Title of article
Finite element analysis and distributed control of laminated composite shells using LQR/IMSC approach
Author/Authors
Bhattacharya، نويسنده , , Partha and Suhail، نويسنده , , Hassan and Sinha، نويسنده , , Prasanta K.، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2002
Pages
9
From page
273
To page
281
Abstract
In the present study a shear deformable shell element is developed based on Reissnerʹs hypothesis for the analysis of smart laminated composite shells. The electric field is defined in the curvilinear co-ordinate system. The mathematics of arbitrary shell geometry is amenable to the flexible mapping characteristic of the finite element formulation developed in the present work. Lameʹs parameters and the radii of curvature are generated within the model. An IMSC based LQR control methodology is adopted for the active vibration control of laminated spherical shell with different fibre orientation and varying radius of curvature. Results are presented and are discussed.
Keywords
smart structure , Laminated shell , Linear quadratic regulator , Finite element
Journal title
Aerospace Science and Technology
Serial Year
2002
Journal title
Aerospace Science and Technology
Record number
2228985
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