DocumentCode :
1707139
Title :
Modeling and adaptive analysis for nonlinear system based on system equilibrium manifold expansion model
Author :
Liu Xiao-feng
Author_Institution :
Sch. of Transp. Sci. & Technol., Beihang Univ., Beijing, China
fYear :
2013
Firstpage :
1889
Lastpage :
1894
Abstract :
System´s equilibrium manifold is basically one nonlinear approximate model. And modeling error was determined by the mapping method of equilibrium manifold expansion model. In this paper, a system equilibrium manifold expansion model was proposed, and throughout the identification and calculation a deterioration equilibrium manifold expansion model of two-spool turbofan engine high-pressure compressor was developed. Simulations compared with nonlinear component-level model of this type turbofan engine showed the same modeling accuracy with nonlinear model. This model can further enhance the onboard estimation of aero engine.
Keywords :
aerospace engineering; aerospace engines; approximation theory; nonlinear systems; aero engine estimation; deterioration equilibrium manifold expansion model; modeling error; nonlinear approximate model; nonlinear component-level model; nonlinear system adaptive analysis; nonlinear system modeling; system equilibrium manifold expansion model; two-spool turbofan engine high-pressure compressor; Adaptation models; Analytical models; Atmospheric modeling; Educational institutions; Engines; Manifolds; Nonlinear systems; Aircraft Engine; Equilibrium Manifold; Expansion Model; Model Adaptivity; Nonlinear System;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2013 32nd Chinese
Conference_Location :
Xi´an
Type :
conf
Filename :
6639735
Link To Document :
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