Quick Search Adv Search
   Home  About Journal  Editorial Board  Instruction  Subscription  Download  Message  Contact
JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A 2006, Vol. 32 Issue (01) :18-21    DOI:
论文 Current Issue | Next Issue | Archive | Adv Search << | >>
Vibration control design and simulation method for complex structures
Luo Xiaoping, Huang Hai, Xian Kuicheng*
School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

Abstract
Reference
Related Articles
Download: PDF (0KB)   HTML 1KB   Export: BibTeX or EndNote (RIS)      Supporting Info
Abstract A new vibration control design method based on FEM (finite element method) was proposed for structures to avoid the model error due to simplification and model reduction, in order to solve the difficulty of complex structures modeling and to improve the accuracy of the control design. The method could be implemented easily with the help of commercial FEM analysis softwares. A universal control simulation interface was established in structure analysis package PATRAN/NASTRAN environment with the programmable PCL (patran command language). The effectiveness of the method was demonstrated through the PCL simulation and experimental validation of the vibration control of a piezoelectric adaptive truss structure. The numerical result of the new technology agrees better with the experimental data when compared with Simulink simulation using simplified model. The new FEM method is proved to be more accurate and suitable for the control design simulation and evaluation of complex structures in design stage.
Service
Email this article
Add to my bookshelf
Add to citation manager
Email Alert
RSS
Articles by authors
Keywordsstructure   vibration control   finite element method   simulation     
Received 2004-10-29;
About author:
Cite this article:   
Luo Xiaoping, Huang Hai, Xian Kuicheng.Vibration control design and simulation method for complex structures[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2006,V32(01): 18-21
URL:  
http://bhxb.buaa.edu.cn//EN/     or     http://bhxb.buaa.edu.cn//EN/Y2006/V32/I01/18
Copyright 2010 by JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A