The invention relates to an aircraft gust alleviation self-adaptive feed-forward control system. The aircraft gust alleviation self-adaptive feed-forward control system comprises a disturbance passage, a control passage and a disturbance identification passage; a discrete transfer function of the control passage is identified by adopting an identification method, and the disturbance identification passage is established on the basis of the discrete transfer function; a disturbance identified by the disturbance identification passage is used as a feedback calculation input for the coefficient calculation of a feed-forward controller, the feed-forward controller is designed by virtue of an FIR model, so that a compensation effect is improved, the control efficiency is increased, and the requirement of the aircraft gust alleviation self-adaptive feed-forward control is maximally satisfied.


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    Title :

    Aircraft gust alleviation self-adaptive feed-forward control system


    Contributors:
    WANG YONGZHI (author) / LI FENG (author) / WU JIAN (author)

    Publication date :

    2015-11-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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