DocumentCode :
1104330
Title :
The suppression of drift and transient effects for frequency-domain identification
Author :
McCormack, Anthony S. ; Flower, John O. ; Godfrey, Keith R.
Author_Institution :
Dept. of Eng., Warwick Univ., Coventry, UK
Volume :
43
Issue :
2
fYear :
1994
fDate :
4/1/1994 12:00:00 AM
Firstpage :
232
Lastpage :
237
Abstract :
The identification of linear system dynamics from measurements corrupted by low-frequency aperiodic noise is discussed for situations where a periodic excitation can be applied to the system. It is shown that, by considering the low-frequency harmonic content of the disturbing noise, accurate elimination of the disturbance can be achieved for typical linear/nonlinear trend characteristics. The removal of transient effects from the initial response of the system to the excitation is also discussed. This is applicable when the experimental time is limited, as can be the case for systems with long time constants. The removal of the transient effects can be coupled with estimation of the drift parameters, thus allowing the effects of both the transients and the drift to be removed simultaneously
Keywords :
control system synthesis; fast Fourier transforms; frequency-domain synthesis; harmonic analysis; identification; interference (signal); interference suppression; interpolation; linear systems; noise; signal processing; transients; disturbing noise; drift parameters; drift suppression; excitation; frequency-domain identification; identification; interpolation; linear system dynamics; linear/nonlinear trend characteristics; low-frequency aperiodic noise; low-frequency harmonic content; time constants; transient effects; Control system synthesis; Control systems; Frequency estimation; Helium; Linear systems; Low-frequency noise; Noise measurement; Process control; Signal design; Signal processing;
fLanguage :
English
Journal_Title :
Instrumentation and Measurement, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9456
Type :
jour
DOI :
10.1109/19.293426
Filename :
293426
Link To Document :
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