DocumentCode
581689
Title
Inner and outer loop nonlinear controller design of miniature unmanned helicopters
Author
Yuebang, He ; Hailong, Pei ; Hongbo, Zhou
Author_Institution
Key Lab. of Autonomous Syst. & Networked Control, South China Univ. of Technol., Guangzhou, China
fYear
2012
fDate
25-27 July 2012
Firstpage
1040
Lastpage
1045
Abstract
Considering the small inertia and quick response of angular velocity of the miniature unmanned helicopters, an inner-outer loop nonlinear controller is presented based on the simplified model. In the inner loop, a robust H∞ static output controller is designed to control the angular velocity. And in the outer loop, a pole assignment method is used to control the position and yaw angle after dynamic transformation of control surface. Then the controller is compensated for the whole model. The obtained control method has solved the problem of the difficulty of the nonlinear controller to be implemented, and obtains good trajectory tracking performance. At last, simulation results illustrate its high stability, robustness and good trajectory tracking performance.
Keywords
H∞ control; angular velocity control; autonomous aerial vehicles; control system synthesis; helicopters; nonlinear control systems; pole assignment; robust control; trajectory control; angular velocity control; compensation; dynamic transformation; miniature unmanned helicopter; nonlinear controller design; pole assignment method; position control; robust H∞ static output controller design; robustness; stability; trajectory tracking; yaw angle control; Angular velocity; Educational institutions; Electronic mail; Helicopters; Robustness; Stability analysis; Trajectory; pole assignment; robust H∞ static output controller; stability;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2012 31st Chinese
Conference_Location
Hefei
ISSN
1934-1768
Print_ISBN
978-1-4673-2581-3
Type
conf
Filename
6390077
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