Modified Independent Modal Space Control for Large-Flexible Asymmetrical Resonant Structures

被引:0
作者
Zhang, Peng [1 ]
He, Fangpo [1 ]
机构
[1] Flinders Univ S Australia, Adv Control Syst Res Grp, Adelaide, SA, Australia
来源
2019 IEEE 10TH INTERNATIONAL CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING (ICMAE 2019) | 2019年
关键词
modified independent modal space control; multiple-input multiple-output; asymmetrical resonant structures; vibration suppression;
D O I
10.1109/icmae.2019.8881027
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents the design and implementation of a Modified Independent Modal Space Control (MIMSC) method for vibration suppression of multiple-input multiple-output asymmetrical resonant structures. The proposed method offers several important features over its classical counterpart. It can control any number of modes with a fixed number of sensors and actuators, reduces the computation load involved with the classical method, and provides flexible configurations to arrange the required input/output signals for controlling individual modes. Using a unique model module, the proposed method is potentially applicable to large-scale systems with distinctive vibration characteristics. The effectiveness of the proposed MIMSC method is validated via simulation and experimental studies on a given one-plane asymmetrical plate structure.
引用
收藏
页码:354 / 358
页数:5
相关论文
共 9 条