DocumentCode
343349
Title
High-gain feedback control of surge and rotating stall in axial flow compressors
Author
Nayfeh, Mahir A. ; Abed, Eyad H.
Author_Institution
Dept. of Electr. Eng., Maryland Univ., College Park, MD, USA
Volume
4
fYear
1999
fDate
1999
Firstpage
2663
Abstract
The paper contributes to the understanding of bifurcation control of axial flow compressor stall phenomena. A high-gain feedback control design is presented that results in maximum steady-state pressure rise for a range of operating conditions beyond the surge line. Analysis and numerical results are presented to support the conclusions
Keywords
bifurcation; compressors; feedback; pressure control; stability; transient response; Moore Greitzer model; axial flow compressors; bifurcation control; feedback; pressure control; rotating stall; stability; surge; Bifurcation; Compressors; Control design; Control systems; Educational institutions; Feedback control; Pressure measurement; Stability analysis; Steady-state; Surges;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1999. Proceedings of the 1999
Conference_Location
San Diego, CA
ISSN
0743-1619
Print_ISBN
0-7803-4990-3
Type
conf
DOI
10.1109/ACC.1999.786553
Filename
786553
Link To Document