中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Conditional disturbance negation based active disturbance rejection control for hypersonic vehicles

文献类型:期刊论文

作者Sun, Jinlin; Pu, Zhiqiang1; Yi, Jianqiang
刊名CONTROL ENGINEERING PRACTICE
出版日期2019-03-01
卷号84页码:159-171
关键词Active disturbance rejection control Conditional disturbance negation Disturbance characterization indicator Hypersonic vehicle
ISSN号0967-0661
DOI10.1016/j.conengprac.2018.11.016
通讯作者Pu, Zhiqiang(zhiqiang.pu@ia.ac.cn)
英文摘要This paper presents a conditional disturbance negation (CDN) based active disturbance rejection control (ADRC) scheme for the velocity and altitude tracking control of flexible air-breathing hypersonic vehicles (FAHVs) in the presence of various uncertainties and disturbances. A pioneering CDN module is proposed to selectively compensate the total disturbances according to the characteristics of the total disturbances and the FAHV dynamics, which is aimed at canceling some detrimental disturbances while profiting from other beneficial disturbances. Firstly, model-based extended state observers are applied to estimate the total disturbances in FAHVs in an efficient way. Based on the Lyapunov theory and the estimated disturbances, a novel disturbance characterization indicator (DCI) is then designed to show whether the total disturbance harms or benefits the tracking performance in engineering practice. Then, DCI is utilized to construct the CDN module. In consequence, the CDN based FAHV tracking control is implemented in an ADRC framework, yielding the CDN based ADRC scheme. The stability analysis is conducted to show the convergence of the closed-loop system. Finally, the effectiveness and superiority of the proposed control scheme are validated by some representative simulations in various flight conditions.
WOS关键词EXTENDED STATE OBSERVER ; SLIDING MODE CONTROLLER ; OUTPUT-FEEDBACK CONTROL ; FINITE-TIME CONTROL ; CONTROL DESIGN ; ROBUST-CONTROL ; NONLINEAR-SYSTEMS ; ADAPTIVE-CONTROL ; FLIGHT CONTROL ; UNCERTAINTY
资助项目National Natural Science Foundation of China[61603383] ; National Natural Science Foundation of China[61421004] ; 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
语种英语
WOS记录号WOS:000460495700014
出版者PERGAMON-ELSEVIER SCIENCE LTD
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/173211/24962]  
专题综合信息系统研究中心_飞行器智能技术
通讯作者Pu, Zhiqiang
作者单位1.Chinese Acad Sci, Inst Automat, Beijing 100190, Peoples R China
2.Univ Chinese Acad Sci, Beijing 100049, Peoples R China
推荐引用方式
GB/T 7714
Sun, Jinlin,Pu, Zhiqiang,Yi, Jianqiang. Conditional disturbance negation based active disturbance rejection control for hypersonic vehicles[J]. CONTROL ENGINEERING PRACTICE,2019,84:159-171.
APA Sun, Jinlin,Pu, Zhiqiang,&Yi, Jianqiang.(2019).Conditional disturbance negation based active disturbance rejection control for hypersonic vehicles.CONTROL ENGINEERING PRACTICE,84,159-171.
MLA Sun, Jinlin,et al."Conditional disturbance negation based active disturbance rejection control for hypersonic vehicles".CONTROL ENGINEERING PRACTICE 84(2019):159-171.

入库方式: OAI收割

来源:自动化研究所

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