Abstract This paper proposed a method of adaptive controller with a lead-lag parameters compensator and applied to a kind of aircraft boundary control system (ABCS). This method ensures optimization of fuzzy logic control function, and guarantees on-line adaptation of domain in aircraft boundary control system, which can make a great progress in dynamic characteristics and adaptabilities of flight control system. A proposed hybrid adaptation algorithm has been tested in the analogy flight practice speed control system of an induction motor drive. The digital simulation results demonstrated that it could improve transient properties in flight boundary control system, and provide well disturbance rejection in spite of its simplicity.


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    Titel :

    Adaptive Control with Parameters Compensator for Aircraft Boundary Control System


    Beteiligte:
    Kun, Qian (Autor:in) / Kai, Liu (Autor:in) / Hao, Yan (Autor:in) / Kaijun, Liao (Autor:in)


    Erscheinungsdatum :

    12.11.2017


    Format / Umfang :

    8 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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