The advent of electronic controllers in the field of gas turbine control has allowed the implementation of sophisticated control algorithms. This paper proposes one such method, to design a controller using piecewise constant periodic output feedback, which has multifarious advantages, and because the states are not required for feedback, complete pole-assignability is guaranteed and the method is easily implementable.
Issue Section:
Gas Turbines: Controls, Diagnostics, and Instrumentation
1.
Watts
, J. W.
, Dwan
, T. E.
, and Brockus
, C. G.
, 1992
, “Optimal State-Space Control of a Gas Turbine Engine
,” ASME J. Eng. Gas Turbines Power
, 114
, pp. 763
–767
.2.
De Hoff, R. L., Hall, W. E., Adams, R. J., and Gupta, N. K., 1977, “F 100 Multivariable Control Synthesis,” Systems Control Inc., AFAPL-TR-77-35, Vol. I and II.
3.
Seller, J. F., and Danielle, C. J., 1975, “DYNGEN-A Program for Calculating Steady-State and Transient Performance of Turbo-Jet and Turbo-Fan Engines,” Lewis Research Center, NASA.
4.
Hackney, R. D., and Miller, R. J., 1977, “Engine Criteria and Models for Multivariable Control System Design,” AFAPL, OH.
5.
Chammas
, A. B.
, and Leondes
, C. T.
, 1979
, “Pole-Assignment by Piecewise Constant Output Feedback
,” Int. J. Control
, 29
(1
), pp. 31
–38
.6.
Werner
, H.
, and Furuta
, K.
, 1995
, “Simultaneous Stabilization Based on Output Measurement
,” Kybernetika
, 31
(4
), pp. 395
–411
.7.
Mahmoud, M. S., and Singh, M. G., 1981, Large Scale Systems Modeling, Pergamon Press, London.
8.
Lamba
, S. S.
, and Rao
, S. V.
, 1974
, “On Suboptimal Control via the Simplified Model of Davison
,” IEEE Trans. Autom. Control
, AC-19
, pp. 448
–450
.Copyright © 2003
by ASME
You do not currently have access to this content.
