**Open Access**-
**Total Downloads**: 8 -
**Authors :**Princy Saraswat, Rajesh Bhatt, Girish Parmar -
**Paper ID :**IJERTCONV3IS31007 -
**Volume & Issue :**ATCSMT – 2015 (Volume 3 – Issue 31) -
**Published (First Online):**24-04-2018 -
**ISSN (Online) :**2278-0181 -
**Publisher Name :**IJERT -
**License:**This work is licensed under a Creative Commons Attribution 4.0 International License

#### A Comparison between Differential Evolution and Simulated Annealing for Order Reduction of Transformer Linear Section Model

Princy Saraswat1, Rajesh Bhatt 2 and Girish Parmar 3

1,2,3Department of Electronics Engineering,

University College of Engineering, Rajasthan Technical University, Kota, India-324 010.

AbstractIn the present work, a comparative study between Differential Evolution (DE) and Simulated Annealing (SA) for order reduction of transformer linear section model has been carried out. DE is stochastic, population-based algorithm while SA is a local search algorithm, inspired by the process of physical annealing associated with solids. Reduced order model of transformer linear section is obtained such that reduced order model approximates the original higher order transformer model and maintains the stability of the original system. Both mentioned algorithms are based on the minimization of the integral square error (ISE) between the transient responses of original higher order and the reduced low order transformer models. Firstly the poles are determined by dominant pole retention technique and then the zeros of reduced order transformer model are obtained using DE and SA in order to minimize the ISE between high order and low order models of transformer. The transient response parameters have also been compared along with ISE.

Keywords- Order reduction, DE, SA, Dominant pole, Integral Square Error.

I INTRODUCTION

Generally, physical systems are described by differential equation of higher order for analytical purpose. Model Order Reduction (MOR) is the field that converts large model to smaller model by mathematical approaches. The obtained reduced order model defines the original system behavior accurately without loss of any important information [1-2]. The exact analysis of these systems are monotonous, expensive and complicated [3]. So, Order reduction is motivated for simplifying, analyzing, synthesizing the systems. Also for reducing computational and hardware complexity of practical systems MOR is used. In this paper, DE and SA in association with dominant pole retention technique are compared for transformer model [2], [4] and [5].

Differential Evolution is used to optimize the real parameters, introduced by Storn and Price [6]. DE can be used to find approximate solutions to the problems having objective function non differentiable, non linear, noisy and have many local minima. DE is an Evolutionary algorithm and its main stages are initialization, mutation, recombination and selection. Initialization is the process of defining lower and upper limits of each parameter and then randomly selects initial values of parameters. Mutation is the process of obtaining donor vector from parent vector. Then recombining donor with parent vector, a trial vector is obtained through recombination process

selection of parent vector for next generation. The last three stages are conducted until some stopping condition met. The flow chart is shown in Fig. 1.

Initialization

Initialization

Mutation

Mutation

Crossover/ Recombination

Crossover/ Recombination

Selection

Selection

Stopping No

Criterion

Yes

End

Fig. 1: Flow chart of DE algorithm.

Simulated Annealing is a local search method proposed by Kirkpatrick Gelatt and Vecchi in 1983. SA is a local search algorithm, inspired by the process of physical annealing associated with solids. Simulated annealing (SA) is a random- search technique which exploits an analogy between the way in which a metal cools and freezes into a minimum energy crystalline structure (the annealing process) and the search for a minimum in a more general system [8]. In annealing process a crystalline solid is heated and then allowed to cool by decreasing the temperature of the environment in steps until it achieves its most regular possible crystal lattice configuration. The final configuration results in a solid with superior structural integrity if the cooling schedule is sufficiently slow. In SA a trial configuration is obtained by randomly generated perturbation of the current configuration of the solids. If the energy level of trial configuration is less than that of the current configuration, the trial configuration is accepted and becomes the current configuration. If the energy level of trial

[7]. The trial vector is compared with parent vector for the

configuration is greater than or equal to that of the current configuration then the trial configuration is accepted as current configuration with probability proportional to exp(E / T ) where E is difference in energy levels between

trial configuration and current configuration [8]. The flow chart of SA [9-10] is shown in Fig. 2.

