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

Abstract:

A fuzzy nonsingular terminal 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 nonsingular terminal sliding mode controller is designed. To reduce the chattering in the control input, a fuzzy controller is designed to adaptively tune the switch part gain of nonsingular terminal sliding mode controller according to the nonsingular terminal sliding mode surface. The stability of the control scheme is verified by using Lyapunov principle. Simulation results show that the proposed control scheme is effective.

• Periodical: Applied Mechanics and Materials (Volumes 716-717)
• Pages: 1694-1698
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.716-717.1694
• Online since: December 2014
• Authors: Sheng Bin Hu*, Jian Feng Yin, He Ju Liang, Hui Liu
• Keywords: Flapping Wing Micro Aerial Vehicle, Fuzzy Control, Terminal Sliding Mode Control

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