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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    Titel :

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


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    2015-07-01


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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