This article presents a comparison of controllers which have been applied to a fixed-wing UAV (Unmanned Aerial Vehicle). The comparison is realized between the following nonlinear controllers techniques: sliding modes, nested saturations and back stepping. These controllers are compared and analyzed for altitude, yaw and roll by using simulation tests.


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    Title :

    Nonlinear Controllers Applied to Fixed-Wing UAV


    Contributors:


    Publication date :

    2012-11-01


    Size :

    440873 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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