DocumentCode
3097164
Title
Acceleration feedback enhanced H∞ disturbance attenuation control
Author
He, Yuqing ; Han, Jianda
Author_Institution
Chinese Acad. of Sci., Shenyang
fYear
2007
fDate
5-8 Nov. 2007
Firstpage
839
Lastpage
844
Abstract
In this paper, a robust controller design method is proposed with measurable acceleration signals. In general, the normal high-gain acceleration feedback control (AFC) is too complicated to be designed and cannot be used in underactuated or nonlinear systems, as well suffers from the algebraic loop. Whereas, the new controller in this paper overcome all these disadvantages by introducing a linear pre-filter. Subsequently, the Hinfin technique is used to ensure the disturbance to output stability. And, backstepping algorithm is considered to deal with a class of underactuated systems combined with the new robust controller. Finally, simulations are conducted with respect to the tracking control of an unmanned model helicopter. The results are compared with those obtained by the controllers without acceleration feedback and verify the feasibility of the new controller design method.
Keywords
H∞ control; acceleration control; aircraft control; control system synthesis; feedback; helicopters; nonlinear control systems; remotely operated vehicles; robust control; acceleration feedback control; algebraic loop; backstepping algorithm; enhanced H∞ disturbance attenuation control; linear pre-filter; nonlinear systems; robust controller design method; tracking control; underactuated systems; unmanned model helicopter; Acceleration; Accelerometers; Automatic frequency control; Backstepping; Control systems; Design methodology; Feedback control; Nonlinear systems; Robust control; Stability;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics Society, 2007. IECON 2007. 33rd Annual Conference of the IEEE
Conference_Location
Taipei
ISSN
1553-572X
Print_ISBN
1-4244-0783-4
Type
conf
DOI
10.1109/IECON.2007.4460097
Filename
4460097
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