中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Appointed-Time Control for Flexible Hypersonic Vehicles with Conditional Disturbance Negation

文献类型:期刊论文

作者Sun, Jinlin1; Pu, Zhiqiang2,3; Chang, Yafei4; Ding, Shihong1; Yi, Jianqiang2,3
刊名IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS
出版日期2023-10-01
卷号59期号:5页码:6327-6345
ISSN号0018-9251
关键词Vehicle dynamics Convergence Control systems Aerodynamics Closed loop systems Actuators Mathematical models Appointed-time control conditional disturbance negation hypersonic vehicle input saturation prescribed performance control
DOI10.1109/TAES.2023.3274098
通讯作者Pu, Zhiqiang(zhiqiang.pu@ia.ac.cn)
英文摘要This article investigates the antidisturbance control design for flexible air-breathing hypersonic vehicles (FAHVs) with appointed-time prescribed tracking performances. The challenging issues include multisource disturbances, cross-coupling effects of the vehicle dynamics, and asymmetric amplitude and rate saturations. To address these issues, we propose an appointed-time prescribed performance control scheme for FAHVs via conditional disturbance negation technique. In contrast to existing disturbance rejection approaches, the proposed control scheme not only estimates the disturbances first in a fixed time but also evaluates the estimated disturbances and selectively conducts compensation actions according to the insight of the FAHV dynamic characteristics. To further enhance convergence rate, the composite appointed-time prescribed performance controllers are designed for FAHVs via time-varying barrier Lyapunov function and nonsmooth backstepping technique, which ensure satisfactory transient response and steady-state performances. In addition, the asymmetric amplitude and rate saturation problem of actuators are dealt with by introducing unified approximation dynamics. It is rigorously proved that the practical appointed-time convergence of the tracking errors and the fixed-time convergence of all signals in the resultant FAHV closed-loop system can be achieved under the proposed control scheme. Finally, extensive comparative simulations are provided to demonstrate the feasibility and superiority of the proposed approach.
WOS关键词ROBUST ADAPTIVE-CONTROL ; ASYMPTOTIC TRACKING ; NONLINEAR-SYSTEMS ; ATTITUDE-CONTROL ; FLIGHT VEHICLES ; UNCERTAINTY ; SUPPRESSION
资助项目National Natural Science Foundation of China[62003034] ; National Natural Science Foundation of China[62203189] ; Natural Science Foundation of Jiangsu Province[BK20220518]
WOS研究方向Engineering ; Telecommunications
语种英语
出版者IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
WOS记录号WOS:001101791300111
资助机构National Natural Science Foundation of China ; Natural Science Foundation of Jiangsu Province
源URL[http://ir.ia.ac.cn/handle/173211/54895]  
专题复杂系统认知与决策实验室
通讯作者Pu, Zhiqiang
作者单位1.Jiangsu Univ, Sch Elect & Informat Engn, Zhenjiang 212013, Peoples R China
2.Chinese Acad Sci, Inst Automat, Beijing 100190, Peoples R China
3.Univ Chinese Acad Sci, Sch Artificial Intelligence, Beijing 100049, Peoples R China
4.Beijing Inst Control Engn, Beijing 100190, Peoples R China
推荐引用方式
GB/T 7714
Sun, Jinlin,Pu, Zhiqiang,Chang, Yafei,et al. Appointed-Time Control for Flexible Hypersonic Vehicles with Conditional Disturbance Negation[J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS,2023,59(5):6327-6345.
APA Sun, Jinlin,Pu, Zhiqiang,Chang, Yafei,Ding, Shihong,&Yi, Jianqiang.(2023).Appointed-Time Control for Flexible Hypersonic Vehicles with Conditional Disturbance Negation.IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS,59(5),6327-6345.
MLA Sun, Jinlin,et al."Appointed-Time Control for Flexible Hypersonic Vehicles with Conditional Disturbance Negation".IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS 59.5(2023):6327-6345.

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来源:自动化研究所

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