To suppress airfoil flutter, a lot of control methods have been proposed, such as classical control methods and optimal control methods. However, these methods did not consider the influence of actuator faults and control delay. This paper proposes a new finite-time H adaptive fault-tolerant flutter controller by radial basis function neural network technology and adaptive fault-tolerant control method, taking into account actuator faults, control delay, modeling uncertainties, and external disturbances. The theoretic section of this paper is about airfoil flutter dynamic modeling and adaptive fault-tolerant controller design. Lyapunov function and linear matrix inequality are employed to prove the stability of the proposed control method of this paper. The numeral simulation section further proves the effectiveness and robustness of the proposed control algorithm of this paper.


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    Titel :

    A finite-time H-infinite adaptive fault-tolerant controller considering time delay for flutter suppression of airfoil flutter


    Beteiligte:
    Ming-Zhou, Gao (Autor:in) / Xin-Yi, Chen (Autor:in) / Rong, Han (Autor:in) / Jian-Yong, Yao (Autor:in)


    Erscheinungsdatum :

    01.02.2020


    Format / Umfang :

    15 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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