Article ID Journal Published Year Pages File Type
755669 Chinese Journal of Aeronautics 2006 8 Pages PDF
Abstract

The aim of this paper is to present a new method for flight flutter modal parameter identification in noisy environment. This method employs a time frequency (TF) filter to reduce the noise before identification, which depends on the localization property of sweep excitation in TF domain. Then, a generalized total least square (GTLS) identification algorithm based on stochastic framework is applied to the enhanced data. System identification with noisy data is transformed into a generalized total least square problem, and the solution is carried out by the generalized singular value decomposition (GSVD) to avoid the intensive nonlinear optimization computation. A nearly maximum likelihood property can be achieved by ‘optimally’ weighted generalized total least square. Finally, the efficiency of the method is illustrated by means of flight test data.

Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering