Design and development of a tilt-wing UAV
| Autor: | Ertuğrul Çetinsoy, Mustafa Unel, Efe Sırımoğlu, Kayhan Gulez, Cevdet Hançer, İlyas Kandemir, Mahmut Faruk Aksit, Kaan Taha Öner |
|---|---|
| Jazyk: | turečtina |
| Rok vydání: | 2014 |
| Předmět: |
Engineering
Wing business.product_category General Computer Science business.industry UAV quad tilt-wing VTOL IMU Kalman filter Kalman filter Aerodynamics Airplane Takeoff and landing Inertial measurement unit Range (aeronautics) Pitch angle Electrical and Electronic Engineering Aerospace engineering business |
| Zdroj: | Volume: 19, Issue: 5 733-741 Turkish Journal of Electrical Engineering and Computer Science |
| ISSN: | 1300-0632 1303-6203 |
| Popis: | In this paper, the mechanical and aerodynamic design, carbon composite production, hierarchical control system design and vertical flight tests of a new unmanned aerial vehicle (UAV), which is capable of VTOL (vertical takeoff and landing) like a helicopter and long range horizontal flight like an airplane, are presented. Real flight tests show that the aerial vehicle can successfully operate in VTOL mode. Kalman filtering is employed to obtain accurate roll and pitch angle estimations. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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