Robust Controller Development Via Iterative Model Updating for Active Magnetic Bearing Rotor Systems

被引:2
作者
Donati, Giovanni [1 ]
Neri, Massimiliano Ortiz [2 ]
Mugnaini, Marco [3 ]
Basso, Michele [1 ]
Sawicki, Jerzy T. [4 ]
机构
[1] Univ Florence, Dept Informat Engn, I-50139 Florence, Italy
[2] Baker Hughes Co, Nuovo Pignone, I-50127 Florence, Italy
[3] Univ Siena, Dept Informat Engn & Math, I-53100 Siena, Italy
[4] Cleveland State Univ, Washkewicz Coll Engn, Ctr Rotating Machinery Dynam & Control, Cleveland, OH 44115 USA
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 2025年 / 147卷 / 01期
关键词
model updating; robust control; modal shape; active magnetic bearing; AMB; augmented PID; COHERENT STRUCTURES; STABILITY ANALYSIS; FLOWS;
D O I
10.1115/1.4066614
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Modern turbomachinery equipped with active magnetic bearings (AMBs) requires increasingly high-performance controllers to ensure safe and efficient operations. These controllers are typically tuned based on frequency responses, or in more advanced cases based on the plant models. However, effects such as interference fits and shrink fits can significantly impact rotor dynamics, reducing the accuracy and reliability of these models. This study proposes a novel model updating method to deal with problems related to practical applications of model-based controllers. First, this paper presents an iterative model updating method based on an optimization algorithm to adjust the finite element (FE) model of complex rotors used in oil and gas applications, exploiting frequency measurements from the actual rotor. Subsequently, the proposed iterative updating method is utilized to develop a set of rotor models that differ only for some designed rotor modal shapes that are not well identified by the rotor frequency measurements. This set of rotor models is then exploited by a nonsmooth optimization algorithm to synthesize a robust controller-an augmented PID-optimized to ensure a specified level of performance across all scenarios described by the developed set of rotor models, thereby guaranteeing safe operations over time.
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页数:11
相关论文
共 22 条
[1]   Nonlinear dynamics of fully developed swirling jets [J].
Douglas, Christopher M. ;
Emerson, Benjamin L. ;
Lieuwen, Timothy C. .
JOURNAL OF FLUID MECHANICS, 2021, 924
[2]   Impact of precessing vortex core dynamics on the thermoacoustic instabilities in a swirl-stabilized combustor [J].
Karmarkar, Ashwini ;
Gupta, Saarthak ;
Boxx, Isaac ;
Hemchandra, Santosh ;
O'Connor, Jacqueline .
JOURNAL OF FLUID MECHANICS, 2022, 946
[3]  
Lieuwen TC, 2012, UNSTEADY COMBUSTOR PHYSICS, P1, DOI 10.1017/CBO9781139059961
[4]   Instability of vortical and acoustic modes in supersonic round jets [J].
Luo, KH ;
Sandham, ND .
PHYSICS OF FLUIDS, 1997, 9 (04) :1003-1013
[5]  
Manoharan K., 2017, ASME, DOI [10.1115/GT2017-63936, DOI 10.1115/GT2017-63936]
[6]   A weakly nonlinear analysis of the precessing vortex core oscillation in a variable swirl turbulent round jet [J].
Manoharan, Kiran ;
Frederick, Mark ;
Clees, Sean ;
O'Connor, Jacqueline ;
Hemchandra, Santosh .
JOURNAL OF FLUID MECHANICS, 2020, 884
[7]  
Mistry D., 2011, Local Stability Analysis of Swirling Shear Flows
[8]  
Morzynski M, 2008, LECT NOTES COMPUT SC, V4967, P1293
[9]   Further Characterization of the Disturbance Field in a Transversely Excited Swirl-Stabilized Flame [J].
O'Connor, Jacqueline ;
Lieuwen, Tim .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2012, 134 (01)
[10]   Three-dimensional coherent structures in a swirling jet undergoing vortex breakdown: stability analysis and empirical mode construction [J].
Oberleithner, K. ;
Sieber, M. ;
Nayeri, C. N. ;
Paschereit, C. O. ;
Petz, C. ;
Hege, H-C. ;
Noack, B. R. ;
Wygnanski, I. .
JOURNAL OF FLUID MECHANICS, 2011, 679 :383-414