im Journal of JET V°lume 12 (2°19) p.p. 43-52 Issue 3, November 2019 Type of article 1.01 Technology www.fe.um.si/en/jet.html RESPONSE SURFACE METHOD-BASED OPTIMIZATION OF OUTER ROTOR PERMANENT MAGNET SYNCHRONOUS MOTOR NACIN OPTIMIZACIJE ZUNANJEGA ROTORJA ZA TRAJNI MAGNETNI SINHRONSKI MOTOR Vahid Rafiee1, Jawad FaizR Keywords: Response surface surrogate method, outer rotor permanent magnet synchronous motor, sequential quadratic programming optimization Abstract The Finite Element Method (FEM) is a prominent analysis approach. Although it is applicable for simulation and optimization of electrical machines, FEM is a very time-consuming technique. One of the approaches to shorten the optimization runtime is the use of surrogate models instead of FEM. In this paper, the design and optimization of an outer rotor permanent magnet synchronous motor for a hybrid vehicle are investigated. Response surface methodology (RSM) with four input variables is integrated with a sequential quadratic programming algorithm for optimization. Before the optimization, the performance of the surrogate model in the prediction of untried points is validated. Finally, the optimal motor is simulated by FEM to verify the results of RSM-based optimization, and the outputs of both models are compared. R Corresponding author: Professor Jawad Faiz, Tel.: +98 21 6111 4223, Mailing address: Center of Excellence on Applied Electromagnetic Systems, School of Electrical and Computer Engineering. College of Engineering, University of Tehran, North Kargar Avenue, Tehran, E-mail address: jfaiz@ut.ac.ir 1 Center of Excellence on Applied Electromagnetic Systems, School of Electrical and Computer, Engineering. College of Engineering, University of Tehran, North Kargar Ave, Tehran. JET 43 Vahid Rafiee, Jaw ad Faiz JE TVoi. 12! (2019) Issue 3 Povzetek Metoda končnih elementov (FEM) je eden boljših pristopov analize. Čeprav je FEM uporabna za simulacijo in optimizacijo električnih strojev, je pa zelo zamudna tehnika. Eden od pristopov za skrajšanje trajanja optimizacije je uporaba nadomestnih modelov namesto FEM. V prispevku je raziskano načrtovanje in optimizacija sinhronskega motorja s trajnim magnetom zunanjega rotorja za hibridno vozilo. Metodologija odzivne površine (RSM) s štirimi vhodnimi spremenljivkami je integrirana z algoritmom zaporednega kvadratnega programiranja za optimizacijo. Pred optimizacijo je bila uspešnost nadomestnega modela pri napovedovanju neizkušenih točk potrjena. Končno FEM simulira optimalni motor, da preveri rezultate optimizacije na osnovi RSM in primerja izhode obeh modelov. 1 INTRODUCTION The most well-known method for the optimization of an electromagnetic device is the finite element method (FEM). Using this method requires a long runtime. It is highly desirable to reduce the computational time of these optimizations. One of the best approaches to shortening the computation runtime is based on surrogate modelling in which the outputs for any new, untried point are calculated using the surrogate model. Different artificial intelligence methods, including Kriging, radial basis function (RBF), and response surface method, have been used thus far. Kriging and RBF are more complicated than the response surface method and have multiple distance matrix calculations for new untried points. In contrast, RSM gives the closed-form equations of the system, which enables the designer to use any optimization method, including sequential quadratic programming (SQP). Optimization of a linear actuator using RSM has been reported in [2]. In this paper, the objective of the optimization is to minimize the weight with constraints for thrust force and detent force. The design of a slot-less