Input and Assessinitial solution

Input and Assessinitial solution

Estimate initial temperature

Generate newsolution

Generate newsolution

Assess newsolution

Accept new solution

Update stores

Adjustparameters

No Terminate

search

Yes

Stop

Fig. 2: Flow chart of SA algorithm.

Dominant pole retention technique has been used to determine denominator polynomial of reduced order model by taking dominant poles of higher order system. The location of the poles of a transfer function in the S-plane affects greatly the transient response of the system. So in approximation method

the poles near to left half of s-plane are retained and other poles are discarded

For comparison of DE and SA transformer linear section model is taken as test system.

Fig. 3: Air core Transformer and its section.

Figure 3 shows the typical section of transformer model consisting a series resistance rs , a shunt resistance Rs , a self inductance L11, series capacitance Cs , parallel combination of a resistance Rg and a capacitance Cg with respect to ground. There is theory of mutual inductances between the sections of transformer model.

In this work, transformer linear section model (10 Sections) is used as assessment system having poles and zeros as mentioned below [2], [4] and [5]:

TABLE I: POLES AND ZEROS OF TRANSFORMER MODEL

Section | Poles | Zeros |

1 | – 3.06 | -7.39 |

2 | -10.37 | -16.8 |

3 | -19.84 | -28.45 |

4 | -31.33 | -41.92 |

5 | -44.51 | -56.54 |

6 | -58.69 | -71.44 |

7 | -72.94 | -85.45 |

8 | -86.39 | -97.14 |

9 | -97.59 | -104.97 |

10 | -105.09 | — |

In order to obtain reduced order transformer model, DE and SA along with dominant pole retention technique have been used.

Above mentioned techniques are simple and faster and there are few parameters to adjust.

II PROBLEM STATEMENT

G10

(s)

s9 510.1s8 1.106e5s7 1.33e7 s6 9.690e8s5 4.393e10s4

1.223e12s3 1.980e13s2 1.652e14s 5.211e14

s10 529.81s9 1.202e5s8 1.527e7s7 1.191e9s6 5.892e10s5

1.842e12s4 3.513e13s3 3.784e14s2 1.965e15s 3.330e15

Consider an nth order single input single output, linear time invariant system with the following transfer function:a0 a1s a2 s 2 ansn 1

Dominant poles of above system are:

1 = -3.06, 2 = -10.37.

(9)

Gn (s)

b0 b1s b2 s 2

bnsn

(1)

Therefore, the denominator polynomial will be:

Step 1: Calculate the dominant poles of high order model to determine the denominator polynomial of reduced order

D(s) s2 13.43s 31.7322

(10)

model.

The poles of the system to be:

The numerator polynomial of G2 (s) is obtained by DE as:

1 2 … . n .

(2)

N2 (s) 0.7450s 4.9479

So, reduced order model by DE is:

(11)

The denominator of Gr(s) is obtained such that the poles of the low order system are the dominant poles of the high order model as follows:

G2 (s ) 0.7450s 4.9479

s 2 13.43s 31.7322

(12)

1 2 …. r .

So, reduced order systems denominator is determined as:

(s 1)(s 2 )….(s r )

Let obtained denominator is:

Dr ( s ) 0 1s 2 s 2 r sr

(3)

(4)

(5)

with an ISE = 1.4638×106 .

The numerator polynomial of G2 (s) is obtained by SA as:

N2 (s) 0.7657s 4.9786

So, reduced order model by SA is:

G2 (s ) 0.7657s 4.9786

s 2 13.43s 31.7322

(13)

(14)

Step 2: Obtain numerator of reduced order system using DE and SA, respectively by minimizing the ISE between transient responses of high order and low order models of transformer linear section model.

