DocumentCode :
3406480
Title :
Effects of the shape of compressor characteristics on actuator requirements for rotating stall control
Author :
Wang, Yong ; Murray, Richard M.
Author_Institution :
Div. of Eng. & Appl. Sci., California Inst. of Technol., Pasadena, CA, USA
Volume :
4
fYear :
1998
fDate :
21-26 Jun 1998
Firstpage :
1996
Abstract :
We present a systematic analysis on the effects of noise, the shape of compressor characteristics, and bleed valve actuator limits on the performance of controllers in rotating stall control. We use center manifold reduction to the three state Moore Greitzer model with piecewise analytic compressor characteristics. For the reduced system, the optimal control which achieves the largest operability enhancement is the “bang-on” control law that drives the valve to open against its rate limit. For the optimal controller, we also derive approximate formulas for the operability enhancement as a function of the noise level, the actuator limits, and the shape of compressor characteristics. The predictions by the formulas are compared with numerical simulations using a model for a low speed axial compressor
Keywords :
actuators; aerospace engines; compressors; control system synthesis; optimal control; valves; actuator requirements; bang-on control law; bleed valve actuator limits; compressor characteristics; low speed axial compressor; noise level; operability enhancement; optimal control; rotating stall control; systematic analysis; three state Moore Greitzer model; Actuators; Control systems; Noise level; Noise shaping; Numerical simulation; Optimal control; Performance analysis; Predictive models; Shape control; Valves;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1998. Proceedings of the 1998
Conference_Location :
Philadelphia, PA
ISSN :
0743-1619
Print_ISBN :
0-7803-4530-4
Type :
conf
DOI :
10.1109/ACC.1998.702975
Filename :
702975
Link To Document :
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