首页 | 本学科首页   官方微博 | 高级检索  
     

多轴振动试验控制的整型权函数法
引用本文:姜双燕,陈怀海,贺旭东,崔旭利.多轴振动试验控制的整型权函数法[J].振动与冲击,2011,30(9):136-144.
作者姓名:姜双燕  陈怀海  贺旭东  崔旭利
作者单位:飞行器结构力学与控制教育部重点实验室;南京航空航天大学振动工程研究所;南京 210016
基金项目:国家自然科学基金(10972104); 南京航空航天大学基本科研业务费专项科研项目资助(NS2010007)
摘    要:研究了应用于多轴向多激励随机振动控制的H∞整型控制方法,并且针对在频响函数矩阵病态的频率点处,响应自谱和互谱超出工程预定参考谱目标的情况,分解设计了H∞整型加权矩阵,从而改进频响函数矩阵病态情况,并对系统进行算法解耦。然后用整型矩阵对驱动信号的傅氏谱进行修正,进入控制回路迭代运算。实验验证表明,用文中算法设计整型权函数矩阵并修正驱动信号,可以有效的改善响应自谱和互谱的控制效果,抑制某些频率点处频响函数的不良影响。

关 键 词:回路整型设计    多轴向多激励    振动试验    振动控制  

Method of loop-shaping weighting functions for multi-axis vibration test control
JIANG Shuang-yan,CHEN Huai-hai,HE Xu-dong,CUI Xu-li.Method of loop-shaping weighting functions for multi-axis vibration test control[J].Journal of Vibration and Shock,2011,30(9):136-144.
Authors:JIANG Shuang-yan  CHEN Huai-hai  HE Xu-dong  CUI Xu-li
Affiliation:MOE Key Lab of Structure Mechanics and Control for Aircraft; Institute of Vibration Engineering Research; Nanjing University of Aeronautics and Astronautics; Nanjing, 210016; China
Abstract:H∞ loop-shaping control method is proposed in the paper for the MEMA(Multi Exciter/Multi Axis) random vibration test. In practice, the response spectrums of the control points are always difficult to meet the reference ones at the frequencies where the frequency response function matrices are ill-conditioned. An H∞ pre- compensator is decomposed and designd for the controller. The conditions of the frequecy response fucntion matrices are improved and the controlled plant is decoupled by an algorithm. The Fourier spectrum of the drive signal is shaped by the compensator in the control loop to replace the original one. The experiment shows that with the present method in this paper, the drive singal is mended, the response spectrums of the control points are improved because the poor conditions of the frequency response function at specified frequencies are rejected.
Keywords:loop-shaping design  multi-axis multi-exciter  vibration test  vibration control  
本文献已被 CNKI 等数据库收录!
点击此处可从《振动与冲击》浏览原始摘要信息
点击此处可从《振动与冲击》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号