Different solutions to the problem of aerodynamic surface failure during formation flight are presented. Adaptive control laws are applied in order to compensate for surface blockages. Two different approaches are described in detail, Model Reference Adaptive Control and L1 Adaptive Control, in order to improve the fault-tolerance of a baseline controller designed with static gains. Simulation results are included, showing a substantial improvement of fault-tolerance performance when adaptive augmentation is used.


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    Title :

    Fault tolerant formation flight control using different adaptation techniques


    Contributors:
    Tancredi, Daniele (author) / Gu, Yu (author) / Chao, Haiyang (author)


    Publication date :

    2013-05-01


    Size :

    839959 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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