this paper considers application of L1 adaptive output feedback controller to tilt-rotor aircraft longitudinal autopilot design. The proposed adaptive controller has satisfactory performance which meets ADS-33E-PRF Military Rotorcraft handing qualities specifications in the presence of unknown time-varying nonlinearities. Simulations verify the controller.


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    Title :

    L1 adaptive output feedback controller for tilt-rotor aircraft


    Contributors:
    Lu, K. (author) / Liu, Chunsheng (author) / Wang, Zhengzhong (author) / Wang, Weihong (author)


    Publication date :

    2016-08-01


    Size :

    2511667 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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