DocumentCode
1943703
Title
Control strategy design based on fuzzy logic and LQR for 3-DOF helicopter model
Author
Liu, Zhichao ; El haj, Zouhair Choukri ; Shi, Hongbo
Author_Institution
East China Univ. of Sci. & Technol., Shanghai, China
fYear
2010
fDate
13-15 Aug. 2010
Firstpage
262
Lastpage
266
Abstract
In this paper the elevation and traveling control strategy -fuzzy logic which is based on the LQR for a helicopter with three degrees of freedom is considered. The characteristic of channel coupling and nonlinearity of the system will be resolved by dividing the workplace into 4 phases which the system has a linear behavior, the phases are independently considered and LQR controllers are designed separately. It is then shown that fuzzy logic is used to combine all phases and chooses the appropriate controller parameters for the appropriate phase and so on can stabilize the whole nonlinear system. The performance of this strategy is shown by real response in the end of the paper compared to simple LQR.
Keywords
aircraft control; control system analysis; fuzzy control; helicopters; linear systems; nonlinear control systems; stability; 3-DOF helicopter model; LQR controllers; channel coupling; control strategy design; degrees of freedom; elevation control strategy; fuzzy logic; linear system; nonlinear system; stability; traveling control strategy; Aerospace electronics; Control systems; Differential equations; Fuzzy logic; Helicopters; Mathematical model; Robustness;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Information Processing (ICICIP), 2010 International Conference on
Conference_Location
Dalian
Print_ISBN
978-1-4244-7047-1
Type
conf
DOI
10.1109/ICICIP.2010.5564250
Filename
5564250
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