Affiliation:
1. University “Politehnica” of Bucharest
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.
Publisher
Trans Tech Publications, Ltd.
Reference8 articles.
1. C. H. Hsu and E. Lan, Theory of wing rock, AIAA Journal of Aircraft, vol. 22, pp.920-924, (1985).
2. Yoshinaga, T., Tate, A., and Noda, J., Wing rock of delta wings with an analysis by the phase plane method', Proceedings of the AIAA Atmospheric Flight Mechanics Conference, Monterey, AIAA Washington, DC, , 93.
3. A. H. Nayfeh , J. M. Elzebda and D .T. Mook, Analytical study of the subsonic wing rock phenomenon for slender delta wings, Journal of Aircraft , vol. 26, no. 9, pp.805-809, (1989).
4. S. N. Singh, W. Yim, and W. R. Wells, Direct adaptive and neural control of the wing rock motion of slender delta wings, Journal of Guidance Control Dynamics, vol. 18, pp.25-30, Jan. (1995).
5. R. Ordonez and K. M. Passino, Wing rock regulation with a timevarying angle of attack, 15th IEEE Int. Symposium on Intelligent Control (ISIC 2000), Greece, pp.145-150, July (2000).