A model to represent multiple actuator failure cases is developed by polytopic concept. The design of passive fault-tolerant control (FTC) with considerations of both normal and actuator failure cases is investigated, depending on the availability of actuator redundancies. By introducing the parameter dependent Lyapunov and slack methods, an improved algorithm to minimize the peak-to-peak gain of the closed-loop system is proposed. Numerical simulation studies subject to all elevon outages are conducted to illustrate the effectiveness of the designed approach to passive FTC.


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    Title :

    Passive fault-tolerant flight controller design against actuator outages


    Contributors:
    Yu, Xiang (author) / Zhang, Youmin (author)


    Publication date :

    2014-08-01


    Size :

    239800 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Design of passive fault-tolerant flight controller against actuator failures

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    A Fault-tolerant Flight Controller Design for Actuator Faults

    Yee, J.-S. / Wang, J. L. / Jang, B. | British Library Conference Proceedings | 2001