permanent magnet linear synchronous machine (PMLSM) using RSM with three input variables and two responses has been reported in [4]. Rotor pole design in a brushless permanent magnet motor has been proposed in [5] in which cogging torque is expressed in terms of three structural variables of the rotor and air gap length in RSM surrogate model. The design and optimization of a PM synchronous motor using an RSM surrogate model to increase constant power speed range (CPSR) has been studied in [6], in which the RSM has three input variables, and a genetic algorithm has been used to optimize the RSM equations. In the present paper, an outer rotor permanent magnet motor with particular application for hybrid vehicles is designed. To shorten the computational time, the equations of RSM surrogate model of the system are proposed. Finally, the closed-form equations of the motor are optimized using a sequential quadratic programming (SQP) algorithm to determine the optimum point. The results of the RSM and FEM are compared. 2 INITIAL DESIGN OF MOTOR The design and optimization of an outer rotor surface-mounted permanent magnet machine with 12 slots and 10 poles are investigated here. The proposed machine delivers 400 Nm torque at 1200 rpm. To maximize the fill factor, prefabricated winding has been used, [7]; thus, the stator has open slots to enable assembling this type of winding. The magnets of the motor are mounted on the surface of the rotor in the air gap. 44 JET Response surface method-based optimization of outerrotors permanent magnet synchronous motor 3 RESPONSE SURFACE SURROGATE MODEL The best advantage of the RSM Surrogate model is its closed-form equation (y=f(x1,x2^,xn)). The Outputs functions expressed by the inputs for a linear model are as follows [8]: f (x) = ß +X ßiXi « (3.1) and for quadratic models, it is as follows: f(x) = ß0 + £ ß X, +£ ß Xl +± XßjX.Xj (3.2) i=1 ii=1 i< j where fi, ßj and ß are the coefficients of the polynomial and X, and Xj are the input variables of the system. The ceeOOicieeOo ß, ere celculeOed so Ocllcwo: ß = [ X X]-1 X> -1 (3-3) where X io Ohe matrix nO Ohe iepuO verisbleo sed y io Ohe cerreoseedieo output velueo Oer Ohe oempled seieOo- 4 RSM SURROGATE MODEL OF MOTOR In this paper, the design space consists of four input variables, and the Box-Behnken RSM surrogate model is used to model this design space. The maximum input current (Imax), slot height, the width of the bottom of the slot, and the thickness of the magnets are considered as input variables of this surrogate model. Fig. 1 shows the geometry and three structural input variables. Figure 1: Geometry and structural variables of the motor JET 45 Vahid Rafiee, Jaw ad Faiz JE TVoi. 12! (2019) Issue 3 The range of these variables in the design space has been shown in Table 1. Making a Box-Behnken set of sample points for the surrogate model for a k-dimensional design space requires 2k(k-1)+C0 sample point [9], [10]. C0 is the centre point, and it determines the curvature of the model. Here, four central points are simulated; 28 sample points are generated by Box-Behnken, and the corresponding outputs are calculated using FEM. Table 1: Rengh of input variables Input variable Parameter name Minimum Maximum Imax A 130 160 Slot height B 20 34 Slot width C 12 18 Magnet thickness D 7 12 Table 2 presents the list of simulated points selected by Box Behnken with their corresponding responses. The price, torque, and efficiency of the motor are considered as surrogate model responses. Table 3 shows the analysis of variance (ANOVA) of these responses. In each of the responses, the terms with the p-value higher than 0.1 are insignificant and thus are neglected in the RSM equations. All