Model Free Adaptive Pitch Control of a Flapping Wing Micro Aerial Vehicle with Input Saturation

2020 ◽  
Author(s):  
Tianhe Wang ◽  
Shangtai Jin ◽  
Zhongsheng Hou
Keyword(s):  
Input Saturation ◽  
Flapping Wing ◽  
Micro Aerial Vehicle ◽  
Pitch Control ◽  
Model Free ◽  
Aerial Vehicle

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

2013 ◽  
Vol 427-429 ◽  
pp. 1179-1182
Author(s):  
Sheng Bin Hu ◽  
Jin Yuan Xu ◽  
Xuan Wu ◽  
Chi Zhang ◽  
Yi Hao He
Keyword(s):  
Sliding Mode ◽  
Flapping Wing ◽  
Sliding Mode Controller ◽  
Terminal Sliding Mode ◽  
Micro Aerial Vehicle ◽  
Fuzzy Sliding Mode Control ◽  
Control Scheme ◽  
Fast Terminal Sliding Mode ◽  
Aerial Vehicle ◽  
Fuzzy Sliding Mode

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.

Modeling and simulation study of an insect-like flapping-wing micro aerial vehicle

2006 ◽  
Vol 20 (7) ◽  
pp. 807-824 ◽  
Author(s):  
Decan Zuo ◽  
Wenyuan Chen ◽  
Songlin Peng ◽  
Weiping Zhang
Keyword(s):  
Modeling And Simulation ◽  
Simulation Study ◽  
Flapping Wing ◽  
Micro Aerial Vehicle ◽  
Aerial Vehicle
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