南方科技大学知识苑(SUSTech KC): Anti-Unwinding Sliding Mode Control for Rigid Spacecraft Based on Modified Rodrigues Parameters

题名	Anti-Unwinding Sliding Mode Control for Rigid Spacecraft Based on Modified Rodrigues Parameters
作者	Dong，Rui Qi 1; Wu，Ai Guo 1; Zhang，Ying 1; Duan，Guang Ren2 ; Huang，Jing 3
发表日期	2022
DOI	10.1109/TAES.2022.3218277
发表期刊	IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS 影响因子和分区
ISSN	0018-9251
EISSN	1557-9603
卷号	PP 期号:99页码:1-13
摘要	In this paper, attitude maneuver control without unwinding phenomenon is investigated for rigid spacecraft via modified Rodrigues parameters. A novel switching function is constructed by a hyperbolic sine function to guarantee that the sliding surface contains two stable equilibria. A sliding mode controller is developed to ensure that the sliding surface is reachable. Moreover, a dynamic parameter is designed to guarantee unwinding-free performance of the closed-loop system when the system states outside the sliding surface. In addition, a boundary layer is introduced to deal with the chattering problem. Further, the unwinding-free performance within the boundary layer is guaranteed by imposing some conditions on the parameters of the switching function. Finally, comparison simulations are performed to verify the effectiveness and superiority of the presented control law.
关键词	Aerodynamics Angular velocity Anti-unwinding Attitude control Materials requirements planning Modified Rodrigues parameters Rigid spacecraft Sliding mode control Space vehicles Switches
相关链接	[Scopus记录]
收录类别	EI ; SCI
语种	英语
学校署名	其他
资助项目	Joint Funds of the National Natural Science Foundation of China["62203255","U2013203"] ; Shenzhen Science and Technology Program["RCJC20210609104400005","62188101","SAST2018-088"] ; Science Center Program of National Natural Science Foundation of China[JCYJ20210324132413034] ; Shanghai Aerospace Science and Technology Innovation Foundation[61803258] ; National Natural Science Foundation of China[20QA1404400] ; null[KQTD20210811090146075]
WOS研究方向	Engineering ; Telecommunications
WOS类目	Engineering, Aerospace ; Engineering, Electrical & Electronic ; Telecommunications
WOS记录号	WOS:001006747500033
出版者	IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
EI入藏号	20224613110237
EI主题词	Backstepping ; Boolean functions ; Boundary layers ; Closed loop systems ; Hyperbolic functions ; Rotation ; Sliding mode control ; Switching functions
EI分类号	Computer Theory, Includes Formal Logic, Automata Theory, Switching Theory, Programming Theory:721.1 ; Control Systems:731.1 ; Specific Variables Control:731.3 ; Mathematics:921 ; Algebra:921.1 ; Mechanics:931.1 ; Systems Science:961
ESI学科分类	ENGINEERING
Scopus记录号	2-s2.0-85141625238
来源库	Scopus
全文链接	https://ieeexplore.ieee.org/stamp/stamp.jsp?tp=&arnumber=9933626
引用统计	被引频次[WOS]：2
成果类型	期刊论文
条目标识符	http://sustech.caswiz.com/handle/2SGJ60CL/411887
专题	工学院_系统设计与智能制造学院
作者单位	1.School of Mechanical Engineering and Automation, Harbin Institute of Technology (Shenzhen), Shenzhen, P. R. China 2.Center for Control Science and Technology, Southern University of Science and Technology, Shenzhen, P. R. China 3.Shanghai Aerospace Control Technology Institute, Shanghai, China
推荐引用方式 GB/T 7714	Dong，Rui Qi,Wu，Ai Guo,Zhang，Ying,et al. Anti-Unwinding Sliding Mode Control for Rigid Spacecraft Based on Modified Rodrigues Parameters[J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS,2022,PP(99):1-13.
APA	Dong，Rui Qi,Wu，Ai Guo,Zhang，Ying,Duan，Guang Ren,&Huang，Jing.(2022).Anti-Unwinding Sliding Mode Control for Rigid Spacecraft Based on Modified Rodrigues Parameters.IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS,PP(99),1-13.
MLA	Dong，Rui Qi,et al."Anti-Unwinding Sliding Mode Control for Rigid Spacecraft Based on Modified Rodrigues Parameters".IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS PP.99(2022):1-13.