DocumentCode
529317
Title
Fuzzy sliding-mode control for a Mini-UAV
Author
Fu-Kuang Yeh ; Ching-Mu Chen ; Jian-Ji Huang
Author_Institution
Dept. of Comput. Sci. & Inf. Eng., ChungChou Inst. of Technol., Changhua, Taiwan
fYear
2010
fDate
18-21 Aug. 2010
Firstpage
3317
Lastpage
3323
Abstract
This work addresses a fuzzy sliding-mode controller, which is mainly composed of the sliding mode controller and the fuzzy inference mechanism, for a mini unmanned air vehicle (UAV) with propellers to follow the predetermined trajectory. In this paper, a sliding-mode controller with a sliding surface is designed. And a fuzzy sliding-mode controller is proposed, such that a simple fuzzy inference mechanism is adopted to estimate the upper bound of lumped uncertainty. Therefore, the fuzzy sliding-mode controller is proposed in which the fuzzy inference mechanism with centre of membership functions is investigated. Accordingly, trajectory tracking control of a mini-UAV using the proposed control strategies is illustrated while a mini-UAV is flying. Finally, we employ the Lyapunov stability theory to achieve the stability analysis of the overall nonlinear tracking system. Extensive simulation results are obtained to validate the effectiveness of the fuzzy sliding-mode controller.
Keywords
Lyapunov methods; aircraft; fuzzy control; fuzzy reasoning; mobile robots; nonlinear control systems; position control; remotely operated vehicles; variable structure systems; Lyapunov stability theory; fuzzy inference; fuzzy sliding mode control; mini UAV; nonlinear tracking system; propeller trajectory; unmanned air vehicle; Attitude control; Equations; Mathematical model; Silicon; Stability analysis; Unmanned aerial vehicles; Upper bound; Fuzzy Sliding-Mode Control; Nonlinear System; UAV;
fLanguage
English
Publisher
ieee
Conference_Titel
SICE Annual Conference 2010, Proceedings of
Conference_Location
Taipei
Print_ISBN
978-1-4244-7642-8
Type
conf
Filename
5602550
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