DocumentCode
2405226
Title
Revisited Dos Samara Unmanned Aerial Vehicle: Design and control
Author
Alexis, Kostas ; Tzes, Anthony
Author_Institution
Electr. & Comput. Eng. Dept., Univ. of Patras, Greece
fYear
2012
fDate
14-18 May 2012
Firstpage
3645
Lastpage
3650
Abstract
In this article, the design, system modeling and control of a new hybrid type of Unmanned Aerial Vehicle (UAV) is presented. Based on the flight principles of the Dos Samara UAV, a new vehicle that combines the capability of hovering, like a helicopter, and high speed-increased endurance flying, like a fixed-wing aircraft, is designed. The nonlinear dynamics model of the aircraft operating in helicopter mode is derived and linearized around hovering operation. Based on this model an LQ-controller is designed. The performance of the overall system is examined in simulation studies.
Keywords
autonomous aerial vehicles; control system synthesis; helicopters; linear quadratic control; nonlinear dynamical systems; ίight principles; Dos Samara unmanned aerial vehicle; LQ-controller design; fixed-wing aircraft; helicopter; high speed-increased endurance flying; hovering operation; nonlinear dynamics model; system modeling; Aerodynamics; Brushless motors; Helicopters; Nonlinear dynamical systems; Propellers; Solid modeling;
fLanguage
English
Publisher
ieee
Conference_Titel
Robotics and Automation (ICRA), 2012 IEEE International Conference on
Conference_Location
Saint Paul, MN
ISSN
1050-4729
Print_ISBN
978-1-4673-1403-9
Electronic_ISBN
1050-4729
Type
conf
DOI
10.1109/ICRA.2012.6224559
Filename
6224559
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