DocumentCode
2559103
Title
Control of compressor rotating stall without distributed sensing using bifurcation stabilization
Author
Sparks, Andrew ; Gu, Guoxiang
Author_Institution
Inst. of Technol., Wright-Patterson AFB, OH, USA
Volume
6
fYear
1997
fDate
4-6 Jun 1997
Firstpage
3716
Abstract
Control of rotating stall in axial compressors is considered. A local bifurcation stabilization theorem using the projection method for the case of an uncontrollable, unobservable critical mode is described and extended to control laws that do not vanish at the critical or bifurcation point. This result is used to derive sufficient conditions for several control laws to guarantee that the subcritical pitchfork bifurcation of an axial compressor model is made supercritical so that the rotating stall hysteresis is eliminated. Each of the control laws considers operation at a set point distinct from the critical point and depends only on annulus-averaged quantities as feedback variables to simplify sensing and signal processing requirements. A numerical example shows the transformation of the bifurcation from subcritical to supercritical and the elimination of the hysteresis region
Keywords
bifurcation; compressors; dynamics; feedback; gas turbines; hysteresis; series (mathematics); stability; Taylor series; axial compressors; bifurcation stabilization; dynamics; feedback; gas turbines; hysteresis; projection method; rotating stall control; subcritical bifurcation; sufficient conditions; supercritical bifurcation; Bifurcation; Differential equations; Engines; Feedback; Hysteresis; Partial differential equations; Signal processing; Sparks; Sufficient conditions; Turbines;
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.1997.609539
Filename
609539
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