Adaptive Fuzzy Nonsmooth Backstepping Output-Feedback Control for Hypersonic Vehicles With Finite-Time Convergence
Sun, Jinlin1,2; Yi, Jianqiang1,2; Pu, Zhiqiang1,2; Liu, Zhen1,2
刊名IEEE TRANSACTIONS ON FUZZY SYSTEMS
2020-10-01
卷号28期号:10页码:2320-2334
关键词Backstepping Adaptive fuzzy control Fuzzy logic finite-time control fixed-time state observer
ISSN号1063-6706
DOI10.1109/TFUZZ.2019.2934934
英文摘要

It is commonly believed that uncertainties are obstacles to the tracking performances of flexible air-breathing hypersonic vehicles (FAHVs). In addition, the estimation of unmeasured states in an FAHV makes this issue much more complicated. To deal with these difficulties, this article explores a novel adaptive fuzzy nonsmooth backstepping output-feedback control scheme for the FAHV with closed-loop finite-time convergence. First, to approximate the unknown dynamics of the FAHV, some function approximators are constructed by utilizing an interval type-2 (IT2) fuzzy logic system. On this basis, a fixed-time convergent adaptive IT2 fuzzy observer is designed to estimate the unmeasured flight path angle and the unmeasured angle of attack of the FAHV accurately and rapidly. Consequently, the estimation errors of the designed observer are convergent in a fixed time independent of their initial estimation errors. Furthermore, based on the estimated states, velocity and altitude tracking controllers are designed by using a finite-time adaptive IT2 fuzzy nonsmooth backstepping control technique, which avoids the problem of "explosion of complexity" in traditional backstepping methods. Subsequently, rigorous Lyapunov stability analysis is conducted to show the finite-time convergence of the closed-loop signals of the FAHV control system. Finally, the robustness and superiority of the proposed control scheme is validated by several simulations in representative scenarios.

资助项目National Natural Science Foundation of China[61421004] ; National Natural Science Foundation of China[61603384] ; National Natural Science Foundation of China[61603383] ; Beijing Advanced Innovation Center of Intelligent Robots and Systems[2016IRS23]
WOS关键词UNCERTAIN NONLINEAR-SYSTEMS ; DYNAMIC SURFACE CONTROL ; SLIDING MODE CONTROL ; CONTROL DESIGN ; OBSERVER ; STABILIZATION
WOS研究方向Computer Science ; Engineering
语种英语
出版者IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
WOS记录号WOS:000578002800004
资助机构National Natural Science Foundation of China ; Beijing Advanced Innovation Center of Intelligent Robots and Systems
内容类型期刊论文
源URL[http://ir.ia.ac.cn/handle/173211/42147]  
专题综合信息系统研究中心_飞行器智能技术
通讯作者Liu, Zhen
作者单位1.Univ Chinese Acad Sci, Beijing 100049, Peoples R China
2.Chinese Acad Sci, Inst Automat, Beijing 100190, Peoples R China
推荐引用方式
GB/T 7714
Sun, Jinlin,Yi, Jianqiang,Pu, Zhiqiang,et al. Adaptive Fuzzy Nonsmooth Backstepping Output-Feedback Control for Hypersonic Vehicles With Finite-Time Convergence[J]. IEEE TRANSACTIONS ON FUZZY SYSTEMS,2020,28(10):2320-2334.
APA Sun, Jinlin,Yi, Jianqiang,Pu, Zhiqiang,&Liu, Zhen.(2020).Adaptive Fuzzy Nonsmooth Backstepping Output-Feedback Control for Hypersonic Vehicles With Finite-Time Convergence.IEEE TRANSACTIONS ON FUZZY SYSTEMS,28(10),2320-2334.
MLA Sun, Jinlin,et al."Adaptive Fuzzy Nonsmooth Backstepping Output-Feedback Control for Hypersonic Vehicles With Finite-Time Convergence".IEEE TRANSACTIONS ON FUZZY SYSTEMS 28.10(2020):2320-2334.
个性服务
查看访问统计
相关权益政策
暂无数据
收藏/分享
所有评论 (0)
暂无评论
 

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。


©版权所有 ©2017 CSpace - Powered by CSpace