DocumentCode :
105297
Title :
Brief Paper - Robust attitude control of uncertain quadrotors
Author :
Hao Liu ; Yongqiang Bai ; Geng Lu ; Yisheng Zhong
Author_Institution :
Dept. of Autom., Tsinghua Univ., Beijing, China
Volume :
7
Issue :
11
fYear :
2013
fDate :
July 18 2013
Firstpage :
1583
Lastpage :
1589
Abstract :
This study presents a controller design method to achieve the robust attitude control for uncertain quadrotors. The proposed linear time-invariant controller consists of a proportional-derivative (PD) controller and a robust compensator. The PD controller is designed for the nominal linear system to achieve the desired tracking and the robust compensator is added to restrain the influence of the uncertainties. It is proven that attitude tracking errors are bounded and the boundaries can be made as small as desired. Experimental results on the quadrotor are given to confirm the effectiveness of this control method.
Keywords :
PD control; attitude control; autonomous aerial vehicles; control system synthesis; linear systems; robust control; rotors; tracking; uncertain systems; PD controller design method; attitude tracking error; linear system; linear time-invariant controller design method; proportional-derivative controller; robust attitude control; robust compensator; uncertain quadrotor;
fLanguage :
English
Journal_Title :
Control Theory & Applications, IET
Publisher :
iet
ISSN :
1751-8644
Type :
jour
DOI :
10.1049/iet-cta.2012.0964
Filename :
6587896
Link To Document :
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