Rejecting multiple-period disturbances: active vibration control of a two degree-of-freedom piezoelectric flexible structure system

2014 ◽  
Vol 21 (16) ◽  
pp. 3368-3382 ◽  
Author(s):  
Chi-Ying Lin ◽  
Wei-Hsiang Chiu ◽  
Jonqlan Lin
2011 ◽  
Vol 19 (2) ◽  
pp. 284-296 ◽  
Author(s):  
Jan-Willem van Wingerden ◽  
Anton Hulskamp ◽  
Thanasis Barlas ◽  
Ivo Houtzager ◽  
Harald Bersee ◽  
...  

2001 ◽  
Vol 37 (6) ◽  
pp. 502-509
Author(s):  
Hiroaki FUKUSHIMA ◽  
Yue WU ◽  
Toshiharu SUGIE ◽  
Gi-Hwan BAE ◽  
Yoshiyuki SUZUKI

Aerospace ◽  
2006 ◽  
Author(s):  
H. F. Lam ◽  
W. H. Liao

Transmissibilities for two-degree-of-freedom (2DoF) passive systems have been extensively investigated in the past. However, for semi-active control systems, the transmissibilities are rarely analyzed. The expressions of non-dimensional transmissibilities for the semi-active control systems are not found. There are no closed-form transfer functions for general semi-active control systems. The control algorithms for semi-active systems need to be specified first. Therefore, three reference systems (skyhook, groundhook, and their hybrid) are proposed. These equivalent systems are the references for the semi-active control systems to achieve. In this paper, the 2DoF skyhook, groundhook and hybrid systems for semi-active control are studied. The displacement and acceleration transmissibilities of those three reference systems are formulated and analyzed. Their transmissibilities are also compared with the passive system. Each of reference systems is classified as Ideal and Non-Ideal systems. The differences between the Ideal and Non-Ideal systems are also discussed. The optimal systems and their corresponding parameters are identified.


2016 ◽  
Vol 2016 ◽  
pp. 1-8 ◽  
Author(s):  
Xianjun Sheng ◽  
Yuanli Kong ◽  
Fengyun Zhang ◽  
Rui Yang

Flexible structures have been widely used in many fields due to the advantages of light quality, small damping, and strong flexibility. However, flexible structures exhibit the vibration in the process of manipulation, which reduces the pointing precision of the system and causes fatigue of the machine. So, this paper focuses on the identification method for active vibration control of flexible structure. The modal parameters and transfer function of the system are identified from the step response signal based on Prony algorithm, while the vibration is attenuated by using the input shaping technique designed according to the parameters identified from the Prony algorithm. Eventually, the proposed approach is applied to the most common flexible structure, a piezoelectric cantilever beam actuated by Macro Fiber Composite (MFC). The experimental results demonstrate that the Prony algorithm is very effective and accurate on the dynamic modeling of flexible structure and input shaper could significantly reduce the vibration and improve the response speed of system.


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