Active Control Optimization for Minimizing the Dynamic Response of Functionally Graded Plate

A control optimization problem for functionally graded (FG) plates is presented using a first-order shear deformation plate theory including through-the-thickness normal strain effect. The aim of the optimization is to minimize the vibrational response of FG plate with constraints on the control ene...

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Main Authors: M. E. Fares, M. Kh. Elmarghany, Doaa Atta
Format: Article
Language:English
Published: Hindawi Limited 2014-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2014/516303
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spelling doaj-fd1a6d6ed03646a6ba1ed90f8b16a7302020-11-24T23:00:47ZengHindawi LimitedInternational Journal of Aerospace Engineering1687-59661687-59742014-01-01201410.1155/2014/516303516303Active Control Optimization for Minimizing the Dynamic Response of Functionally Graded PlateM. E. Fares0M. Kh. Elmarghany1Doaa Atta2Department of Mathematics, Faculty of Science, Mansoura University, Mansoura 35516, EgyptDepartment of Mathematics, Faculty of Science, Mansoura University, Mansoura 35516, EgyptDepartment of Mathematics, Faculty of Science, Mansoura University, Mansoura 35516, EgyptA control optimization problem for functionally graded (FG) plates is presented using a first-order shear deformation plate theory including through-the-thickness normal strain effect. The aim of the optimization is to minimize the vibrational response of FG plate with constraints on the control energy used in the damping process. An active control optimization is presented to determine the optimal level of a closed loop control function. Plate thickness and a homogeneity parameter of FG plates are used as design variables. Numerical results for the optimal control force and the total energy for a simply supported FG plate are given. The influence of through-the-thickness normal strain effect on the accuracy of the obtained results is illustrated. The effectiveness of the present control and design procedure is examined.http://dx.doi.org/10.1155/2014/516303
collection DOAJ
language English
format Article
sources DOAJ
author M. E. Fares
M. Kh. Elmarghany
Doaa Atta
spellingShingle M. E. Fares
M. Kh. Elmarghany
Doaa Atta
Active Control Optimization for Minimizing the Dynamic Response of Functionally Graded Plate
International Journal of Aerospace Engineering
author_facet M. E. Fares
M. Kh. Elmarghany
Doaa Atta
author_sort M. E. Fares
title Active Control Optimization for Minimizing the Dynamic Response of Functionally Graded Plate
title_short Active Control Optimization for Minimizing the Dynamic Response of Functionally Graded Plate
title_full Active Control Optimization for Minimizing the Dynamic Response of Functionally Graded Plate
title_fullStr Active Control Optimization for Minimizing the Dynamic Response of Functionally Graded Plate
title_full_unstemmed Active Control Optimization for Minimizing the Dynamic Response of Functionally Graded Plate
title_sort active control optimization for minimizing the dynamic response of functionally graded plate
publisher Hindawi Limited
series International Journal of Aerospace Engineering
issn 1687-5966
1687-5974
publishDate 2014-01-01
description A control optimization problem for functionally graded (FG) plates is presented using a first-order shear deformation plate theory including through-the-thickness normal strain effect. The aim of the optimization is to minimize the vibrational response of FG plate with constraints on the control energy used in the damping process. An active control optimization is presented to determine the optimal level of a closed loop control function. Plate thickness and a homogeneity parameter of FG plates are used as design variables. Numerical results for the optimal control force and the total energy for a simply supported FG plate are given. The influence of through-the-thickness normal strain effect on the accuracy of the obtained results is illustrated. The effectiveness of the present control and design procedure is examined.
url http://dx.doi.org/10.1155/2014/516303
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