & Complexity,2022,35(2):604-622.
APA	Zhao Qin,&Duan Guang-Ren.(2022).Fully Actuated System Approach for 6DOF Spacecraft Control Based on Extended State Observer.Journal of Systems Science & Complexity,35(2),604-622.
MLA	Zhao Qin,et al."Fully Actuated System Approach for 6DOF Spacecraft Control Based on Extended State Observer".Journal of Systems Science & Complexity 35.2(2022):604-622.