Piezo patch sensor/actuator control of the vibrations of a cantilever under axial load

被引:14
作者
Sloss, JM [1 ]
Bruch, JC
Sadek, IS
Adali, S
机构
[1] Univ Calif Santa Barbara, Dept Math, Santa Barbara, CA 93106 USA
[2] Univ Calif Santa Barbara, Dept Mech & Environm Engn, Santa Barbara, CA 93106 USA
[3] Amer Univ Sharjah, Dept Mat & Stat, Sharjah, U Arab Emirates
[4] Univ Natal, Sch Mech Engn, ZA-4041 Durban, South Africa
基金
美国国家航空航天局; 美国国家科学基金会;
关键词
piezoelectric control; smart beams; axial loading; vibration control;
D O I
10.1016/j.compstruct.2003.09.015
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The effect of axial force in the vibration control of beams is studied by means of an integral equation formulation, which facilitates the numerical solution of the problem of finding the eigenfrequencies and eigenfunctions of a freely vibrating beam controlled by piezo patch sensors and actuators. The basic formulation of the problem is given in terms of a differential equation which is converted to an equivalent integral equation formulation by introducing an explicit Green's function. After approximating the kernel of the integral equation in terms of Fourier series based on the eigenfrequencies of the host structure, a method of solution is outlined which consists of expressing the integral equation as an infinite series of linear equations and using a finite of number of these equations in the numerical solution. Numerical results are obtained for different values of the gain, the axial load and for three patch sizes. The first three vibration frequencies of the controlled and uncontrolled beam are given. The tip deflections of the beam for different axial loads are also plotted to compare transient behaviour. (C) 2003 Elsevier Ltd. All rights reserved.
引用
收藏
页码:423 / 428
页数:6
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