Multi–Input Multi–Output Hybrid Active Vibration Control for High Frequency Random Vibration

被引:0
|
作者
A. Singh
M.S. Allen
M. Schmidt-Landin
W.J. DeLima
机构
[1] University of Wisconsin - Madison,
[2] Honeywell Federal Manufacturing & Technologies,undefined
来源
Experimental Techniques | 2022年 / 46卷
关键词
Modal test; Model calibration; MIMO active vibration control; Piezo actuators; Electromagnetic shakers;
D O I
暂无
中图分类号
学科分类号
摘要
Electromagnetic shakers and closed loop control systems are commonly used in qualification tests for environmental vibration conditions. However, shakers have resonances and anti-resonances at high frequencies. Resonances can be beneficial in that the shaker needs to exert less force to achieve the desired environment, but they can make it more challenging for the control system to match the desired environment. Anti-resonances are more problematic because they represent frequencies where the voltage input to the shaker causes little motion (at some locations on the slip table or adapter plate). Hence, these can cause the system to require driver voltage levels above the controller capacity and cause the test to abort and could even cause damage to the shaker. This paper proposes and characterizes a hybrid shaker system that uses piezoelectric actuator(s) in addition to the electromagnetic shaker to create a MIMO control system. It is hoped that the additional control effort introduced by the piezoelectric actuator can eliminate anti-resonances, expanding the frequency range over which the desired environment can be achieved. Furthermore, the actuators have very different capabilities as a function of frequency, and this is found to significantly reduce the control effort needed by the primary electromagnetic shaker.
引用
收藏
页码:67 / 79
页数:12
相关论文
共 50 条
  • [1] Multi-Input Multi-Output Hybrid Active Vibration Control for High Frequency Random Vibration
    Singh, A.
    Allen, M. S.
    Schmidt-Landin, M.
    DeLima, W. J.
    [J]. EXPERIMENTAL TECHNIQUES, 2022, 46 (01) : 67 - 79
  • [2] Multi-input Multi-output Active Vibration Control for High Frequency Random Vibration
    Singh, Aabhas
    Allen, Matt
    DeLima, Washington J.
    [J]. SPECIAL TOPICS IN STRUCTURAL DYNAMICS, VOL 5, 2019, : 37 - 47
  • [3] Limit strategy for multi-input multi-output random vibration control
    Zheng, Ronghui
    Xie, Wenwei
    Wei, Xiaohui
    Chen, Huaihai
    [J]. MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2023, 195
  • [4] Multi-input multi-output random vibration control using Tikhonov filter
    Cui Song
    Chen Huaihai
    He Xudong
    Zheng Wei
    [J]. Chinese Journal of Aeronautics, 2016, (06) : 1649 - 1663
  • [5] Multi-input multi-output random vibration control using Tikhonov filter
    Cui Song
    Chen Huaihai
    He Xudong
    Zheng Wei
    [J]. CHINESE JOURNAL OF AERONAUTICS, 2016, 29 (06) : 1649 - 1663
  • [6] Multi-input multi-output random vibration control using Tikhonov filter
    Cui Song
    Chen Huaihai
    He Xudong
    Zheng Wei
    [J]. Chinese Journal of Aeronautics., 2016, 29 (06) - 1663
  • [7] Investigation of multi-input multi-output sine on random mixed vibration control
    Ma, Yi
    Chen, Huaihai
    Zheng, Ronghui
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 2024, 238 (12) : 5565 - 5579
  • [8] Matrix power control algorithm for multi-input multi-output random vibration test
    MOE Key Laboratory of Structure Mechanics and Control for Aircraft, Institute of Vibration Engineering Research, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
    [J]. Chin J Aeronaut, 6 (741-748):
  • [9] Spectral decoupled correction algorithm for multi-input multi-output random vibration control
    Zheng, Ronghui
    Liu, Chuang
    Feng, Guosong
    Wei, Xiaohui
    Chen, Huaihai
    [J]. JOURNAL OF VIBRATION AND CONTROL, 2023,
  • [10] Matrix Power Control Algorithm for Multi-input Multi-output Random Vibration Test
    Cui Xuli
    Chen Huaihai
    He Xudong
    Jiang Shuangyan
    [J]. CHINESE JOURNAL OF AERONAUTICS, 2011, 24 (06) : 741 - 748