Internal model control design based on approximation of linear discrete dynamical systems

被引:9
|
作者
Vasu, G. [1 ]
Kumar, M. Siva [2 ]
Raju, M. Ramalinga [3 ]
机构
[1] Raghu Engn Coll A, Dept EEE, Visakhapatnam, Andhra Pradesh, India
[2] Gudlavalleru Engn Coll A, Dept EEE, Gudlavalleru 521356, Andhra Pradesh, India
[3] JNTUK, UCEK A, Dept EEE, Kakinada 533001, Andhra Pradesh, India
关键词
Model order reduction; Discrete internal model control; Enhanced differential evolution algorithm; Improved discrete Multi-Point Pade approximation; Discrete-time systems; ORDER REDUCTION; POWER-SYSTEMS;
D O I
10.1016/j.apm.2021.04.017
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this paper, a new direct discrete approximation based internal model control design is proposed to the linear discrete dynamical systems. The approximation method is used to determine an accurate and stable reduced-order model for the considered original higher-order discrete-time system. The method involves an enhanced Differential Evolution algorithm to ascertain the stable denominator polynomial coefficients, and the preferable reduced numerator polynomial coefficients are evaluated by using the improved discrete multi-point Pade approximation approach. The method deploys on discrete step integral square error minimization between the original dynamical system and the approximated model, together with retaining their discrete impulse response energy values. The approximated model has been considered an internal (predictive) model and proceeds with an optimal internal model controller design to improve the discrete dynamical system behaviour according to the reference input/the set point. The controller's best performance is attained by tuning the single filter parameter 'lambda' by minimizing the integral square error between the reference input and the actual output of the dynamical system using the enhanced differential evolution algorithm. The acceptability and applicability of the proposed process reduction-based controller design have been validated on a single-input single-output supersonic jet engine inlet dynamical model. The controller robust study is conducted by inserting 10% disruption uncertainty in the system dynamical model poles and zeros. The method has also been extended to the discrete multi-input multi-output dynamical model of the single machine infinite bus power system to develop an optimal internal model control-based power system stabilizer. The simulation results showing better reference input tracking, comparison of performance indices, and also highlight the efficacy of the proposed controller design. (C) 2021 Elsevier Inc. All rights reserved.
引用
收藏
页码:683 / 700
页数:18
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