Attitude Control of Flapping Wing Micro Aerial Vehicle Based on Double Fuzzy Sliding Mode Control

Sheng Bin Hu; Wen Hua Lu; Zhi Yi Chen; Lei Lei; Yi Xuan Zhang

doi:10.4028/www.scientific.net/AMR.468-471.704

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 468-471Attitude Control of Flapping Wing Micro Aerial...

Attitude Control of Flapping Wing Micro Aerial Vehicle Based on Double Fuzzy Sliding Mode Control

Abstract:

An adaptive Double Fuzzy Sliding Mode Control scheme for attitude control of Flapping Wing Micro Aerial Vehicle is proposed in this paper. Based on the feedback linearization technique, a sliding mode controller is designed. To faster response speed, a fuzzy controller is designed to adaptively tune the slope of sliding mode surface. To reduce the chattering, another fuzzy controller is designed to adaptively tune the switch part of sliding mode control. The system stability is proved by Lyapunov principle. Simulation results show that the proposed control scheme is effective.