Modelling, Simulation and Nonlinear Control of Permanent Magnet Linear Synchronous Motor

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ISSN: 2278-8875 Modelling, Simulation and Nonlinear Control of Permanent Magnet Linear Synchronous Motor Dr.K.Alicemary 1, Mrs. B. Arundhati 2, Ms.Padma.Maridi 3 Professor and Principal, Vignan s Institute of Information Technology, JNTUK, Duvvada, Visakhapatnam, India 1 HOD & Associate Professor, Dept. of Electrical & Electronics Engineering, Vignan s Institute of Information Technology, JNTUK, Duvvada, Visakhapatnam, India 2 Dept.of Electrical & Electronics Engineering, Vignan s Institute of Information Technology, JNTUK, Duvvada, Visakhapatnam, India 3 Abstract: This paper describes a nonlinear model of the Permanent Magnet Linear Synchronous Motor and an analogy between the rotary motor and the linear motor. Constructional details of various sub-models for the permanent magnet linear synchronous motor are given and their implementation in SIMULINK is outlined. A novel control of PMSM is designed by which the system nonlinearity is cancelled. In addition, a linear state feedback control law based on pole placement technique to achieve zero steady state error with respect to reference current specification is employed to improve the dynamic response. The extensive simulation is performed through MATLAB SIMULINK. Keywords: Dynamic Modelling; Permanent magnet linear synchronous motor I. INTRODUCTION In today's competitive industrial environment, a tremendous amount of resources are dedicated to simple, optimal, and efficient solutions for the process automation, machine tool and material handling systems. Linear motors can give machine tools linear motion directly without indirect coupling mechanisms such as gear boxes, chains and screws. In particular, permanent magnet direct drive motors are becoming more and more popular in machine automation nowadays. The advantages of permanent magnet motor drives are their gearless structure, excellent control Characteristics like high speed, high acceleration and the most importantly, high motion precision and better efficiency. PMLSMs are used in lifts, paper machines, propulsion units of ships, windmills etc. In PMLSM, the moving part (mover) of which consists of a slotted armature and three-phase windings, while the surface permanent magnets (SPMs) are mounted along the whole length of the path (stator). 1 -armature, 2 - PMs 3 -carrier, 4 - guiderail Fig.1 : permanent magnet linear synchronous motor LSMs operating on the principle of the travelling magnetic field, the speed v of the moving part is equal to the synchronous speed v s of the travelling magnetic field depends only on the input frequency f (angular input frequency ω = 2πf) and pole pitch τ. It does not depend on the number of poles 2p. Copyright to IJAREEIE www.ijareeie.com 555

v = v s = 2fτ = ω π τ This paper is organized as follow: Section I gives the Introduction of the Permanent Magnet Linear Synchronous Motor. Section II is helpful to understand the analogy between permanent magnet linear synchronous motor and rotary motor. Section III explains the System dynamic modeling of motor. Section IV show the performance of open loop motor and Section V describes closed loop system and Section VI show the performance of closed loop motor the last section concludes the paper and followed by the references. II. ANALOGY BETWEEN THE PERMANENT MAGNET ROTARY SYNCHRONOUS MOTOR AND THE PMLSM The electrical model of the PMLSM can be obtained by analogy to a permanent magnet rotary synchronous motor, as shown in Fig. 2. For a rotary motor, the three armature windings shift one another by an electrical angle of 2π/3, and each winding covers an electrical angle of π in the stationary reference. Fig 2 : Electrical model of the PMLSM By analogy, the stator armature windings of a PMLSM shift one another by a distance of 2τ/3 (τ: pole pitch step between two consecutive magnetic poles of secondary) and each winding covers a distance of τ in the linear reference frame. The electrical angle along which the primary of the PMLSM moves in the linear reference frame can be expressed by θ e = N p x ; N p = π τ Here, N p is the electrical position constant of the PMLSM. TABLE I. EQUIVALENCES OF ELECTRICAL ANGLE AND ELECTRICAL ANGULAR SPEED With the rapid development in computer hardware and software, new simulation packages which are faster and more user friendly are now available. This paper discusses the use of one such product, the SIMULINK software of MATLAB, in the dynamic modeling of the PMLSM. The main advantage of SIMULINK over other programming software is that, instead of compilation of program code, the simulation model is built up systematically by means of basic function blocks. Through a convenient graphical user interface (GUI), the function blocks can be created, linked and edited easily using menu commands, the keyboard and an appropriate pointing device (such as the mouse). A set of machine differential equations can thus be modeled by interconnection of appropriate function blocks, each of which performing a specific mathematical operation. Programming efforts are drastically reduced and the debugging of errors is easy. Since SIMULINK is a model operation programmer, the simulation model can be easily developed by addition of new sub-models to cater for various control functions. As a sub-model the PMLSM could be incorporated in a complete electric motor drive system. III. DYNAMIC MODEL OF PMLSM USING SIMULINK A generalized dynamic model of the PERMANENT MAGNET LINEAR SYNCHRONOUS MOTOR consists of an electrical sub-model to implement the three-phase to two-axis (3/2) transformation of stator voltage and current calculation, a thrust submodel to calculate the developed electromagnetic thrust, and a mechanical sub-model to yield the rotor or mover velocity. Copyright to IJAREEIE www.ijareeie.com 556

