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Fault-Tolerant Control for T–S Fuzzy Systems With Application to Near-Space Hypersonic Vehicle With Actuator Faults

机译:TS模糊系统的容错控制及其在执行器故障的近空高超声速飞行器中的应用

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This paper addresses the problem of fault-tolerant control for Takagi–Sugeno (T–S) fuzzy systems with actuator faults. First, a general actuator fault model is proposed, which integrates time-varying bias faults and time-varying gain faults. Then, sliding-mode observers (SMOs) are designed to provide a bank of residuals for fault detection and isolation. Based on Lyapunov stability theory, a novel fault-diagnostic algorithm is proposed to estimate the actuator fault, which removes the classical assumption that the time derivative of the output errors should be known as in some existing work. Further, a novel fault-estimation observer is designed. Utilizing the estimated actuator fault, an accommodation scheme is proposed to compensate for the effect of the fault. In addition, a sufficient condition for the existence of SMOs is derived according to Lyapunov stability theory. Finally, simulation results of a near-space hypersonic vehicle are presented to demonstrate the efficiency of the proposed approach.
机译:本文解决了具有执行器故障的Takagi–Sugeno(TS)模糊系统的容错控制问题。首先,提出了一个通用的执行器故障模型,该模型综合了时变偏置故障和时变增益故障。然后,将滑模观察器(SMO)设计为提供一组残差用于故障检测和隔离。基于李雅普诺夫稳定性理论,提出了一种新的故障诊断算法来估计执行器故障,该算法消除了现有工作中应知道输出误差的时间导数的经典假设。此外,设计了一种新颖的故障估计观测器。利用估计的执行器故障,提出了一种调节方案来补偿故障的影响。此外,根据Lyapunov稳定性理论,得出了存在SMO的充分条件。最后,提出了近空间高超音速飞行器的仿真结果,以证明该方法的有效性。

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