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Adaptive Identification and Control of Flow-Induced Cavity OscillationsProgress towards an adaptive self-tuning regulator (STR) for the cavity tone problem is discussed in this paper. Adaptive system identification algorithms were applied to an experimental cavity-flow tested as a prerequisite to control. In addition, a simple digital controller and a piezoelectric bimorph actuator were used to demonstrate multiple tone suppression. The control tests at Mach numbers of 0.275, 0.40, and 0.60 indicated approx. = 7dB tone reductions at multiple frequencies. Several different adaptive system identification algorithms were applied at a single freestream Mach number of 0.275. Adaptive finite-impulse response (FIR) filters of orders up to N = 100 were found to be unsuitable for modeling the cavity flow dynamics. Adaptive infinite-impulse response (IIR) filters of comparable order better captured the system dynamics. Two recursive algorithms, the least-mean square (LMS) and the recursive-least square (RLS), were utilized to update the adaptive filter coefficients. Given the sample-time requirements imposed by the cavity flow dynamics, the computational simplicity of the least mean squares (LMS) algorithm is advantageous for real-time control.
Document ID
20030005485
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Kegerise, M. A.
(NASA Langley Research Center Hampton, VA United States)
Cattafesta, L. N.
(Florida Univ. Gainesville, FL United States)
Ha, C.
(Florida Univ. Gainesville, FL United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2002-3158
Report Number: AIAA Paper 2002-3158
Meeting Information
Meeting: 1st AIAA Flow Control Conference
Location: Saint Louis, MO
Country: United States
Start Date: June 24, 2002
End Date: June 27, 2002
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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