DocumentCode
294355
Title
Backstepping designs for jet engine stall and surge control
Author
Krstic, M. ; Protz, J.M. ; Paduano, J.D. ; Kokotovic, P.V.
Author_Institution
Dept. of Mech. Eng., Maryland Univ., College Park, MD, USA
Volume
3
fYear
1995
fDate
13-15 Dec 1995
Firstpage
3049
Abstract
A new systematic method for nonlinear control design-backstepping-is applied to low-order compression system models. Backstepping achieves global asymptotic stability of both stall and surge in the presence of large uncertainties in the compressor model. Throughout our presentation, we explore the control design implications of the nonlinear equilibrium properties of compressors
Keywords
aerospace engines; asymptotic stability; compressors; control system synthesis; nonlinear control systems; backstepping designs; compressors; global asymptotic stability; jet engine stall control; jet engine surge control; low-order compression system models; nonlinear control design; nonlinear equilibrium properties; Asymptotic stability; Backstepping; Bifurcation; Ducts; Educational institutions; Fluid dynamics; Jet engines; Shape control; Surges; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1995., Proceedings of the 34th IEEE Conference on
Conference_Location
New Orleans, LA
ISSN
0191-2216
Print_ISBN
0-7803-2685-7
Type
conf
DOI
10.1109/CDC.1995.478612
Filename
478612
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