Resilient control of flexible hypersonic vehicles against unmatched distributed faults  

作　　者：Dong ZHAO Wenjing REN 

机构地区：[1]School of Artificial Intelligence,Anhui University,Hefei 230601,China [2]Key Laboratory of System Control and Information Processing,Ministry of Education,Shanghai Jiao Tong University,Shanghai 200240,China [3]School of Electrical Engineering and Automation,Hefei University of Technology,Hefei 230009,China

出　　处：《Chinese Journal of Aeronautics》2024年第5期60-70,共11页中国航空学报（英文版）

基　　金：This work was supported by the National Natural Science Foundation of China(Nos.62203002 and 62203148);Natural Science Foundation of Anhui Province,China(Nos.2208085QF204 and 2208085QF203);the Open Project Program of Fujian Provincial Key Laboratory of Intelligent Identification and Control of Complex Dynamic System,China(No.2022A0001);the Fundamental Research Funds for the Central Universities,China(No.JZ2022HGTA0346).

摘　　要：This paper studies a robust fault compensation and vibration suppression problem of flexible hypersonic vehicles.The controlled plant is represented by a cascade system composed of a nonlinear Ordinary Differential Equation(ODE)and an Euler-Bernoulli Beam Equation(EBBE),in which the vibration dynamics is coupled with the rigid dynamics and suffers from distributed faults.A state differential transformation is introduced to transfer distributed faults to an EBBE boundary and a longitudinal dynamics is refined by utilizing T-S fuzzy IF-THEN rules.A novel T-S fuzzy based fault-tolerant control algorithm is developed and related stability conditions are established.The robust exponential stability and well-posedness are proved by using the modified l_(0)-semigroup based Lyapunov direct approach.A simulation study on the longitudinal dynamics of flexible hypersonic vehicles effectively verifies the validity of the developed theoretical results.

关 键 词：Flexible hypersonic vehicles ODE-EBBE cascade Robust exponential stability Unmatched distributed fault compensation Vibration suppression 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计] V448