Fast Terminal Fuzzy Sliding Mode Control for Attitude of Flapping Wing Micro Aerial Vehicle
2013 ◽
Vol 427-429
◽
pp. 1179-1182
Keyword(s):
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.
2012 ◽
Vol 178-181
◽
pp. 2801-2804
2014 ◽
Vol 716-717
◽
pp. 1694-1698
2012 ◽
Vol 605-607
◽
pp. 1478-1482
2012 ◽
Vol 468-471
◽
pp. 704-707
2012 ◽
Vol 443-444
◽
pp. 177-182
Keyword(s):
2017 ◽
Vol 71
◽
pp. 521-529
◽
2018 ◽
Vol 233
(2)
◽
pp. 280-298
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