• 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