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
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