Innovative Morphing UAV Design and Manufacture

Yıl 2023, Cilt: 7 Sayı: 2, 184 - 189, 25.07.2023

Sezer Çoban , Tugrul Oktay

https://doi.org/10.30518/jav.1253901

Cited By: 3

Öz

In this study, an unmanned aerial vehicle (UAV) with passive pre-flight and active in-flight morphing capability was designed and manufactured. First of all, conceptual design work was done. Wing and tail, which are the main carriers, were selected to ensure maximum liftt, minimum drag and stability of the UAV. Liquid fuel engines were preferred due to their high power and airtime. The engine, which enables the controlled and uncontrolled flight of the UAV, has been run-in to make it safer and more efficient before being used in real-time flights. Profiles were selected by analyzing the tail set consisting of the rudder and the elevator. The nose cone of the unmanned aerial vehicle was produced by improving the aerodynamic performance. In the aircraft geometry, the passive morphing mechanism, which is performed once before the flight, and the active morphing mechanism, which is performed continuously during the flight, are manufactured using servo motors. This improved the flight performance and made it possible to fly in some unfavorable conditions. The most basic superior feature of the manufactured UAV from the existing UAVs is its ability to morphing.

Anahtar Kelimeler

UAV, Design, Manufacture, Morphing

Destekleyen Kurum

TÜBİTAK

Proje Numarası

115M603

Teşekkür

This work was supported by Research Fund of The Scientific and Technological Research Council of Turkey (TUBITAK) under Project Number: 115M603.

Kaynakça

• Ameduri, S., & Concilio, A. (2020). Morphing wings review: aims, challenges, and current open issues of a technology. Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 0954406220944423.
• Çoban, S. (2019). Simultaneous tailplane of small UAV and autopilot system design. Aircraft Engineering and Aerospace Technology.
• Çoban, S., & Oktay, T. (2018). Simultaneous Design of a Small UAV (Unmanned Aerial Vehicle) Flight Control System and Lateral State Space Model. Journal of Aviation, 2(2), 70-76.
• Friswell, M. I., & Inman, D. J. (2006, April). Morphing concepts for UAVs. In 21st Bristol UAV systems conference (pp. 13-1).
• Gamboa, P., Aleixo, P., Vale, J., Lau, F., & Suleman, A. (2007). Design and testing of a morphing wing for an experimental UAV. University of beira interior covilha (portugal).
• Gomez, J. C., & Garcia, E. (2011). Morphing unmanned aerial vehicles. Smart Materials and Structures, 20(10), 103001.
• Harvey, C., Gamble, L. L., Bolander, C. R., Hunsaker, D. F., Joo, J. J., & Inman, D. J. (2022). A review of avian- inspired morphing for UAV flight control. Progress in Aerospace Sciences, 132, 100825.
• Joshi, S., Tidwell, Z., Crossley, W., & Ramakrishnan, S. (2004). Comparison of morphing wing stategies based upon aircraft performance impacts. In 45th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics & materials conference (p. 1722).
• Konar, M. (2019). Redesign of morphing UAV's winglet using DS algorithm based ANFIS model. Aircraft Engineering and Aerospace Technology, 91(9), 1214-1222.
• Konar, M. (2020). Simultaneous determination of maximum acceleration and endurance of morphing UAV with ABC algorithm-based model. Aircraft Engineering and Aerospace Technology.
• Min, Z., Kien, V. K., & Richard, L. J. (2010). Aircraft morphing wing concepts with radical geometry change. The IES Journal Part A: Civil & Structural Engineering, 3(3), 188-195.
• Oktay, T., & Coban, S. (2017). Lateral autonomous performance maximization of tactical unmanned aerial vehicles by integrated passive and active morphing. International Journal of Advanced Research in Engineering, 3(1), 1-5.
• Önal, M., Çoban, S., Yapici, A., & Bilgiç, H. H. (2019). Araştırma Makalesi/Research Article DOI: 10.30518/jav. 633775. Journal of Aviation, 3(2), 106-112.
• Popov, A. V., Grigorie, T. L., Botez, R. M., Mébarki, Y., & Mamou, M. (2010). Modeling and testing of a morphing wing in open-loop architecture. Journal of Aircraft, 47(3), 917-923.
• Sofla, A. Y. N., Meguid, S. A., Tan, K. T., & Yeo, W. K. (2010). Shape morphing of aircraft wing: Status and challenges. Materials & Design, 31(3), 1284-1292.
• Thill, C., Etches, J. A., Bond, I. P., Potter, K. D., & Weaver, P. M. (2010). Composite corrugated structures for morphing wing skin applications. Smart Materials and Structures, 19(12), 124009.
• Uzun, M., & Çoban, S. (2021). Aerodynamic Performance Improvement with Morphing Winglet Design. Journal of Aviation, 5(1), 16-21.
• Uzun, M., Özdemir, M., Yıldırım, Ç. V., & Çoban, S. (2022). A novel biomimetic wing design and optimizing aerodynamic performance. Journal of Aviation, 6(1), 12-25.
• Vasista, S., Tong, L., & Wong, K. C. (2012). Realization of morphing wings: a multidisciplinary challenge. Journal of aircraft, 49(1), 11-28.
• Vocke III, R. D., Kothera, C. S., Woods, B. K., & Wereley, N. M. (2011). Development and testing of a span- extending morphing wing. Journal of Intelligent Material Systems and Structures, 22(9), 879-890.