terms of the equations in efficiency and torque are significant, but in price just six terms are significant, and the others are ignored. The quadratic polynomials of the RSM surrogate model of the system are calculated using Eq. (2) by substituting the simulated matrices of Table 2. The closed-form equations of the price, torque, and efficiency are as follows: Pr ice = 211.1693 + 6.04295 + 3.8953C + 46.74D + 1.0097BC 2 2 (4.1) + 0.4897C2 -0.5266D Torque = 359.3804 + 36.63A - 12.5602B -7.6114C + 12.5046D -2.1576AB -1.2546AC + 2.4269AD - 4.0435BC - 2.5859BD (4.2) -1.6512CD-0.7935A2 -2.9347B2 -1.5774C2 -4.7137D2 Efficiency = 0.9138 - 0.0047A + 0.0129B + 0.0084C + 0.0062D +0.0012AB + 0.0007AC + 0.0005AD - 0.0022BC - 0.0009BD (4.3) -0.0005CD -0.0003A2 -0.0035B2 -0.0005C2 -0.0014D2 The most expensive part of the motor is the magnet, and in Eq. (4), D has the greatest coefficient (46.74). Torque highly depends on the current, and in Eq. (5) the greatest positive coefficient is the coefficient of the current, which is 36.63. As the current and the conduction loss increase, the efficiency decreases. Thus, the current in Eq. (6) has a negative coefficient. 46 JET Response surface method-based optimization of outerrotors permanent magnet synchronous motor Table 2: List of sampled points by Box Behnken sampling and corresponding responses A B C D Price ($) Torque (Nm) Efficiency (%) 1 145 34 12 9.5 212.86 354.7 91.63 2 145 27 15 9.5 211.16 359.38 91.38 3 145 20 12 9.5 202.62 371.55 88.58 4 145 34 18 9.5 222.67 330.42 92.91 5 145 20 15 7 157.86 349.38 88.84 6 145 34 15 12 263.35 348.76 92.71 7 130 27 12 9.5 207.76 326 91.01 8 160 20 15 9.5 205.14 406.98 89.09 9 160 27 12 9.5 207.76 402.52 89.94 10 160 34 15 9.5 217.15 377.54 91.9 11 145 27 15 9.5 211.16 359.38 91.38 12 130 20 15 9.5 205.14 329.26 90.32 13 160 27 15 12 257.38 405.42 91.41 14 145 27 12 7 160.49 346.36 0.8967 15 145 34 15 7 169.89 329.25 91.63 16 145 20 15 12 251.37 379.23 90.3 17 145 27 15 9.5 211.16 359.38 91.38 18 145 27 18 7 168.28 334.85 91.45 19 130 34 15 9.5 217.15 308.45 92.64 20 145 27 18 12 261.77 356.33 92.59 21 160 27 15 7 163.89 375 90.04 22 160 27 18 9.5 215.55 385.35 91.74 23 145 20 18 9.5 208.39 363.44 90.77 24 130 27 15 12 257.38 328.21 92.26 25 145 27 15 9.5 211.16 359.38 91.38 26 130 27 15 7 163.89 307.5 91.11 27 145 27 12 12 253.98 374.44 91.03 28 130 27 18 9.5 215.55 313.85 92.50 Table 4 presents the fit statistics of the surrogate model. In this table, C.V% is the coefficient of variance, R2 is the coefficient of determination. In all responses, the R2 and adjusted R2 are close; thus, there is no insignificant variable in the surrogate model, [8]. Finally, the Adeq precision is the measure of the signal-to-noise ratio. In all responses, the Adeq precision is higher than 4, which shows that the model is desirable and can navigate the design space, [8]. JET 47 Vahid Rafiee, Jaw ad Faiz JE TVoi. 12! (2019) Issue 3 Table 3: ANOVA for quadratic form of RSM Source p-value Price Efficiency Evrque Model < 0.0001 < 0.0001 < 0.0001 A 1 < 0.0001 < 0.0001 B < 0.0001 < 0.0001 < 0.0001 C < 0.0001 < 0.0001 < 0.0001 D < 0.0001 < 0.0001 < 0.0001 AB 1 < 0.0001 < 0.0001 AC 1 < 0.0001 0.0004 AD 1 0.0006 < 0.0001 BC < 0.0001 < 0.0001 < 0.0001 BD 0.6392 < 0.0001 < 0.0001 CD 1 0.0004 < 0.0001 A2 1 0.0075 0.0029 B2 0.4254 < 0.0001 < 0.0001 C2 < 0.0001 0.0002 < 0.0001 D2 < 0.0001 < 0.0001 < 0.0001 Table 4: Fit statistics of the RSM surrogate model Price ($) Torque (Nm) Efficiency (%) Mean 211.15 355.09 91.13 C.V% 0.0272 0.1499 0.0264 R2 1 0.9998 0.9998 Adjusted R2 1 0.9996 0.9996 Predicted R2 1 0.999 0.9988 Adeq Prediction 2510.4112 256.2085 242.4228 Fig. 2 presents the actual values calculated by FEM and the predicted values by RSM. This figure shows that there is a good agreement between the predicted and actual values. 