The Integral Square Error is given by [5] and [12]:

with an ISE = 2.1800×106 .

ISE [ y (t ) yr

0

(t )]2 dt

(6)

So, obtain numerator by DE and SA, respectively. Let the numerator is:

r s 0 1s 2 s 2 r sr 1

So, the reduced order model obtained is given as:

0 1s 2 s2 r sr 1

(7)

(8)

Gr (s)

0 1s 2

s2 r sr

Fig. 4: Step response of high order and low order transformer models.

III ORDER REDUCTION OF TRANSFORMER LINEAR SECTION MODEL

Consider a 10th order system described by transfer function having poles and zeros shown in table I:

The step responses of high order and low order models of transformer linear section by DE and SA are shown in Fig. 4, which show that the transformer low order models are good approximation of the original high order transformer model, keeping ISE minimum.

Also, the frequency responses of high order and low order models of transformer by DE and SA are shown in Fig. 5, which are also comparable.

Fig. 5: Frequency response of high order and low order transformer models.

A comparison of transient response parameters of high order and low order transformer models is given in Table II, which shows that both reduced order models parameters are identical to high order transformer model.

Models | Rise time (sec.) | Settling time(sec.) | Steadystate |

Transformer 10th Order model | 0.655 | 1.2 | 0.157 |

Transformer 2nd Order model by DE | 0.664 | 1.19 | 0.156 |

Transformer 2nd Order model by SA | 0.66 | 1.185 | 0.156 |

Models | Rise time (sec.) | Settling time(sec.) | Steadystate |

Transformer 10th Order model | 0.655 | 1.2 | 0.157 |

Transformer 2nd Order model by DE | 0.664 | 1.19 | 0.156 |

Transformer 2nd Order model by SA | 0.66 | 1.185 | 0.156 |

TABLE II: TRANSIENT RESPONSE PARAMETERS

A comparison of ISE obtained from the above techniques has been given in Table III.

TABLE III: COMPARISON OF ISE

Algorithm | Reduced Model | ISE |

DE | 0.7450s 4.9479 s2 13.43s 31.7322 | 1.4638×106 |

SA | 0.7657s 4.9786 s2 13.43s 31.7322 | 2.1800×106 |

IV CONCLUSIONS

In the present work, two techniques DE and SA in association with dominant pole retention technique have been compared for the order reduction of transformer linear section model. The ISE has been calculated between high and low order transformer model and found to be low for DE as compared with SA in combination with dominant pole retention technique. Both low order transformer models are good approximation of high order transformer model. Reduced order models preserve the uniqueness of original high order transformer model and also the transient specifications are found to be comparable. Hence finally it can be concluded that combination of DE with dominant pole retention technique is more accurate than SA with dominant pole retention technique. The algorithms have been implemented in MATLAB 7.11.0 and the computational time taken is about 4 seconds for both the algorithms.

REFERENCES

[1]. R. Prasad, S. P. Sharma and A. K. Mittal, Linear Model Reduction using the Advantages of Mihailov Criterion and Factor Division, Journal of the Institute of Engineers (India), vol. 84, June 2003, pp 7-10. [2]. M. Srinivasan and A. Krishnan, Transformer Linear Section Model Order Reduction with an Improved Pole Clustering, European Journal of Scientific Research, vol. 44, no. 4, pp. 541-549, 2010. [3]. D. Kranthi Kumar, S. K. Nagar and S. K. Bhardwaj, Model Order Reduction of S.I.S.O. AND M.I.M.O. Systems Based on Genetic Algorithm, International Conference on Automation, Robotics and control systems, 2010. [4]. CH. Seshukumar, B. Dasu and M. Siva Kumar, A Hybrid Reduction Technique for Transformer Linear Section Model, International Journal of Engineering Research & Technology (IJERT), vol. 2 Issue 11, November 2013. [5]. P. Saraswat, G. Parmar and R. Bhatt, Order Reduction of Transformer Linear Section Model by Differential Evolution, 4th InternationalConference, ICATETR-2015, BKIT Kota, 19-20 June 2015(accepted).

