Induction machine control using robust eigenstructure assignment

被引:8
作者
Duval, C
Clerc, G
Le Gorrec, Y
机构
[1] Univ Lyon 1, CNRS, UMR 5005, CEGELY, F-69622 Villeurbanne, France
[2] Univ Lyon 1, CNRS, UMR 5007, LAGEP,ESCPE, F-69622 Villeurbanne, France
[3] Univ Nantes, Ecole Polytech, IREENA, F-44306 Nantes, France
关键词
induction motor; state feedback; linear matrix inequalities; eigenstructure assignment; Kalman filters; robustness;
D O I
10.1016/j.conengprac.2004.12.009
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Control of induction machines is well known to be difficult owing to the fact that the models of induction motor are highly nonlinear and time variant. In this paper, we propose a very simple approach based on linear eigenstructure assignment and eigenstructure projection to design an efficient control law. This is the first step to a more global approach using multimodel eigenstructure assignment and self-scheduling. The controller, which is proposed here, is not scheduled (with the rotor speed) but still has correct performance over the entire operating range of the induction motor. A Kalman filter is used to estimate the flux vector. The simulation is based on the non-linear model and the application is made on an experimental bench. (c) 2005 Elsevier Ltd. All rights reserved.
引用
收藏
页码:29 / 43
页数:15
相关论文
共 17 条
[1]  
[Anonymous], 1990, Control of Electrical Drives
[2]  
Bose B. K., 1986, Power electronics and AC drives
[3]  
BOSE BK, 1998, IEEE IND ELECT SOC N, V45, P7
[4]   H-INFINITY SYNTHESIS USING A BILINEAR POLE SHIFTING TRANSFORM [J].
CHIANG, RY ;
SAFONOV, MG .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (05) :1111-1117
[5]   A robust self-scheduled missile autopilot:: design by multi-model eigenstructure assignment [J].
Döll, C ;
Le Gorrec, Y ;
Ferreres, G ;
Magni, JF .
CONTROL ENGINEERING PRACTICE, 2001, 9 (10) :1067-1078
[6]  
DUMUR D, 1998, IFAC WORKSH MOT CONT
[7]  
GARCIA SG, 1999, IEE P-ELECT POW APPL, V146, P282
[8]  
LAROCHE E, 2000, REV INT GENIE ELECT, V3, P7
[9]  
Le Gorrec Y, 1998, J GUID CONTROL DYNAM, V21, P77, DOI 10.2514/2.4200
[10]  
LEGORREC Y, 1998, P CESA98 C NB HAMM T