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
发表期刊IEEE TRANSACTIONS ON FUZZY SYSTEMS
ISSN1063-6706
2020-10-01
卷号28期号:10页码:2320-2334
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.

关键词Backstepping Adaptive fuzzy control Fuzzy logic finite-time control fixed-time state observer
DOI10.1109/TFUZZ.2019.2934934
关键词[WOS]UNCERTAIN NONLINEAR-SYSTEMS ; DYNAMIC SURFACE CONTROL ; SLIDING MODE CONTROL ; CONTROL DESIGN ; OBSERVER ; STABILIZATION
收录类别SCI
语种英语
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]
项目资助者National Natural Science Foundation of China ; Beijing Advanced Innovation Center of Intelligent Robots and Systems
WOS研究方向Computer Science ; Engineering
WOS类目Computer Science, Artificial Intelligence ; Engineering, Electrical & Electronic
WOS记录号WOS:000578002800004
出版者IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
七大方向——子方向分类智能控制
引用统计
被引频次:46[WOS]   [WOS记录]     [WOS相关记录]
文献类型期刊论文
条目标识符http://ir.ia.ac.cn/handle/173211/42148
专题复杂系统认知与决策实验室_飞行器智能技术
通讯作者Liu, Zhen
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
第一作者单位中国科学院自动化研究所
通讯作者单位中国科学院自动化研究所
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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.
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