| 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
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| 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 |
| Atıf Sayıları | |
| Web of Science | 11 |
| Scopus | 15 |
| Google Scholar | 20 |
| Dergi Adı | PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING |
| Yayıncı | SAGE Publications Ltd |
| Açık Erişim | Hayır |
| ISSN | 0954-4100 |
| E-ISSN | 2041-3025 |
| CiteScore | 2,9 |
| SJR | 0,372 |
| SNIP | 0,690 |