This paper treats the question of control of two-dimensional incompressible, unsteady wake flow behind a circular cylinder at Reynolds number Re=100. Two finite-dimensional lower order models based on proper orthogonal decomposition (POD) are considered for the control system design. Control action is achieved via cylinder rotation. Linear optimal control theory is used for obtaining stabilizing feedback control systems. An expression for the region of stability of the system is derived. Simulation results for 18-mode POD models obtained using the control function and penalty methods are presented. These results show that in the closed-loop system mode amplitudes asymptotically converge to the chosen equilibrium state for each flow model for large perturbations in the initial states.
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September 2001
Technical Papers
Optimal Feedback Control of Vortex Shedding Using Proper Orthogonal Decomposition Models
Sahjendra N. Singh,
Sahjendra N. Singh
Department of Electrical and Computer Engineering, University of Nevada, Las Vegas, NV 89154-4026
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James H. Myatt,
James H. Myatt
Airforce Research Laboratory (AFRL/VACA), 2210 Eighth St., Bldg. 146, Wright-Patterson AFB, OH 45433-7531
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Gregory A. Addington,
Gregory A. Addington
Airforce Research Laboratory (AFRL/VACA), 2210 Eighth St., Bldg. 146, Wright-Patterson AFB, OH 45433-7531
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Siva Banda,
Siva Banda
Airforce Research Laboratory (AFRL/VACA), 2210 Eighth St., Bldg. 146, Wright-Patterson AFB, OH 45433-7531
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James K. Hall
James K. Hall
Airforce Research Laboratory (AFRL/VACA), 2210 Eighth St., Bldg. 146, Wright-Patterson AFB, OH 45433-7531
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Sahjendra N. Singh
Department of Electrical and Computer Engineering, University of Nevada, Las Vegas, NV 89154-4026
James H. Myatt
Airforce Research Laboratory (AFRL/VACA), 2210 Eighth St., Bldg. 146, Wright-Patterson AFB, OH 45433-7531
Gregory A. Addington
Airforce Research Laboratory (AFRL/VACA), 2210 Eighth St., Bldg. 146, Wright-Patterson AFB, OH 45433-7531
Siva Banda
Airforce Research Laboratory (AFRL/VACA), 2210 Eighth St., Bldg. 146, Wright-Patterson AFB, OH 45433-7531
James K. Hall
Airforce Research Laboratory (AFRL/VACA), 2210 Eighth St., Bldg. 146, Wright-Patterson AFB, OH 45433-7531
Contributed by the Fluids Engineering Division for publication in the JOURNAL OF FLUIDS ENGINEERING. Manuscript received by the Fluids Engineering Division October 28, 2000; revised manuscript received May 1, 2001. Associate Editor: P. Bradshaw.
J. Fluids Eng. Sep 2001, 123(3): 612-618 (7 pages)
Published Online: May 1, 2001
Article history
Received:
October 28, 2000
Revised:
May 1, 2001
Citation
Singh, S. N., Myatt , J. H., Addington , G. A., Banda , S., and Hall, J. K. (May 1, 2001). "Optimal Feedback Control of Vortex Shedding Using Proper Orthogonal Decomposition Models ." ASME. J. Fluids Eng. September 2001; 123(3): 612–618. https://doi.org/10.1115/1.1385513
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