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�������պ����ѧѧ�� 2006, Vol. 32 Issue (01) :18-21    DOI:
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����ƽ, �ƺ�, �̿���*
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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

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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.
Keywords�� structure   vibration control   finite element method   simulation     
Received 2004-10-29;


About author: ����ƽ(1967-),��,������ˮ��,������, aidong67@163.com.
����ƽ, �ƺ�, �̿���.���ӽṹ�񶯿����������淽���о�[J]  �������պ����ѧѧ��, 2006,V32(01): 18-21
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
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