DocumentCode
530734
Title
Backstepping control of each channel for a quadrotor aerial robot
Author
Yali, Yu ; Changhong, Jiang ; Haiwei, Wu
Author_Institution
Eng. Training Center, Harbin Eng. Univ., Harbin, China
Volume
3
fYear
2010
fDate
24-26 Aug. 2010
Firstpage
403
Lastpage
407
Abstract
This paper has presented a model of vertical take-off and landing(VTOL) unmanned air vehicle. It has four rotors, so as quadrotor aerial robot. It can hover or fly at low speed indoor or unwinded outdoor. The quadrotor aerial robot is a highly nonlinear, multivariable, strongly coupled and under-actuated subsystem because it has 6-DOF but only has four inputs. Nonlinear mathematical model of quadrotor aerial robot which is based on Newton-Euler formalism is deduced in the paper, also described nonlinear control strategy for it. Backstepping of nonlinear controller design was based on constructing Lyapunov function for closed-loop system. The controller guarantees stability, tracking performance and robotness of the system. The effective control design scheme is shown through nonlinear simulations.
Keywords
Lyapunov methods; aircraft control; closed loop systems; control system synthesis; helicopters; mobile robots; multivariable control systems; nonlinear control systems; remotely operated vehicles; Lyapunov function; Newton-Euler formalism; backstepping control; closed-loop system; nonlinear controller design; nonlinear mathematical model; quadrotor aerial robot; under-actuated subsystem; vertical take-off and landing unmanned air vehicle; Bismuth; Educational institutions; Force; Lead; Robots; Torque; Yttrium; Backstepping; Newton-Euler formalism; VTOL; quadrotor aerial robot;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer, Mechatronics, Control and Electronic Engineering (CMCE), 2010 International Conference on
Conference_Location
Changchun
Print_ISBN
978-1-4244-7957-3
Type
conf
DOI
10.1109/CMCE.2010.5610299
Filename
5610299
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