Sepulchre, R and Kokotovic, P (1998) Shape signifiers for control of a low-order compressor model. IEEE Transactions on Automatic Control, 43. pp. 1643-1648. ISSN 0018-9286Full text not available from this repository.
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.
|Divisions:||Div F > Control|
|Depositing User:||Cron Job|
|Date Deposited:||18 May 2016 19:16|
|Last Modified:||25 May 2016 00:38|