航空学报 > 2003, Vol. 24 Issue (2): 140-143

有理分式正交多项式频响函数模态参数识别

王彤, 张令弥   

  1. 南京航空航天大学振动工程研究所 江苏南京 210016
  • 收稿日期:2002-04-03 修回日期:2002-06-12 出版日期:2003-04-25 发布日期:2003-04-25

Modal Identification with Frequency Response Function Based on Rational Fraction Orthogonal Polynomials

WANG Tong, ZHANG Ling-mi   

  1. Institute of Vibration Engineering; Nanjing University of Aeronauti cs and Astronautics; Nanjing 210016; China
  • Received:2002-04-03 Revised:2002-06-12 Online:2003-04-25 Published:2003-04-25

摘要: 讨论一种多输入的频域模态参数识别方法。该方法将频响函数表示为具有矩阵系数的有理分式,利用Forsythe 正交多项式减少方程的病态并解耦系统矩阵,随后运用特征值与奇异值分解求解系统的极点与留数。使用欧洲国家航空界广泛使用的GARTEUR 飞机模型进行仿真计算。结果表明:该方法在30 %噪声下仍具有对严重耦合模态的识别能力;振型识别较为准确;适当提高分母阶次能取得更好的识别结果。

关键词: 模态识别, 多输入多输出, 有理分式, 正交多项式, 频响函数

Abstract: This paper discusses a multiple-input modal identification method in the frequency domain. The frequencyresponse function (FRF) is expressed as a rational fraction formulation with matrix coefficients. The Forsytihe orthogonal polynomial is exploited to reduce the ill-conditioning of the equations and to decouple the system matrix.Taking use of the eigenvalue decomposition and singular value decomposition, the poles and residues of the systemare solved. An aircraft model called GARTEUR, which is widely used in European aerospace community, is takento test this algorithm. It was proved that this method is good for heavily coupled modes even polluted by high noiselevels (up to 30 %) . Good modal identification results are obtained, which can be further improved while higher order of the denominator polynomials is used.

Key words: modal identification, multiple input multiple output, orthogonal polynomials, frequency response function, rational fraction

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