Nonlinear Control Law Design for Lateral Aircraft Dynamics at High Angles of Attack

Costin Ene

doi:10.4028/www.scientific.net/AMM.325-326.1210

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 325-326Nonlinear Control Law Design for Lateral Aircraft...

Nonlinear Control Law Design for Lateral Aircraft Dynamics at High Angles of Attack

Abstract:

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.

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Periodical:

Applied Mechanics and Materials (Volumes 325-326)

Pages:

1210-1214

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.325-326.1210

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Online since:

June 2013

Authors:

Costin Ene

Keywords:

Adaptivebackstepping, High Alpha, Lyapunov Stability, Wing Rock System

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References

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