Event-Triggered Output Regulation for Networked Flight Control System Based on an Asynchronous Switched System Approach

被引:32
|
作者
Li, Lili [1 ]
Song, Linyang [1 ]
Li, Tieshan [2 ,3 ]
Fu, Jun [4 ]
机构
[1] Dalian Maritime Univ, Coll Marine Elect Engn, Dalian 116026, Peoples R China
[2] Dalian Maritime Univ, Nav Coll, Dalian 116026, Peoples R China
[3] Univ Elect Sci & Technol China, Sch Automat Engn, Chengdu 611731, Peoples R China
[4] Northeastern Univ, State Key Lab Synthet Automat Proc Ind, Shenyang 110819, Peoples R China
来源
IEEE TRANSACTIONS ON SYSTEMS MAN CYBERNETICS-SYSTEMS | 2021年 / 51卷 / 12期
基金
中国国家自然科学基金;
关键词
Switched systems; Switches; Aircraft; Aerospace control; Atmospheric modeling; Aerospace electronics; Event-triggering; networked flight control system (NFCS); output regulation; switched system; H-INFINITY CONTROL; NONLINEAR-SYSTEMS; LINEAR-SYSTEMS; STABILIZATION; ROBUST; STABILITY;
D O I
10.1109/TSMC.2020.2981192
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this article, the event-triggered output regulation problem is investigated for a networked flight control system with a switched system approach. By properly scheduling triggered times of periodic sampling associated with continuous event-triggering and switching instants of each subsystem, an alternate event-triggered mechanism based on the subsystem model is proposed to transmit the triggered information to the candidate controller. Since the subsystem may switch between two adjacent events while the corresponding controller does not switch, asynchronous switching may occur. Meanwhile, an event-triggered switching signal caused by asynchronous switching is designed with the mode-dependent average dwell time approach and event-triggered instants. By constructing multiple Lyapunov functions in the framework of the input delay approach and designing an error feedback controller, the sufficient condition for event-triggered asynchronous output regulation problem is solved. Finally, the proposed methods are proved to be effective by the F-18 aircraft model.
引用
收藏
页码:7675 / 7684
页数:10
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