Yazar "Uzun, Metin" için listeleme
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The aerodynamic force estimation of a swept-wing UAV using ANFIS based on metaheuristic algorithms
Uzun, Metin; Bilgiç, Hasan Hüseyin; Çopur, Engin Hasan; Çoban, Sezer (Cambridge University Press, 2023)In this paper, a new approach to modeling and controlling the problems associated with a morphing unmanned aerial vehicle (UAV) is proposed. Within the scope of the study, a dataset was created by obtaining a wide range ... -
Aerodynamic Performance Improvement with Morphing Winglet Design
Uzun, Metin; Çoban, Sezer (Journal of aviation (Online), 2021)The aim of this study is to reduce unnecessary lift and minimize drag at the same time when the aircraft reaches a certain speed level by using the active morphing method during flight. In this study, the flight performance ... -
Autonomous flight performance maximization for slung load carrying rotary wing mini unmanned aerial vehicle
Uzun, Metin (Emerald Publishing, 2024)Purpose: This research study aims to minimize autonomous flight cost and maximize autonomous flight performance of a slung load carrying rotary wing mini unmanned aerial vehicle (i.e. UAV) by stochastically optimizing ... -
Electrically Driven VTOL Flying Car Designing and Aerodynamic Analysis
Uzun, Metin; Çoban, Sezer (Avrupa Bilim ve Teknoloji Dergisi, 2021)In this study, the design of the electric powered VTOL Flying car was made in the CAD program, and the longitudinal, vertical and lateral flight dynamics were examined and aerodynamic analysis was made. In the design, the ... -
Flight control system design of UAV with wing incidence angle simultaneously and stochastically varied
Uzun, Metin (Emerald Publishing, 2024)PurposeThis study aims to simultaneously and stochastically maximize autonomous flight performance of a variable wing incidence angle having an unmanned aerial vehicle (UAV) and its flight control system (FCS) design.Des ... -
İnsansız hava araçlarında çoklu pervane sistemi kullanımının uçuş performansına etkisinin sayısal olarak incelenmesi
Dönmez, Kasım Şahin (İskenderun Teknik Üniversitesi, 2024)Bu çalışmanın amacı, toplam kalkış ağırlığındaki değişikliklerle elektronik donanım ve pervane tipini değiştirmeden yatay ve düşey yönlerde birden fazla pervane kullanarak Sabit Pervaneli İnsansız Hava Araçları ihtiyacını ... -
MALE UAV selection in interval Type-2 fuzzy sets environment
Çoban, Sezer; Kiracı, Kasım; Akan, Ercan; Uzun, Metin (IOS Press BV, 2022)Unmanned Aerial Vehicles (UAVs) are increasingly used in the military field. Especially in recent years, UAVs have been a very effective instrument in gaining airspace superiority and military success. Many countries compete ... -
A Novel Biomimetic Wing Design and Optimizing Aerodynamic Performance
Uzun, Metin; Özdemir, Mustafa; Yıldırım, Çağrı Vakkas; Çoban, Sezer (Edit Publishing, 2022)In this article, numerical and experimental analyzes were made by adding winglet and endless blade to the tip of the airfoil to improve the wind turbine blade performance. Similarly, the change in performance was investigated ... -
Simultaneous UAV having actively sweep angle morphing wing and flight control system design
Uzun, Metin; Oktay, Tuğrul (Emerald Publishing, 2023)Purpose: The purpose of this paper is to improve autonomous flight performance of an unmanned aerial vehicle (UAV) having actively sweep angle morphing wing using simultaneous UAV and flight control system (FCS) design. ... -
Structural and Fatigue Analysis of a UAV Wing
Uzun,Metin; Çınar,Hasan; Kocamer,Abdullah; Çoban,Sezer (Vedat Veli ÇAY, 2024)In this study, the structural and fatigue analyses of an unmanned aerial vehicle wing are investigated together. The spar, which is the main load carrier of the wing, and the ribs, which are the structural support parts ... -
Structural comparison of vertical and horizontal layout of carrying arms of rotary-wing UAV with finite element analysis
Kocamer, Abdullah; Çınar, Hasan; Uzun, Metin; Çoban, Sezer (European Mechanical Science, 2023)In this study, numerical analysis of the fuselage of a rotary wing unmanned aerial vehicle was conducted. A fuselage that is resistant to the loads on the fuselage and has maximum lightness has been designed. In this ...
