In this paper, nonlinear sliding mode controller is used in coordination with lookahead-based steering guidance law to simulate the autonomous maneuvering capabilities of a nonlinear, coupled, six degrees of freedom stratospheric airship model. The closed-loop simulation results are presented which signify the robustness of the sliding mode based controller in achieving the commanded maneuver in the presence of modeled uncertainties and wind disturbances.


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    Title :

    Autonomous maneuvering of a stratospheric airship


    Contributors:
    Gobiha, D (author) / Sinha, Nandan K (author)


    Publication date :

    2018-01-01


    Size :

    1024403 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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