Reduced equivalent systems have inherent closed-loop poles at the origin in the sliding mode for conventional sliding mode control (SMC). A systematic design strategy is developed for arbitrarily placing all SMC closed-loop poles. The speed control of a vertical takeoff and landing aircraft whose aerodynamic parameters vary considerably during flight is investigated. An outstanding output tracking performance and robustness against system parameter uncertainties and external disturbances are achieved.


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    Title :

    Robust vertical takeoff and landing aircraft control via integral sliding mode


    Contributors:
    Huang, Y.J. (author) / Kuo, T.C. (author) / Way, H.K. (author)

    Published in:

    Publication date :

    2003


    Size :

    6 Seiten, 10 Quellen




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English