[6]. R. Storn and K. Price, Differential Evolution a Simple and Efficient Heuristic for Global Optimization over Continuous Spaces, Journal of Global Optimization, pp. 341359, 1997. [7]. S. Das and P. N. Suganthan, Differential Evolution: A Survey of State- of- the- art, IEEE transactions on Evolutionary Computation, vol. 15, no. 1, February 2011. [8]. E. Aarts, J. Korst, Simulated annealing and Boltzmann machines: a stochastic approach to combinatorial optimization and neural computing, New York: Wiley,1989. [9]. Y. K. Soni and R. Bhatt, Simulated Annealing Optimized PID Controller design using ISE, IAE, IATE and MSE error criterion, International Journal of Advanced Research in Computer Engineering & Technology, vol. 2, July 2013. [10]. Franco Busetti, Simulated annealing overview. [11]. G.Parmar, R. Prasad and S. Mukherjee, Reduction

of linear dynamic systems using dominant pole retention method and modified cauer continued fraction, Journal of Computer Science, vol. 1, no. 6, pp. 547-554, May-June, 2006.

[12]. G. Parmar, R. Prasad and S. Mukherjee, Order Reduction of Linear Dynamic Systems using Stability Equation Method and GA, International Journal of Electrical, Computer, Electronics and Communication Engineering, vol. 1, no. 2, 2007.AUTHORS BIOGRAPHY

Ms Princy Saraswat was born in Kota (Rajasthan), India, in 1991. She received B. Tech. in Electronics and Communication Engineering from Maharishi Arvind International Institute of Technology, Kota (Rajasthan), India in 2013 and M. Tech. (pursuig) with specialization Control and Instrumentation from Rajasthan Technical University, Kota, India. Her area of interest is model order reduction of Large scale systems using optimization techniques.

Mr. Rajesh Bhatt was born in Kota (Rajasthan), India, in 1973. He received B. E. in Electronics Instrumentation & Control from Engineering College Kota (Rajasthan), India in 1996 and M.E. in Power System Engineering from Engineering college Kota (Rajasthan), India in 2010. He is pursuing Ph.D. in Electronics Engineering with specialization Control and Instrumentation from University college of Engineering,

Kota (Rajasthan), India. He has published more than

24 research papers in various International/National Journals and Conferences. He was working as Assistant Professor in Department of Electronics Engineering at Rajasthan Technical University, since 1998. His research interests are in the area of Control, Transducers and Model Order Reduction of Large scalesystems.

Dr. Girish Parmar was born in Bikaner (Rajasthan), India, in 1975. He received B.Tech. in Instrumentation and Control Engineering from National Institute of Technology, Jalandhar (Punjab), India in 1997 and M.E. Electrical (Gold Medalist) with specialization in Measurement and Instrumentation from Indian Institute of Technology, Roorkee, India in 1999. He obtained his Ph.D. in Electrical Engineering. in 2007 under Quality Improvement Programme from Indian Institute of

Technology, Roorkee, India. He is life member of Systems Society of India (LMSSI) and Associate member of Institution of Engineers, India (AMIE). He has published more than 100 research papers in various International/National Journals and Conferences. He is author of several technical books. He was working as Assistant Professor in Department of Electronics Engineering at Rajasthan Technical University, since 1999. His research interests are in the area of Process Instrumentation & Control, Optimization, Signal Processing, System Engineering and Model Order Reduction of Large scale systems. He joined as a Principal of Modi Institute of Technology, Kota in December, 2011. Presently, he is working as Associate Professor in the department of Electronics Engg., Rajasthan Technical University, Kota, since July 2013.