• DocumentCode
    2372792
  • Title

    Parameter identification for a triaxial shaker system

  • Author

    Dougherty, John J. ; El-Sherief, Hossny

  • Author_Institution
    TRW Syst. Integration Group, San Bernardino, CA, USA
  • fYear
    1996
  • fDate
    15-18 Sep 1996
  • Firstpage
    558
  • Lastpage
    563
  • Abstract
    Different approaches to parameter identification for a triaxial shaker system are examined. One approach uses an output error formulation of a cost function, which is then minimized using a standard algorithm. Two other approaches use a cost function defined through an input error formulation. The cost function is minimized through, alternately, a standard function minimization algorithm and a linearized least-squares algorithm. For the case of fewer measurements than degrees of freedom, a generalized technique for reconstructing the states is proposed. This technique does not make any assumptions regarding the absence of external forces on unmeasured degrees of freedom. The three approaches to parameter identification are compared for two different systems
  • Keywords
    aerospace test facilities; dynamic testing; least squares approximations; minimisation; parameter estimation; testing; United States Air Force; cost function minimization; linearized least-squares algorithm; output error formulation; parameter identification; state reconstruction; triaxial shaker system; vibration testing; Analytical models; Cost function; Frequency domain analysis; Frequency measurement; Frequency response; Minimization methods; Nonlinear equations; Parameter estimation; Shape measurement; Time domain analysis;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications, 1996., Proceedings of the 1996 IEEE International Conference on
  • Conference_Location
    Dearborn, MI
  • Print_ISBN
    0-7803-2975-9
  • Type

    conf

  • DOI
    10.1109/CCA.1996.558921
  • Filename
    558921