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23540

Static Output Feedback Controller for Structural Acoustics System

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Last updated: 04 Jan 2025

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Abstract

This paper proposes designing an optimal static output feedback controller for a structural-acoustics coupled system as efficient control architecture. Modelling of sound transmission through a plate-cavity-plate system is presented. In this coupled structural acoustic system, an approximate series solution is assumed for the displacements of the plates and the pressure inside the cavity. The solution of the coupled system is obtained using Galarkin's method. The system to be modeled is consisting of a rectangular cavity with two flexible plates, one at the top of the cavity while the other at the bottom and four other fixed boundaries. Piezoelectric pair patches are considered to be bonded to the top plate, and each
pair is assumed to produce a pure moment actuation. The top plate is exposed to an external pressure excitation due to a planar wave generated by a sound source mounted above the cavity. Displacements at the mid points are calculated for the upper and lower plates. In the control scheme, the controller gains have been optimally tuned using genetic algorithms. The proposed architecture is compared to the linear quadratic Gaussian state feedback controller. The two controllers are compared for the time responses. The proposed controller shows a superior performance with simple implementation requirements.

DOI

10.21608/asat.2009.23540

Keywords

Active control, Static Output Feedback Controller, Structural Acoustic System

Authors

First Name

M.

Last Name

Gharib

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Affiliation

Lecturer Assistant, Aerospace Engineering Department, Cairo University, Cairo, Egypt.

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First Name

A.

Last Name

Omran

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Affiliation

Lecturer Assistant, Aerospace Engineering Department, Cairo University, Cairo, Egypt.

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Orcid

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First Name

G.

Last Name

El-Bayoumi

MiddleName

-

Affiliation

Professor, Aerospace Engineering Department, Cairo University, Cairo, Egypt.

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Volume

13

Article Issue

AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT- 13, May 26 – 28, 2009

Related Issue

4377

Issue Date

2009-05-01

Receive Date

2019-01-03

Publish Date

2009-05-01

Page Start

1

Page End

17

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_23540.html

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https://asat.journals.ekb.eg/service?article_code=23540

Order

43

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Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

Static Output Feedback Controller for Structural Acoustics System

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Article

Created At

22 Jan 2023