DocumentCode
2661516
Title
Flutter modal identification with frequency-based least squares estimator using vector orthogonal polynomials
Author
Wei, Tang
Author_Institution
Coll. of Autom., Northwestern Polytech. Univ., Xian
fYear
2008
fDate
16-18 July 2008
Firstpage
265
Lastpage
269
Abstract
Frequency-based least squares (LS) estimators are widely used tools for flutter modal identification of aircraft. These methods are known to suffer from a poor numerical condition when the frequency spans or model order becomes large. A new approach using vector orthogonal polynomial basis is employed in this paper to solve the problem, The key idea of this method is to represent the frequency response function (FRF) matrix in a left matrix fraction description (LMFD) model, and expand the numerator and denominator polynomial matrices in a vector orthogonal basis. As a result, a perfect numerical condition (numerical condition=1) can be obtained for linear least squares estimator. Finally, the efficiency of the approach is illustrated by means of real flight test data.
Keywords
aircraft testing; elasticity; frequency response; least squares approximations; parameter estimation; polynomial matrices; vehicle dynamics; aircraft; flutter modal identification; frequency response function matrix; frequency-based least squares estimator; left matrix fraction description model; linear least squares estimator; polynomial matrices; vector orthogonal polynomials; Aircraft; Atmospheric measurements; Frequency domain analysis; Frequency estimation; Frequency response; Least squares approximation; Parameter estimation; Polynomials; Testing; Vectors; Frequency domain; LS estimator; Numerical condition;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference, 2008. CCC 2008. 27th Chinese
Conference_Location
Kunming
Print_ISBN
978-7-900719-70-6
Electronic_ISBN
978-7-900719-70-6
Type
conf
DOI
10.1109/CHICC.2008.4605239
Filename
4605239
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