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.
Unmanned Aerial Vehicle Mass Model Peculiarities
Advs in Intelligent Syst., Computing
International scientific-practical conference ; 2020 ; Chernihiv, Ukraine June 29, 2020 - July 01, 2020
2020-08-30
10 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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