DocumentCode :
2195302
Title :
On the identification of a nonlinear function in a feedback loop
Author :
Mehta, Prashant G. ; Banaszuk, Andrzej
Author_Institution :
Center for Appl. Math., Cornell Univ., Ithaca, NY, USA
Volume :
5
fYear :
2001
fDate :
2001
Firstpage :
4320
Abstract :
Many models of systems, important in practice have the form of an interconnection of a known linear model and an unknown nonlinear function. One example of such a system is a model of thermoacoustic instability affecting gas turbine engines and rockets (so-called thermoacoustic feedback loop). In this paper, we propose a computationally attractive algorithm for identifying static nonlinearity in a thermoacoustic feedback loop which is either in a limit cycle or is being, driven by Gaussian noise. The algorithm is based upon functional analytic treatment of the describing function method and lends itself nicely to a class of limit cycling or noise driven feedback systems where the nonlinearity is of a special type. We present examples as well as a simulations with the thermoacoustic feedback loop as an application of the identification algorithm
Keywords :
Gaussian noise; computational complexity; feedback; gas turbines; identification; limit cycles; nonlinear functions; rockets; thermal stability; Gaussian noise; computationally attractive algorithm; describing function; feedback loop; functional analytic treatment; gas turbine engines; identification; interconnection; known linear model; limit cycle; noise driven feedback systems; nonlinear function; rockets; static nonlinearity identification; thermoacoustic feedback loop; thermoacoutic instability; unknown nonlinear function; Combustion; Delay; Engines; Feedback loop; Gaussian noise; Limit-cycles; Mathematical model; Noise shaping; Shape; Turbines;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 2001. Proceedings of the 40th IEEE Conference on
Conference_Location :
Orlando, FL
Print_ISBN :
0-7803-7061-9
Type :
conf
DOI :
10.1109/.2001.980880
Filename :
980880
Link To Document :
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