Modelling for robust feedback control of fluid flows
Modelling for robust feedback control of fluid flows
This paper addresses the problem of designing low-order and linear robust feedback controllers that provide a priori guarantees with respect to stability and performance when applied to a fluid flow. This is challenging since whilst many flows are governed by a set of nonlinear, partial differential-algebraic equations (the Navier-Stokes equations), the majority of established control system design assumes models of much greater simplicity, in that they are firstly: linear, secondly: described by ordinary differential equations, and thirdly: finite-dimensional. With this in mind, we present a set of techniques that enables the disparity between such models and the underlying flow system to be quantified in a fashion that informs the subsequent design of feedback flow controllers, specifically those based on the \(\mathcal{H}_\infty\) loop-shaping approach. Highlights include the application of a model refinement technique as a means of obtaining low-order models with an associated bound that quantifies the closed-loop degradation incurred by using such finite-dimensional approximations of the underlying flow. In addition, we demonstrate how the influence of the nonlinearity of the flow can be attenuated by a linear feedback controller that employs high loop gain over a select frequency range, and offer an explanation for this in terms of Landahl’s theory of sheared turbulence. To illustrate the application of these techniques, a \(\mathcal{H}_\infty\) loop-shaping controller is designed and applied to the problem of reducing perturbation wall-shear stress in plane channel flow. DNS results demonstrate robust attenuation of the perturbation shear-stresses across a wide range of Reynolds numbers with a single, linear controller.
687-722
Jones, Bryn
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Heins, Peter
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Kerrigan, Eric
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Morrison, Jonathan F.
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Sharma, Ati S.
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25 March 2015
Jones, Bryn
b660e0f9-93f0-46ac-8aba-adb6ceba617f
Heins, Peter
d73df3f6-f569-4eb4-b16b-2d4a26d59fa2
Kerrigan, Eric
d2f62138-2072-4901-b453-de035c698cf5
Morrison, Jonathan F.
7fcc8b7e-397e-4891-97cd-ab5406f8d01e
Sharma, Ati S.
cdd9deae-6f3a-40d9-864c-76baf85d8718
Jones, Bryn, Heins, Peter, Kerrigan, Eric, Morrison, Jonathan F. and Sharma, Ati S.
(2015)
Modelling for robust feedback control of fluid flows.
Journal of Fluid Mechanics, 769, .
(doi:10.1017/jfm.2015.84).
Abstract
This paper addresses the problem of designing low-order and linear robust feedback controllers that provide a priori guarantees with respect to stability and performance when applied to a fluid flow. This is challenging since whilst many flows are governed by a set of nonlinear, partial differential-algebraic equations (the Navier-Stokes equations), the majority of established control system design assumes models of much greater simplicity, in that they are firstly: linear, secondly: described by ordinary differential equations, and thirdly: finite-dimensional. With this in mind, we present a set of techniques that enables the disparity between such models and the underlying flow system to be quantified in a fashion that informs the subsequent design of feedback flow controllers, specifically those based on the \(\mathcal{H}_\infty\) loop-shaping approach. Highlights include the application of a model refinement technique as a means of obtaining low-order models with an associated bound that quantifies the closed-loop degradation incurred by using such finite-dimensional approximations of the underlying flow. In addition, we demonstrate how the influence of the nonlinearity of the flow can be attenuated by a linear feedback controller that employs high loop gain over a select frequency range, and offer an explanation for this in terms of Landahl’s theory of sheared turbulence. To illustrate the application of these techniques, a \(\mathcal{H}_\infty\) loop-shaping controller is designed and applied to the problem of reducing perturbation wall-shear stress in plane channel flow. DNS results demonstrate robust attenuation of the perturbation shear-stresses across a wide range of Reynolds numbers with a single, linear controller.
Text
Jones-et-al.pdf
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More information
Accepted/In Press date: 3 February 2015
Published date: 25 March 2015
Organisations:
Aerodynamics & Flight Mechanics Group
Identifiers
Local EPrints ID: 374083
URI: http://eprints.soton.ac.uk/id/eprint/374083
ISSN: 0022-1120
PURE UUID: 6c31367f-e913-46b4-86c0-abb2adbe2b65
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Date deposited: 05 Feb 2015 15:34
Last modified: 15 Mar 2024 03:46
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Contributors
Author:
Bryn Jones
Author:
Peter Heins
Author:
Eric Kerrigan
Author:
Jonathan F. Morrison
Author:
Ati S. Sharma
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