Vibration control of flexible similar structures with detuned parameters

被引:0
|
作者
Luo Y. [1 ]
Xu M. [1 ]
Zhang S. [1 ]
Zhang X. [1 ]
机构
[1] State Key Lab for Strength and Vibration of Mechanical Structures, Xi'an Jiaotong University, Xi'an
来源
| 2017年 / Chinese Vibration Engineering Society卷 / 36期
关键词
Detuned parameters; Flexible similar structure; Modal localization; Vibration control;
D O I
10.13465/j.cnki.jvs.2017.23.003
中图分类号
学科分类号
摘要
Coupled dynamic modeling and vibration control of flexible similar structures with detuned parameters are important for designing aerospace structures. The coupled dynamic model of a system was established with Lagrange method and its responses were decoupled based on the least square method. Furthermore, the active vibration control model was built and simulated to study the suppression of unstable responses of flexible similar structures with detuned parameters. Finally, the system modal localization caused by detuned parameters was simulated and analyzed. According to vibration control simulation results, it was indicated that the proposed active vibration control method for flexible similar structures with detuned parameters based on their decoupled responses is effective. © 2017, Editorial Office of Journal of Vibration and Shock. All right reserved.
引用
收藏
页码:17 / 21
页数:4
相关论文
共 11 条
  • [1] Zhou Z., Lu Q., Ren G., Et al., On-orbit identification and vibration control for solar arrays with low and close frequencies, Engineering Mechanics, 24, 3, pp. 84-89, (2004)
  • [2] Xiao Y., Wang S., Chen G., The modal analysis for satellite-large space antenna system with finite element method(FEM), Machinery Design & Manufacture, 7, pp. 1-2, (2006)
  • [3] Bendiksen O.O., Mode localization phenomena in large space structures, AIAA Journal, 25, 9, pp. 1241-1248, (1987)
  • [4] Levine West M.B., Salamat M.A., Mode localization experiments on a ribbed antenna, AIAA Journal, 31, 10, pp. 1929-1937, (1993)
  • [5] Liao H., Wang S., Wang J., Et al., Tests for forced response localization of a mistuned bladed disk assembly, Journal of Vibration and Shock, 31, 1, pp. 30-34, (2012)
  • [6] Yang Z., Yang F., Mode localization prediction criterion for t-tail structure, Chinese Journal of Theoretical and Applied Mechanics, 42, 2, pp. 290-299, (2010)
  • [7] Yang F., Yang Z., Effects of mode localization on T-tail flutter characteristics, Journal of Vibration and Shock, 29, 8, pp. 1-4, (2010)
  • [8] Su J., Chen J., Characterization for mode localization level of weakly coupled mirroring symmetrical engineering structures with mistuned structural parameters, Journal of Vibration and Shock, 31, 7, pp. 118-121, (2012)
  • [9] Hu C., Li F., Zou J., Et al., A study on localization of vibration mode in mistuned bladed disk assemblims, Proceedings of the CSEE, 23, 11, pp. 190-194, (2003)
  • [10] Li F., Wang Y., Huang W., Et al., Advances of vibration localization in disordered periodic structures, Advances In Mechanics, 35, 4, pp. 498-512, (2005)