Combined active flow and flight control systems design for morphing unmanned aerial vehicles
Yazarlar (4)
Dr. Öğr. Üyesi Öztürk Özdemir KANAT Kastamonu Üniversitesi, Türkiye
Dr. Öğr. Üyesi Ertuğrul Karatay Erciyes Üniversitesi, Türkiye
Doç. Dr. Oğuz Köse Gümüşhane Üniversitesi, Türkiye
Prof. Dr. Tuğrul Oktay Erciyes Üniversitesi, Türkiye
Makale Türü Özgün Makale (SSCI, AHCI, SCI, SCI-Exp dergilerinde yayınlanan tam makale)
Dergi Adı Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering (Q3)
Dergi ISSN 0954-4100 Wos Dergi Scopus Dergi
Dergi Tarandığı Indeksler SCI-Expanded
Makale Dili İngilizce Basım Tarihi 05-2019
Kabul Tarihi Yayınlanma Tarihi 01-05-2019
Cilt / Sayı / Sayfa 233 / 14 / 5393–5402 DOI 10.1177/0954410019846045
Makale Linki http://dx.doi.org/10.1177/0954410019846045
UAK Araştırma Alanları
Aerodinamik
Özet
In this article, combined active flow control system and flight control system design for morphing unmanned aerial vehicles is applied for the first time for autonomous flight performance maximization. For this purpose, longitudinal and lateral dynamics modeling of morphing unmanned aerial vehicle having active flow control manufactured in Erciyes University, Faculty of Aeronautics and Astronautics, Model Aircraft Laboratory is considered in order to obtain simulation environments. Our produced morphing unmanned aerial vehicle is called as ZANKA-II, which has a mass of 6.5 kg, range of 30 km, endurance of 0.5 h, and ceiling altitude of 6000 m. von Karman turbulence modeling is used in order to model atmospheric turbulence during flight in both longitudinal and lateral simulation environments. A stochastic optimization method called as simultaneous perturbation stochastic approximation is also applied for …
Anahtar Kelimeler
active flow control | Automatic control | closed-loop system | control system | morphing | motion control | proportional–integral–derivative control