中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Augmented fixed-time observer-based continuous robust control for hypersonic vehicles with measurement noises

文献类型:期刊论文

作者Sun, Jinlin1,2; Yi, Jianqiang1,2; Pu, Zhiqiang1,2
刊名IET CONTROL THEORY AND APPLICATIONS
出版日期2019-02-12
卷号13期号:3页码:422-433
关键词linearisation techniques observers control system synthesis vehicle dynamics adaptive control aircraft control uncertain systems robust control variable structure systems space vehicles augmented fixed-time observer measurement noises cruise control flexible air-breathing hypersonic vehicles controller gains finite-time convergence fixed convergence time FAHV gain adaptation law continuous robust control input-output linearisation technique
ISSN号1751-8644
DOI10.1049/iet-cta.2018.5823
通讯作者Yi, Jianqiang(jianqiang.yi@ia.ac.cn)
英文摘要This study is concerned with the augmented fixed-time observer based adaptive super-twisting cruise control for flexible air-breathing hypersonic vehicles (FAHVs). First, the input-output linearisation technique is employed to derive a control oriented FAHV dynamic model. Then, a super-twisting controller is designed to track the reference velocity and altitude commands when faced with various uncertainties and disturbances. In addition, a novel gain adaptation law is constructed as a supplement of the super-twisting controller to avoid overestimating the values of controller gains. The adaptation law keeps the controller gains adapting dynamically to guarantee the finite-time convergence of sliding variables in the presence of disturbances with unknown boundaries. Moreover, augmented fixed-time observers are designed to estimate the true values of measured states and filter out high-frequency sensor noises. Thus, the fixed convergence time of these observers is achieved independently of initial estimation errors. Finally, the augmented fixed-time observers and adaptive super-twisting controller are combined together to ensure the superior tracking performances of FAHVs under the effects of uncertainties, disturbances, and measurement noises.
WOS关键词SLIDING-MODE CONTROL ; BACK-STEPPING CONTROL ; ADAPTIVE-CONTROL ; CONTROL DESIGN ; NONLINEAR CONTROL ; DIFFERENTIATION ; SYSTEMS
资助项目National Natural Science Foundation of China[61421004] ; National Natural Science Foundation of China[61603383] ; National Natural Science Foundation of China[61603384] ; Beijing Advanced Innovation Center of Intelligent Robots and Systems[2016IRS23]
WOS研究方向Automation & Control Systems ; Engineering ; Instruments & Instrumentation
语种英语
WOS记录号WOS:000458252500013
出版者INST ENGINEERING TECHNOLOGY-IET
资助机构National Natural Science Foundation of China ; Beijing Advanced Innovation Center of Intelligent Robots and Systems
源URL[http://ir.ia.ac.cn/handle/173211/25301]  
专题综合信息系统研究中心_飞行器智能技术
通讯作者Yi, Jianqiang
作者单位1.Chinese Acad Sci, Inst Automat, Beijing 100190, Peoples R China
2.Univ Chinese Acad Sci, Sch Artif Intelligence, Beijing 100049, Peoples R China
推荐引用方式
GB/T 7714
Sun, Jinlin,Yi, Jianqiang,Pu, Zhiqiang. Augmented fixed-time observer-based continuous robust control for hypersonic vehicles with measurement noises[J]. IET CONTROL THEORY AND APPLICATIONS,2019,13(3):422-433.
APA Sun, Jinlin,Yi, Jianqiang,&Pu, Zhiqiang.(2019).Augmented fixed-time observer-based continuous robust control for hypersonic vehicles with measurement noises.IET CONTROL THEORY AND APPLICATIONS,13(3),422-433.
MLA Sun, Jinlin,et al."Augmented fixed-time observer-based continuous robust control for hypersonic vehicles with measurement noises".IET CONTROL THEORY AND APPLICATIONS 13.3(2019):422-433.

入库方式: OAI收割

来源:自动化研究所

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