An Experimental Determinatıon And Numerical Analysis Of A Loiter Munition Unmanned Aerial Vehicle System

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dc.authorid0000-0001-5338-726Xen_US
dc.authorid0000-0003-4696-2232en_US
dc.contributor.authorSaraçyakupoğlu, Tamer
dc.contributor.authorÖzçelik, Ahmet Devlet
dc.contributor.authorDelibaş, Heyzem Doğukan
dc.date.accessioned2022-05-12T10:47:22Z
dc.date.available2022-05-12T10:47:22Z
dc.date.issued2022en_US
dc.departmentUygulamalı Bilimler Fakültesien_US
dc.description.abstractThis paper experimentally determinates the calculation of an Unmanned Aerial Vehicle (UAV) and analyzes the design criteria within four different scenarios. The UAV to be designed is a loiter munition UAV system. A mobile or equipment such as a parachute and/or airbag. The UAV may be operable day and night conditions, capable of 2-3 hours of flight hours, and will be launched from a catapult. The UAV navigation system is compact and easily controlled by a personal Global Positioning System (GPS). The mentioned UAV will have a vast operational capability, especially for defense and border security activities since it is equipped with advanced avionics and a small physical footprint for covert operations. As a consequence of this research, it can be claimed that the UAV's mid-wing, twin-tail, and relatively light body will have three axis stability and offer numerous benefits, particularly in terms of operational cost.en_US
dc.identifier.citationSaraçyakupoğlu T., Delibaş H. D., Özçelik A. D “An Experimental Determination and Numerical Analysis of A Loiter Munition Unmanned Aerial Vehicle System” Int. J. of 3D Printing Tech. Dig. Ind., 6(1): 83-101, (2022).en_US
dc.identifier.doi10.46519/ij3dptdi.1083686en_US
dc.identifier.endpage101en_US
dc.identifier.issn2602-3350
dc.identifier.issn2602-3350
dc.identifier.issue1en_US
dc.identifier.startpage83en_US
dc.identifier.trdizinid514825en_US
dc.identifier.urihttps://hdl.handle.net/11363/3502
dc.identifier.urihttps://search.trdizin.gov.tr/tr/yayin/detay/514825
dc.identifier.urihttps://doi.org/
dc.identifier.volume6en_US
dc.indekslendigikaynakTR-Dizinen_US
dc.institutionauthorSaraçyakupoğlu, Tamer
dc.institutionauthorÖzçelik, Ahmet Devlet
dc.language.isoenen_US
dc.publisherKerim ÇETİNKAYAen_US
dc.relation.ispartofInternational Journal of 3D Printing Technologies and Digital Industryen_US
dc.relation.publicationcategoryMakale - Ulusal Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.rightsAttribution-NonCommercial-NoDerivs 3.0 United States*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/us/*
dc.subjectMission profileen_US
dc.subjectSpeed conditionen_US
dc.subjectWeight calculationen_US
dc.titleAn Experimental Determinatıon And Numerical Analysis Of A Loiter Munition Unmanned Aerial Vehicle Systemen_US
dc.typeArticleen_US

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