Title :
Flutter modal identification with frequency-based least squares estimator using vector orthogonal polynomials
Author_Institution :
Coll. of Autom., Northwestern Polytech. Univ., Xian
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;
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
DOI :
10.1109/CHICC.2008.4605239