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CONTROLLING CHAOTIC MOTIONS IN A TWO-DIMENSIONAL AIRFOIL USING TIME-DELAYED FEEDBACK

โœ Scribed by M. RAMESH; S. NARAYANAN


Publisher
Elsevier Science
Year
2001
Tongue
English
Weight
303 KB
Volume
239
Category
Article
ISSN
0022-460X

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โœฆ Synopsis


In this paper, the chaotic motions of a two-dimensional airfoil are controlled by the application of the time-delayed continuous feedback method of Pyragas. The airfoil has cubic pitching sti!ness and linear viscous damping when kept in an incompressible #uid #ow. Four control strategies are implemented with plunging displacement, plunging velocity, pitching angle, and pitching velocity as the feedback signals. The control signal is applied to perturb the airspeed parameter. The response of the system under these four controls is compared. It is found that the feedback control signal derived from the pitching variables was found to be more e!ective in controlling the chaotic motion of the airfoil.


๐Ÿ“œ SIMILAR VOLUMES


RESONANCES OF A NON-LINEAR s.d.o.f. SYST
โœ J.C. JI; A.Y.T. LEUNG ๐Ÿ“‚ Article ๐Ÿ“… 2002 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 207 KB

The primary, superharmonic, and subharmonic resonances of a harmonically excited non-linear s.d.o.f. system with two distinct time-delays in the linear state feeback are studied. The two di!erent time-delays are presented in the proportional feedback and the derivative feedback respectively. The met