| 题名 | Anti-unwinding attitude maneuver control with predefined time for rigid spacecraft with input saturation |
| 作者 | |
| 通讯作者 | Wu, Ai-Guo |
| 发表日期 | 2024-06-01
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| DOI | |
| 发表期刊 | |
| ISSN | 1049-8923
|
| EISSN | 1099-1239
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| 摘要 | In this article, anti-unwinding sliding mode attitude maneuver control with predefined time is investigated for rigid spacecraft with input saturation. First, a nonsingular sliding function containing two equilibrium points is designed to ensure the predefined-time convergence of system states and unwinding-free performance of the closed-loop system on the sliding phase. Then, an auxiliary system with a dynamic parameter is presented to compensate the impact of input saturation. With this parameter, the auxiliary system can handle input saturation that occurs. Based on the sliding function and the auxiliary system, an attitude maneuver controller is developed to guarantee the robustness of the closed-loop system to bounded external disturbance. Under the designed controller, the states of the closed-loop system are driven into a neighborhood of the sliding surface within a predefined time. Moreover, the unwinding phenomenon is also avoided on the reaching phase. Numerical simulation results illustrate the unwinding-free performance and predefined-time convergence of the closed-loop system under the proposed control strategy. |
| 关键词 | |
| 相关链接 | [来源记录] |
| 收录类别 | |
| 语种 | 英语
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| 学校署名 | 通讯
|
| 资助项目 | Joint Funds of the National Natural Science Foundation of China[2024B1515040008]
; Preeminent Youth Team Project of Guangdong Basic and Applied Basic Research Foundation[U2013203]
; National Natural Science Foundation of China["KQTD20210811090146075","RCJC20210609104400005"]
; Shenzhen Science and Technology Program[2023B1212010005]
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| WOS研究方向 | Automation & Control Systems
; Engineering
; Mathematics
|
| WOS类目 | Automation & Control Systems
; Engineering, Electrical & Electronic
; Mathematics, Applied
|
| WOS记录号 | WOS:001241330600001
|
| 出版者 | |
| ESI学科分类 | ENGINEERING
|
| 来源库 | Web of Science
|
| 引用统计 | |
| 成果类型 | 期刊论文 |
| 条目标识符 | http://sustech.caswiz.com/handle/2SGJ60CL/788140 |
| 专题 | 工学院_系统设计与智能制造学院 |
| 作者单位 | 1.Harbin Inst Technol Shenzhen, Guangdong Prov Key Lab Intelligent Morphing Mech &, Shenzhen, Peoples R China 2.Harbin Inst Technol Shenzhen, Dept Automat, Shenzhen 518055, Peoples R China 3.Southern Univ Sci & Technol, Sch Syst Design & Intelligent Mfg, Shenzhen, Peoples R China 4.Tsinghua Univ, Dept Precis Instrument, Beijing, Peoples R China |
| 通讯作者单位 | 系统设计与智能制造学院 |
| 推荐引用方式 GB/T 7714 |
Xu, Yu-Tian,Wu, Ai-Guo,Dong, Rui-Qi. Anti-unwinding attitude maneuver control with predefined time for rigid spacecraft with input saturation[J]. INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL,2024.
|
| APA |
Xu, Yu-Tian,Wu, Ai-Guo,&Dong, Rui-Qi.(2024).Anti-unwinding attitude maneuver control with predefined time for rigid spacecraft with input saturation.INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL.
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| MLA |
Xu, Yu-Tian,et al."Anti-unwinding attitude maneuver control with predefined time for rigid spacecraft with input saturation".INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL (2024).
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| 条目包含的文件 | 条目无相关文件。 | |||||
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