Sensor/actuator optimal design for active vibration control of shell structure

被引:1
|
作者
Kim, SJ [1 ]
Hwang, JS [1 ]
Mok, J [1 ]
机构
[1] Seoul Natl Univ, Dept Aerosp Engn, Seoul 151742, South Korea
关键词
active vibration control; shell structure; sensor/actuator system; finite element method; genetic algorithm;
D O I
10.1117/12.388874
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this paper, a method based on finite element technique is developed for the design of sensor/actuator system of the active vibration control of shell structure. To prevent the adverse effect of spillover, distributed modal sensor/actuator system is established using PVDF film. Although shell structure is three-dimensional structure, the PVDF sensor/actuator system can be treated as two-dimensional. The electrode patterns and lamination angle of PVDF sensor/actuator are optimized to design the modal sensor/actuator system. Finite element programs are developed to consider curved structures having PVDF modal sensor/actuator. The nice-node shell element with five nodal degree of freedoms is used for finite element discretization. Electrode patterns and lamination angles of PVDF sensor/actuator are optimized using genetic algorithm. Sensor is designed to minimize the observation spillover, and actuator is designed to minimize the system energy of the control modes under a given initial condition. Modal sensor/actuator for the first and second modes of singly curved cantilevered shell structure are designed using above mentioned methods. For the demonstration, numerical simulation of the closed loop system is performed. Discrete LQG method is used as a control law.
引用
收藏
页码:594 / 602
页数:9
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