中文版 | English
Title

Anti-unwinding terminal sliding mode attitude tracking control for rigid spacecraft

Author
Publication Years
2022-11-01
DOI
Source Title
ISSN
0005-1098
EISSN
1873-2836
Volume145
Abstract
In this paper, terminal sliding mode attitude tracking control without unwinding for rigid spacecraft is investigated. In order to guarantee the finite-time convergence of the system states and unwinding-free performance of the system on the sliding surface, a novel switching function is constructed by a hyperbolic sine function such that the obtained terminal sliding surface contains two equilibria. Then, a terminal attitude tracking control law is developed to ensure that the system states are driven to the sliding surface in a finite time. Moreover, a boundary layer is introduced to solve the chattering problem of the designed controller. The convergence of the system states within the boundary layer is guaranteed by imposing a constraint for the parameter of the developed switching function. Furthermore, the subsets of attraction domains of the two equilibria are given by designing a dynamic parameter for the proposed control law. The simulation results illustrate that the attitude tracking of rigid spacecraft without unwinding is realized by adopting the proposed attitude control law.
Keywords
URL[Source Record]
Indexed By
Language
English
SUSTech Authorship
Others
Funding Project
National Natural Science Foundation of China[62188101];National Natural Science Foundation of China[U2013203];
WOS Research Area
Automation & Control Systems ; Engineering
WOS Subject
Automation & Control Systems ; Engineering, Electrical & Electronic
WOS Accession No
WOS:000863176200013
Publisher
ESI Research Field
ENGINEERING
Scopus EID
2-s2.0-85137631946
Data Source
Scopus
Citation statistics
Cited Times [WOS]:0
Document TypeJournal Article
Identifierhttp://kc.sustech.edu.cn/handle/2SGJ60CL/401596
DepartmentSouthern University of Science and Technology
Affiliation
1.School of Mechanical Engineering and Automation,Harbin Institute of Technology (Shenzhen),Shenzhen,518055,China
2.Department of Precision Instrument,Tsinghua University,Beijing,100084,China
3.Center for Control Science and Technology,Southern University of Science and Technology,Shenzhen,518055,China
4.Center for Control Theory and Guidance Technology,Harbin Institute of Technology,Harbin,150001,China
5.School of Aeronautics and Astronautics,Sichuan University,Chengdu,610207,China
Recommended Citation
GB/T 7714
Dong,Rui Qi,Wu,Ai Guo,Zhang,Ying,et al. Anti-unwinding terminal sliding mode attitude tracking control for rigid spacecraft[J]. AUTOMATICA,2022,145.
APA
Dong,Rui Qi,Wu,Ai Guo,Zhang,Ying,Duan,Guang Ren,&Li,Bin.(2022).Anti-unwinding terminal sliding mode attitude tracking control for rigid spacecraft.AUTOMATICA,145.
MLA
Dong,Rui Qi,et al."Anti-unwinding terminal sliding mode attitude tracking control for rigid spacecraft".AUTOMATICA 145(2022).
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