首页|Resilient control of flexible hypersonic vehicles against unmatched distributed faults

Resilient control of flexible hypersonic vehicles against unmatched distributed faults

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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 lo-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.

Flexible hypersonic vehiclesODE-EBBE cascadeRobust exponential stabilityUnmatched distributed fault compensationVibration suppression

Dong ZHAO、Wenjing REN

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School of Artificial Intelligence,Anhui University,Hefei 230601,China

Key Laboratory of System Control and Information Processing,Ministry of Education,Shanghai Jiao Tong University,Shanghai 200240,China

School of Electrical Engineering and Automation,Hefei University of Technology,Hefei 230009,China

National Natural Science Foundation of ChinaNational Natural Science Foundation of ChinaNatural Science Foundation of Anhui Province,ChinaNatural Science Foundation of Anhui Province,ChinaOpen Project Program of Fujian Provincial Key Laboratory of Intelligent Identification and Control of Complex Dynamic SystemFundamental Research Funds for the Central Universities,China

62203002622031482208085QF2042208085QF2032022A0001JZ2022HGTA0346

2024

中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
年,卷(期):2024.37(5)