The invention relates to an aircraft gust alleviation self-adapting feedforward control method based on GOFIR. According to the present invention, the dynamic characteristics of a controlled object are injected into a GOFIR controller through the pole of an identified transfer function, the characteristic of the control system is obtained through an identification method and is represented by the pole of the transfer function, the GOFIR controller is designed by using the pole, and the coefficient of the GOFIR controller is obtained through a self-adapting algorithm; and with the method, the model order of the designed controller can be reduced, and the control efficiency of the controller can be improved.


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    Titel :

    Aircraft gust alleviation self-adapting feedforward control method based on GOFIR


    Beteiligte:
    WANG YONGZHI (Autor:in) / LI FENG (Autor:in) / LI ZHIGUO (Autor:in) / LI GUANGJIA (Autor:in)

    Erscheinungsdatum :

    2015-12-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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