THE APPLICATION OF A FINITE SHELL ELEMENT FOR COMPOSITES CONTAINING PIEZOELECTRIC POLYMERS IN VIBRATION CONTROL

被引:101
作者
LAMMERING, R
机构
[1] Institut für Aeroelastik, Deutsche Forschungsanstalt für Luft- und Raumfahrt, D-3400 Göttingen
关键词
D O I
10.1016/0045-7949(91)90305-6
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
Advanced composite structures with integrated sensors and actuators are becoming increasingly important due to the demand for very large, low-mass space structures. This paper focuses on the finite element analysis of shell structures with thin piezo-electric layers bonded to the surfaces. A finite element formulation taking the piezo-electric effect into account is given and a finite shell element is presented, allowing for the computation of these advanced composite structures. The dynamic matrix equation accounting for the piezo-electric material response is formulated and found to have the same form as the well-known equation of structural dynamics. By using the second or direct method of Lyapunov, a control law is derived, which is used in vibration control and ensures asymptotic stability. A numerical example is given to show the accuracy of the finite element, as well as the efficiency of the algorithm.
引用
收藏
页码:1101 / 1109
页数:9
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