Model reduction and MIMO model predictive control of gas turbine systems

被引:39
作者
Wiese, A. P. [1 ]
Blom, M. J. [1 ]
Manzie, C. [1 ]
Brear, M. J. [1 ]
Kitchener, A. [2 ]
机构
[1] Univ Melbourne, Dept Mech Engn, Parkville, Vic 3052, Australia
[2] SVW Pty Ltd, Spotswood, Vic, Australia
关键词
Gas turbines; MIMO control; Model predictive control; Model reduction; POWER-SYSTEM; DESIGN; MPC;
D O I
10.1016/j.conengprac.2015.09.015
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper presents the development and experimental implementation of an online, fully nonlinear model predictive controller (NMPC) for a gas turbine. The reduced-order, internal model used in the controller was developed from an original high-order, physics,based model using rigorous time scale separation arguments that may be extended to any gas turbine system. A control problem for a prototype gas turbine system is then formulated as a MIMO optimisation problem that may be addressed through NMPC. The controller objective is to regulate compressor exit pressure while tracking compressor bleed demand. The constraint set includes the range of the control actuators, the valid range of the internal model, and safety limits such as the compressor surge margin and maximum turbine inlet temperature. This formulation also includes derivation of the conditions sufficient to prove nominal asymptotic stability of the closed-loop system. Controller performance is then evaluated through representative tracking and regulation experiments. This highlights the advantages of the proposed controller's constraint handling and disturbance rejection. More broadly, these experiments demonstrate that a nonlinear model predictive controller can be successfully deployed on a gas turbine, in real time, without the need for any linearisation. (C) 2015 Elsevier Ltd. All rights reserved.
引用
收藏
页码:194 / 206
页数:13
相关论文
共 35 条
[1]  
Ailer P., 2001, Periodica Polytechnica Transportation Engineering, V29, P117
[2]  
Al Seyab R. K, 2006, THESIS
[3]   AIRCRAFT ENGINE COMMITTEE BEST 1993 PAPER AWARD - CONTROL-ORIENTED HIGH-FREQUENCY TURBOMACHINERY MODELING - GENERAL ONE-DIMENSIONAL MODEL DEVELOPMENT [J].
BADMUS, OO ;
EVEKER, KM ;
NETT, CN .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1995, 117 (03) :320-335
[4]  
Benz M., 2010, J ENG GAS TURBINES P, V133
[5]  
Bock HG, 2007, LECT NOTES CONTR INF, V358, P163
[6]  
Brunell B. J., 2004, P ASME TURBP EXP 200
[7]  
Brunell BJ, 2002, P 41 IEEE C DEC CONT
[8]   A modular code for real time dynamic simulation of gas turbines in Simulink [J].
Camporeale, S. M. ;
Fortunato, B. ;
Mastrovito, M. .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2006, 128 (03) :506-517
[9]   Robust Nonlinear Model Predictive Control of a Run-of-Mine Ore Milling Circuit [J].
Coetzee, Loutjie C. ;
Craig, Ian K. ;
Kerrigan, Eric C. .
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2010, 18 (01) :222-229
[10]  
Davison C. R., 2006, P ASME TURB EXP