Ertuğrul ÇETİNSOY, Efe SIRIMOĞLU, Kaan Taha ÖNER, Cevdet HANÇER, Mustafa ÜNEL, Mahmut Faruk AKŞİT, İlyas KANDEMİR, Kayhan GÜLEZ

86108

Design and development of a tilt-wing UAV

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.

Anahtar Kelimeler:

UAV, quad tilt-wing, VTOL, IMU, Kalman filter

Design and development of a tilt-wing UAV

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.

Keywords:

UAV, quad tilt-wing, VTOL, IMU, Kalman filter,

Turkish Journal of Electrical Engineering and Computer Science-Cover

ISSN: 1300-0632
Yayın Aralığı: Yılda 6 Sayı
Yayıncı: TÜBİTAK

Arşiv

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