DocumentCode :
2559270
Title :
Surge control and test functions for axial flow compressors
Author :
Kang, Wei ; Guoxiang Gu ; Sparks, Andy ; Banda, Siva
Author_Institution :
Dept. of Math., Naval Postgraduate Sch., Monterey, CA, USA
Volume :
6
fYear :
1997
fDate :
4-6 Jun 1997
Firstpage :
3721
Abstract :
The focus of this paper is bifurcation control for axial flow engine compressors. The Moore-Greitzer model is adopted for the analysis. We introduce test functions whose zeros are critical to Hopf bifurcation for the closed-loop system where nonlinear feedback control laws are employed. A test function is also developed to determine the stability of the periodic solutions born at Hopf bifurcation. The analysis based on these test functions leads to a new method of feedback design for control of both stationary and Hopf bifurcation in axial flow compressors. Using the techniques proposed, feedback controllers can be designed to meet several bifurcation control requirements, including elimination of the behavior of surge, coupled with rotating stall
Keywords :
aerospace engines; aerospace testing; bifurcation; closed loop systems; compressors; nonlinear control systems; stability; state feedback; transient response; Hopf bifurcation; Moore-Greitzer model; aeroengines; axial flow compressors; bifurcation control; closed-loop system; nonlinear control systems; stability; state feedback; surge control; Bifurcation; Compressors; Ducts; Engines; Feedback control; Hysteresis; Stability; State feedback; Surges; System testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1997. Proceedings of the 1997
Conference_Location :
Albuquerque, NM
ISSN :
0743-1619
Print_ISBN :
0-7803-3832-4
Type :
conf
DOI :
10.1109/ACC.1997.609540
Filename :
609540
Link To Document :
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