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

Sepulchre, Rodolphe; Kokotovic, Petar

doi:10.1109/9.728888

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

Sepulchre, Rodolphe; Kokotovic, Petar

1998 • In IEEE Transactions on Automatic Control, 43 (11), p. 1643-1648

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https://hdl.handle.net/2268/78065

DOI
10.1109/9.728888

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Keywords :

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.

Disciplines :

Electrical & electronics engineering

Author, co-author :

Sepulchre, Rodolphe ; Université de Liège - ULiège > Dép. d'électric., électron. et informat. (Inst.Montefiore) > Systèmes et modélisation

Kokotovic, Petar

Language :

English

Title :

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

Publication date :

November 1998

Journal title :

IEEE Transactions on Automatic Control

ISSN :

0018-9286

Publisher :

IEEE, Piscataway, United States - New Jersey

Volume :

Issue :

Pages :

1643-1648

Peer reviewed :

Peer Reviewed verified by ORBi

Available on ORBi :

since 29 November 2010

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Bibliography

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