Journal Article

·2011 OPEN ACCESS

Design and development of a tilt-wing UAV

Ertuğrul Çetinsoy , Efe Sırımoğlu , Kaan Taha Öner , Cevdet Hançer , Mustafa Ünel , Mahmut Faruk Akşit , İlyas Kandemir , Kayhan Gülez YTU

TURKISH JOURNAL OF ELECTRICAL ENGINEERING & COMPUTER SCIENCES

Abstract

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

Takeoff and landing Airplane Aerodynamics Tilt (camera) Takeoff Aerospace engineering Wing Range (aeronautics) Flight control surfaces Elevator Computer science Simulation Automotive engineering Engineering Mechanical engineering

Subject Areas

Adaptive Control of Nonlinear Systems ·Control and Systems Engineering ·Physical Sciences
Aerospace and Aviation Technology ·Aerospace Engineering ·Physical Sciences
Inertial Sensor and Navigation ·Aerospace Engineering ·Physical Sciences

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