Nonlinear Control Law Design for Lateral Aircraft Dynamics at High Angles of Attack
2013 ◽
Vol 325-326
◽
pp. 1210-1214
Keyword(s):
In this paper, an adaptive backstepping type design is proposed to control the complex nonlinear behavior of the wing rock phenomenon. This method, based on Lyapunov stability theory, can simultaneouslyachieve parameters identification and control.Finally numerical simulations are presented to justify the effectiveness of the proposed controller.
2021 ◽
pp. 014233122098363
2014 ◽
Vol 24
(3)
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pp. 257-270
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2008 ◽
Vol 22
(08)
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pp. 1015-1023
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2017 ◽
Vol 7
(3)
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pp. 248-254
2011 ◽
Vol 25
(04)
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pp. 521-529
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2013 ◽
Vol 2013
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pp. 1-12
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2011 ◽
Vol 25
(27)
◽
pp. 3671-3678
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