title   
  

Design and development of a tilt-wing UAV

Çetinsoy, Ertuğrul and Sırımoğlu, Efe and Öner, Kaan Taha and Hançer, Cevdet and Ünel, Mustafa and Akşit, Mahmut Faruk and Kandemir, İlyas and Gülez, Kayhan (2011) Design and development of a tilt-wing UAV. Turkish Journal of Electrical Engineering and Computer Sciences, 19 (5). pp. 733-741. ISSN 1300-0632

Full text not available from this repository.

Official URL: http://dx.doi.org/10.3906/elk-1007-621

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 ( U AV), 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.

Item Type:Article
Subjects:T Technology > TK Electrical engineering. Electronics Nuclear engineering > TK1-4661 Electrical engineering. Electronics Nuclear engineering
Q Science > QA Mathematics > QA075 Electronic computers. Computer science
T Technology > TK Electrical engineering. Electronics Nuclear engineering > TK7800-8360 Electronics
ID Code:17314
Deposited By:Mustafa Ünel
Deposited On:27 Oct 2011 14:38
Last Modified:27 Oct 2011 14:38

Repository Staff Only: item control page