Title | Anti-unwinding terminal sliding mode attitude tracking control for rigid spacecraft |
Author | |
Publication Years | 2022-11-01
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DOI | |
Source Title | |
ISSN | 0005-1098
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EISSN | 1873-2836
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Volume | 145 |
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
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SUSTech Authorship | Others
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Funding Project | National Natural Science Foundation of China[62188101];National Natural Science Foundation of China[U2013203];
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WOS Research Area | Automation & Control Systems
; Engineering
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WOS Subject | Automation & Control Systems
; Engineering, Electrical & Electronic
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WOS Accession No | WOS:000863176200013
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Publisher | |
ESI Research Field | ENGINEERING
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Scopus EID | 2-s2.0-85137631946
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Data Source | Scopus
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Citation statistics |
Cited Times [WOS]:3
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Document Type | Journal Article |
Identifier | http://kc.sustech.edu.cn/handle/2SGJ60CL/401596 |
Department | Southern 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.
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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.
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MLA |
Dong,Rui Qi,et al."Anti-unwinding terminal sliding mode attitude tracking control for rigid spacecraft".AUTOMATICA 145(2022).
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