Title :
Shape signifiers for control of a low-order compressor model
Author :
Sepulchre, Rodolphe ; Kokotovic, Petar
Author_Institution :
Inst. Montefiore, Liege Univ., Belgium
fDate :
11/1/1998 12:00:00 AM
Abstract :
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
Keywords :
aerospace engines; compressors; feedback; stability; transients; Moore-Greitzer model; aeroengines; compressors; feedback; instability; jet engines; low-order compressor model; rotating stall; shape signifier; skewness; surge; throttle control; Aerodynamics; Control systems; Differential equations; Feedback control; Hysteresis; Jet engines; Nonlinear control systems; Performance loss; Shape control; Surges;
Journal_Title :
Automatic Control, IEEE Transactions on
