Abstract In this paper, we consider a problem of synthesizing the control system of a small gliding (unpowered) aerial vehicle (GAV) with a high-aspect ratio wing (λ ≈ 10). This wing makes it possible to increase significantly the flight range and improve the maneuvering characteristics of the aerial vehicle itself.


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    Title :

    Synthesizing the control system of a small gliding unmanned aerial vehicle with high-aspect ratio wing


    Contributors:

    Published in:

    Publication date :

    2012-07-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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