Fuzzy Nonsingular Terminal Sliding Mode Control for Attitude of Flapping Wing Micro Aerial Vehicle
2014 ◽
Vol 716-717
◽
pp. 1694-1698
Keyword(s):
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.
2012 ◽
Vol 605-607
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pp. 1478-1482
2013 ◽
Vol 427-429
◽
pp. 1179-1182
2017 ◽
2013 ◽
Vol 655-657
◽
pp. 1048-1052
2014 ◽
Vol 39
(6)
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pp. 902-908
◽
2021 ◽
Vol 1952
(3)
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pp. 032013