Active Control Optimization for Minimizing the Dynamic Response of Functionally Graded Plate. (27th October 2014)

• Record Type: Journal Article
• Authors: Fares, M. E.; Elmarghany, M. Kh.; Atta, Doaa
• Other Names: Barrett Ronald M. Academic Editor.
• Is Part Of: International journal of aerospace engineering. Volume 2014(2014)
• Publication Date: 2014-10-27
• Subjects: Aerospace engineering -- Periodicals; 629.105
• DOI: 10.1155/2014/516303
• Languages: English
• ISSNs: 1687-5966

Abstract

Abstract : 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.