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Fast Terminal Fuzzy Sliding Mode Control for Attitude of Flapping Wing Micro Aerial Vehicle

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Abstract:

A fast terminal fuzzy sliding mode control scheme for the attitude of flapping wing micro aerial vehicle is proposed in this paper. Based on the feedback linearization technique, a fast terminal sliding mode controller is designed. To diminish the chattering in the control input, a fuzzy controller is designed to adjust the generalized gain of fast terminal fuzzy sliding mode controller according to fast terminal sliding mode surface. The stability of the control algorithm is verified by using Lyapunov theory. Simulation results show that the proposed control scheme is effective.

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Periodical:

Applied Mechanics and Materials (Volumes 427-429)

Pages:

1179-1182

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.427-429.1179

Citation:

Cite this paper

Online since:

September 2013

Authors:

Sheng Bin Hu*, Jin Yuan Xu, Xuan Wu, Chi Zhang, Yi Hao He

Keywords:

Attitude Control, Flapping Wing Micro Aerial Vehicle, Fuzzy Control, Terminal Sliding Mode

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© 2013 Trans Tech Publications Ltd. All Rights Reserved

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References

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