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首页> 外文期刊>European Journal of Control >Robust passive adaptive fault tolerant control for stochastic wing flutter via delay control
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Robust passive adaptive fault tolerant control for stochastic wing flutter via delay control

机译:通过延迟控制的随机翼颤动的鲁棒被动自适应容错控制

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摘要

The problem of robust passive adaptive fault tolerant control for the stochastic wing flutter model is studied in this paper. The stochastic wing flutter model considered possesses the control delay, disturbances, external stochastic bounded disturbance, loss of effectiveness (LOE) and lock-in-place (LIP). The proposed model is a more general LOE-LIP flutter model and covers several common actuator fault tolerant situations. A fault tolerant flutter adaptive observer is given to provide the information of wing flutter states. By combining stability theory of stochastic differential equation, Lyapunov method, adaptive control principles, and linear matrix inequalities (LMIs) technique, the robust passive adaptive fault tolerant controller based on the observer is constructed to solve the wing flutter problem. The passivation of the closed-loop system is theoretically proved. The passive control design for the wing flutter model has its practical significance. The controller can improve the robustness of the closed-loop system, and it accords with the real situation of aeroelastic system. Finally, the applicability and correctness of the proposed controller is well carried out by simulation examples. (C) 2019 European Control Association. Published by Elsevier Ltd. All rights reserved.
机译:本文研究了随机翼形颤动模型的鲁棒无源自适应容错控制的问题。考虑的随机机翼颤动模型具有控制延迟,干扰,外部随机界限干扰,有效性丧失(LOE)和锁定(唇)。所提出的模型是一种更通用的LOE唇颤函模型,涵盖了几个常见的执行器容错情况。给出了容错颤动自适应观察者提供翼颤振态的信息。通过组合随机微分方程的稳定性理论,Lyapunov方法,自适应控制原理和线性矩阵不等式(LMIS)技术,构造了基于观察者的鲁棒无源自适应容错控制器以解决机翼颤动问题。理论上证明了闭环系统的钝化。机翼颤动模型的被动控制设计具有实际意义。控制器可以提高闭环系统的稳健性,符合空气弹性系统的实际情况。最后,通过模拟实施例,所提出的控制器的适用性和正确性很好地进行。 (c)2019年欧洲控制协会。 elsevier有限公司出版。保留所有权利。

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