The article discusses the features of the mass balance of an unmanned aerial vehicle (UAV) and the mass of UAV safety equipment; the equation of the UAV mass balance and the dependence of the UAV take-off mass on the known loads and the relative masses of the UAV parts are obtained taking into account safety and airworthiness; The main systems designed to replace the pilot on board an unmanned aerial vehicle are considered; The dependence of the total mass of the apparatus on the masses of means ensuring safe operation is demonstrated; the calculations of several options for the mass balance depending on the purpose of the unmanned aerial vehicle; the dependence of the thrust-weight ratio, flight range, maximum speed and mass of an unmanned aerial vehicle of civilian use is considered in a first approximation; the developed mass balance model was tested in the project of creating the Sparrow unmanned aerial vehicle at the National Aerospace University, Kharkov Aviation Institute.


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    Titel :

    Unmanned Aerial Vehicle Mass Model Peculiarities


    Weitere Titelangaben:

    Advs in Intelligent Syst., Computing


    Beteiligte:
    Shkarlet, Serhiy (Herausgeber:in) / Morozov, Anatoliy (Herausgeber:in) / Palagin, Alexander (Herausgeber:in) / Kritskiy, Dmitriy (Autor:in) / Yashin, Sergiy (Autor:in) / Koba, Sergiy (Autor:in)

    Kongress:

    International scientific-practical conference ; 2020 ; Chernihiv, Ukraine June 29, 2020 - July 01, 2020



    Erscheinungsdatum :

    2020-08-30


    Format / Umfang :

    10 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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