48 JET Response surface method-based optimization of outerrotors permanent magnet synchronous motor 5 OPTIMIZATION OF MOTOR The motor is optimized using the closed-form equations of the RSM surrogate model. The goal Min: Price s.t Torque > 400 Nm Efficiency > 91% (5.1) 175 210 245 Actual Price ($) 93 300 330 360 390 420 Actual Torque (Nm) (b) 90 91 92 93 Actual Efficiency (%) (c) Figure 2: Predicted versus actual values at sampled points for (a) Price, (b) Torque, (c) Efficiency of the optimization is to minimize the price of the motor, considering the following constraints for torque and efficiency. Sequential quadratic programming (SQP) is applied to optimize the price. The optimization is performed using the RSM equations. The final values of the RSM input parameters at the Table 5: Izpui variables di itt optimum poizi Input variable Parameter symbol Optimum value Imax (A) A 160 Slot height (mm) B 24.9084 Slot width (mm) C 16.2131 Thickness of magnet (mm) D 10.2329 JET 49 Vahid Rafiee, Jawad Faiz JE TVo 1 12(2019 ) Issue 3 optimum point is presented in Table 5. After the optimization, the optimal point is simulated by FEM to verify the results of the RSM based optimization. Fig. 3(a) and (b) show the torque and efficiency of the motor at optimum point using FEA in one complete electrical period of the motor, which indicates that the torque and efficiency constraints are satisfied at the optimal point. CD cr jO 300 - 2oo I-,-,-,-,- 0 2 4 6 8 10 Time (ms) (a) 8g I-,-,-,-,- 0 2 4 6 8 10 Time (ms) (b) Figure 3: (a) Torque of optimum motor using FEA (b) efficiency of the optimum motor using FEA A full comparison of the RSM and FEM at the optimum point has been presented in Table 6. According to this table, the error of the RSM surrogate model is acceptable; thus, this method can be used instead of FEM in optimizations. For a precise investigation at the optimal point, the field density of the motor at full load is shown in Fig. 4. This figure indicates that there is no saturation in the motor, and a good performance of the motor is guaranteed. Table 6: Comparison of RSM end FEA et optimal point RSM FEA Error Price ($) 224.5 224.6 3.87e-04 Torque (Nm) 400 400.4 9.90e-04 Efficiency (%) 91 91.2 2.10e-03 50 JET Response surface method-based optimization of outerrotors permanent magnet synchronous motor 7 CONCLUSION Generally speaking, the optimization of electromagnetic devices takes a long computation time using FEM. This paper presented an RSM surrogate-based model optimization. All needed outputs of the model were described by closed-form equations in RSM. Having a closed-form set of equations enables the designer to use the best algorithm of optimization, and SQP was used here. Comparison of RSM and FEM results show that there is a good agreement between the RSM surrogate model and FEM. Simulating the motor by FEM at the optimal point verified the results of the RSM based optimization. 8 REFERENCES [1] A. Forrester, A. Sobester, and A. Keane: Engineering design via surrogate modelling: a practical guide. John Wiley & Sons, 2008 [2] H. M. Hasanien, A. S. Abd-Rabou, and S. M. Sakr: Design optimization of transverse flux linear motor for weight reduction and performance improvement using response surface methodology and genetic algorithms, IEEE Trans. Energy Convers., vol. 25, no. 3, pp. 598-605, 2010 [3] G. Lei, J. Zhu, Y. Guo, C. Liu, and B. Ma: A review of design optimization methods for electrical machines, Energies, vol. 10, no. 12, p. 1962, 2017 [4] S.-I. Kim, J.-P. Hong, Y.-K. Kim, H. Nam, and H.-I. 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