dc.contributor.author | Saraçyakupoğlu, Tamer | |
dc.contributor.author | Özçelik, Ahmet Devlet | |
dc.contributor.author | Delibaş, Heyzem Doğukan | |
dc.date.accessioned | 2022-05-12T10:47:22Z | |
dc.date.available | 2022-05-12T10:47:22Z | |
dc.date.issued | 2022 | en_US |
dc.identifier.citation | Saraçyakupoğlu 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.issn | 2602-3350 | |
dc.identifier.issn | 2602-3350 | |
dc.identifier.uri | https://hdl.handle.net/11363/3502 | |
dc.description.abstract | This 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.language.iso | eng | en_US |
dc.publisher | Kerim ÇETİNKAYA | en_US |
dc.relation.isversionof | 10.46519/ij3dptdi.1083686 | en_US |
dc.rights | info:eu-repo/semantics/openAccess | en_US |
dc.rights | Attribution-NonCommercial-NoDerivs 3.0 United States | * |
dc.rights.uri | http://creativecommons.org/licenses/by-nc-nd/3.0/us/ | * |
dc.subject | Mission profile | en_US |
dc.subject | Speed condition | en_US |
dc.subject | Weight calculation | en_US |
dc.title | An Experimental Determinatıon And Numerical Analysis Of A Loiter Munition Unmanned Aerial Vehicle System | en_US |
dc.type | article | en_US |
dc.relation.ispartof | International Journal of 3D Printing Technologies and Digital Industry | en_US |
dc.department | Uygulamalı Bilimler Fakültesi | en_US |
dc.authorid | 0000-0001-5338-726X | en_US |
dc.authorid | 0000-0003-4696-2232 | en_US |
dc.identifier.volume | 6 | en_US |
dc.identifier.issue | 1 | en_US |
dc.identifier.startpage | 83 | en_US |
dc.identifier.endpage | 101 | en_US |
dc.relation.publicationcategory | Makale - Ulusal Hakemli Dergi - Kurum Öğretim Elemanı | en_US |
dc.contributor.institutionauthor | Saraçyakupoğlu, Tamer | |
dc.contributor.institutionauthor | Özçelik, Ahmet Devlet | |