Reference : Shape signifiers for throttle control of a low-order compressor model

	Document type :	Scientific journals : Article
	Discipline(s) :	Engineering, computing & technology : Electrical & electronics engineering
	To cite this reference:	http://hdl.handle.net/2268/78065

Title :	Shape signifiers for throttle control of a low-order compressor model
Language :	English
Author, co-author :	Sepulchre, Rodolphe [Université de Liège - ULg > Dép. d'électric., électron. et informat. (Inst.Montefiore) > Systèmes et modélisation >]
	Kokotovic, Petar [ > > ]
Publication date :	Nov-1998
Journal title :	IEEE Transactions on Automatic Control
Publisher :	IEEE
Volume :	43
Issue/season :	11
Pages :	1643-1648
Peer reviewed :	Yes (verified by ORBi)
ISSN :	0018-9286
City :	Piscataway
Country :	NJ
Keywords :	[en] Aeroengine instabilities ; compressor characteristics ; Moore–Greitzer model
Abstract :	[en] Rotating stall and surge, two instability mechanisms limiting the performance of aeroengines compressors, are studied on the third-order Moore–Greitzer model. The skewness of the compressor characteristic, a single parameter shape signifier, is shown to determine the key qualitative properties of feedback control.
Permalink :	http://hdl.handle.net/2268/78065
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