An aircraft model that incorporates independently adjustable engine throttles and ailerons is employed to develop an adaptive control scheme in the presence of actuator failures. This model captures the key features of aircraft flight dynamics when in the engine differential mode. Based on this model an adaptive feedback control scheme for asymptotic state tracking is developed and applied to a transport aircraft model in the presence of two types of failures during operation, rudder failure and aileron failure. Simulation results are presented to demonstrate the adaptive failure compensation scheme.


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    Title :

    Adaptive Failure Compensation for Aircraft Tracking Control Using Engine Differential Based Model


    Contributors:
    Y. Liu (author) / X. Tang (author) / G. Tao (author) / S. M. Joshi (author)

    Publication date :

    2006


    Size :

    6 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English