National University of Defense Technology has begun a research program to investigate and test ducted-fan propeller architecture for UAV designing. Development of a prototype continues to support ongoing research in the area of autonomous systems. In this paper, we build a nonlinear dynamic model of Ducted-Fan UAV for verifying appropriate controller behavior, and design a hierarchical controller for hovering flight of the UAV.


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    Titel :

    Modeling and Hovering Control of an Ducted-Fan UAV in Low Speed Crosswind



    Erschienen in:

    Advanced Materials Research ; 466-467 ; 1060-1064


    Erscheinungsdatum :

    2012-02-10


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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