Vibration control of spacecraft box structures using a collocated piezo-actuator/sensor

被引：1
|
作者：
Damaren, CJ
Oguamanam, DCD
机构：
[1] Univ Toronto, Inst Aerosp Studies, Toronto, ON M3H 5T6, Canada
[2] Ryerson Univ, Dept Mech & Ind Engn, Toronto, ON M5B 2K3, Canada
来源：
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES | 2004年 / 15卷 / 05期
关键词：
smart structures; box structures; collation; strictly positive real;
D O I：
10.1177/1045389X04040901
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
The problem of vibration control in box-type structures is examined by inclusion of piezo-electric smart structural elements. The box is modeled as a system of joined plates in which both extensional and bending deflections are incorporated. By collocating the sensor and actuator elements, the input-output property of passivity is achieved independent of the number of modeled modes and details such as frequencies and mode shapes. Robust vibration control is achieved by designing a strictly positive real dynamic compensator for the system.
引用
收藏
页码：369 / 374
页数：6
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