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dc.contributor.authorPetrík, Nikolas Michael
dc.contributor.authorPecho, Pavol
dc.date.accessioned2021-06-23T10:15:42Z
dc.date.available2021-06-23T10:15:42Z
dc.date.issued2021
dc.identifier.urihttp://drepo.uniza.sk/handle/hdluniza/467
dc.description.abstractThe paper is focused on comprehensive design of an unmanned aerial vehicle with fixed wing, which would add efficiency to specific activities performed by rescue services. The current rapid development of unmanned aerial vehicles is slowly becoming part of many industries around the world. The aim of this paper is to design an unmanned aerial vehicle that could provide safe, reliable, and efficient operation. The overall design, construction, and installation of the proposed unmanned aerial vehicle should integrate several modern technologies. To make an ideal design of unmanned aerial vehicle it is required to possess the knowledge of current construction methods of additive manufacturing, understanding of legislation in operating conditions and, in addition to general knowledge of unmanned vehicles, also comprehensive skills in programming and configuration of autonomous control elements of autonomous unmanned systems. After the production of the unmanned aerial vehicle with fixed wing, very good technical properties were demonstrated during experimental ground tests. Achieved technical properties are comparable to those owned by the unmanned aerial vehicles that are currently on the market. The final design configuration using an infrared-sensitive optical device could perform activities such as: searching for missing persons in hard-to-reach and vast terrain or searching for forest fires.en_US
dc.language.isosken_US
dc.publisherUniversity of Zilinaen_US
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectUnmanned aerial vehicleen_US
dc.subjectunmanned aerial systemsen_US
dc.subjectconfigurationen_US
dc.subjectcontrol uniten_US
dc.subjectoptical deviceen_US
dc.subjectsensorsen_US
dc.subjectPixhawk 4en_US
dc.subjectautonomous flighten_US
dc.titleDesign and construction of a UAV device with a fixed wing for the conditions of rescue servicesen_US
dc.typeConference paperen_US
dc.identifier.doihttps://doi.org/10.26552/pas.Z.2021.2.32


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