Makale detayı · 2011
Design and development of a tilt wing UAV
Turkish Journal of Electrical Engineering and Computer Sciences
YÖKSİS
OpenAlex
Açık erişim · bronze
SJR Q3
JCR Q4
TR Index
Atıf 26
Yüzdelik 89.7%
FWCI 2.08
- Yıl
- 2011
- ISSN
1300-0632- Tür
- article
Veri kaynağı ayrımı
- YÖKSİS YÖKSİS makale kaydı
- OpenAlex OpenAlex zenginleştirmesi (özet, atıf, konular)
Özet
İngilizce (OpenAlex)
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.
Konular
- Adaptive Control of Nonlinear Systems
- Aerospace and Aviation Technology
- Inertial Sensor and Navigation
Birincil konu Adaptive Control of Nonlinear Systems