Abstract An approach is proposed to solving the problem of collaborative design of the structure and stabilization system of a maneuverable unmanned aerial vehicle (UAV) taking into account the requirements of aeroelastic stability. The models and methods, which employ this approach, are described.


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    Title :

    Design of unmanned aerial vehicle structure and stabilization system for aeroelastic stability


    Contributors:

    Published in:

    Publication date :

    2015-07-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English