Control and Identification of Vortex Wakes1

Author:

Anderson C. R.1,Chen Y.-C.2,Gibson J. S.2

Affiliation:

1. Department of Mathematics, University of California, Los Angeles, Los Angeles, CA 90095-1597

2. Mechanical and Aerospace Engineering, University of California, Los Angeles, Los Angeles, CA 90095-1597

Abstract

In this paper, control and identification methods for vortex wakes are investigated. The particular problem studied concerns the stabilization of vortices behind a flat plate, using backside suction as an actuator. The flow dynamics are modeled with a discrete vortex method. Feedback control results for a linear PI controller are presented as well as identification results for a class of input/output models that can be used to design more sophisticated controllers. [S0022-0434(00)00502-5]

Publisher

ASME International

Subject

Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering

Reference19 articles.

1. Bushnell, D. M. , 1992, “Longitudinal Vortex Control—Techniques and Applications,” The 32nd Lanchester Lecture, Aeronaut. J., 96, pp. 293–312.

2. Gad-el-Hak, M., and Bushnell, D. M., 1991, “Separation Control: Review,” ASME J. Fluids Eng., 113, pp. 5–30.

3. Gunzburger, M. D., 1995, Flow Control, Springer-Verlag, New York.

4. Saffman, P. G., and Sheffield, J. S., 1977, “Flow Over a Wing with an Attached Free Vortex,” Stud. Appl. Math., 57, pp. 107–117.

5. Anderson, C. R., Chang, H.-L., and Gibson, J. S., 1993, “Adaptive Control of Vortex Dynamics,” 32nd Control and Decision Conference, IEEE, Dec.

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