III. 1. ELECTRICAL SUB-MODEL OF THE PMLSM The voltage equations for the permanent magnet synchronous motor in synchronously rotating reference frame are V qs = R s i qs + Pλ qs + ω e λ ds (1) V ds = R s i ds + Pλ ds ω e λ qs (2) Where, λ qs = i qs (3) λ ds = i ds + λ PM (4) By substituting eq no s (3) & (4) in equations (1) & (2) respectively, we get V qs = R s i qs + Pi qs + ω e i ds + ω e λ PM (5) V ds = R s i ds + Pi ds ω e i qs (6) By rearranging equations (5) & (6),then Pi qs = V qs R s i qs ω e i ds ω e λ PM Pi ds = V ds R s i ds + ω e i qs i qs i ds = 1 0 0 1 V qs V ds R s 0 0 R s i qs i ds 0 ω e ω e 0 i qs i ds + ω eλ PM 0 Fig-3 : Electrical Sub Model of PMLSM III. 2. THRUST SUB-MODEL OF PMLSM π F e = 3 P λ 2 τ PMi qs + i ds i qs Copyright to IJAREEIE www.ijareeie.com 557

Fig-4 : Electromagnetic Thrust sub model Where flux = λ PM III. 3. MECHANICAL SUB-MODEL OF PMLSM By taking laplace transform of above equation we obtain F e F l = MV e + BV e F e F l = MSV e + BV e F e F l = MS + B V e From which the ratio, V e F e F l is obtained as V e F e F l = MS + B Fig-.5: Mechanical Sub Model of PMLSM The electrical sub-model in Fig-3, the thrust sub-model in Fig-4, the mechanical sub-model in Fig-5, are grouped together to form the PMLSM model as shown in Fig-6. Fig.6: PMLSM overall Model in SIMULINK IV. OPEN LOOP RESULTS Open loop simulation results for step change in speed at constant Load Thrust shown in fig-7 and for step change in Load Thrust at constant speed is shown in fig-8. Copyright to IJAREEIE www.ijareeie.com 558

Fig-7. Simulation results of PMLSM for step change in speed from 0.8 m/s to1.2 m/s at 5 th sec at constant thrust of 10N Fig.8 : Simulation results of PMLSM for step change in thrust from 10N to 15 N at 5 th sec at constant Speed of 0.8m/s. V. CLOSED LOOP CONTROL SYSTEM In this paper, the proposed controller represented in the conventional two-loop structure for the motor drive is shown in Fig.9. The outer loop is the speed controller, the output of which is the reference value of the thrust F e *. In field oriented control algorithm thrust is controlled by the q-axis current component. Hence the reference value of the currents i q * is computed from reference thrust while id* is zero. The inner loop is the current controller which consists of a nonlinear controller by which the system nonlinearity is canceled using exact feedback linearization. The eigen values of the resulting linear systems are shifted by state feedback to appropriate locations in order to achieve the desire dynamic performance. Since the main task of the current controller is to follow reference thrust set by outer speed loop. For this purpose, the state feedback design is augmented with integral of output errors. Copyright to IJAREEIE www.ijareeie.com 559

Fig.9 : Closed loop Simulink Diagram VI. CLOSED LOOP CONTROL RESULTS Closed loop simulation results for step change in speed at constant thrust of 10N shown in Fig-10. Simulation results for step change in thrust at constant speed are shown in Fig-11. Fig.10 Simulation results of PMLSM for step change in Speed from 0.4 to 0.6 at 5 th sec and from 0.6 to 0.5 at 10 th sec at constant thrust of 10N Copyright to IJAREEIE www.ijareeie.com 560

Fig.11 Simulation results of PMLSM for Step change in thrust from 10 to 8 at 5 th sec and from 8 N to 12N at 10 th sec at constant speed of 0.4m/sec VII. CONCLUSION In this paper we have used SIMULINK software of MATLAB to test the dynamic model of PMLSM at open loop & closed loop control. A generalized approach to the design of the speed control of Linear synchronous Motor has been presented by which the system nonlinearity is cancelled. In addition, a linear state feedback control law based on pole placement technique to achieve zero steady state error with respect to reference current specification is employed to improve the dynamic response. The closed loop control simulation shows good results. The predicted current step responses agreed well with the measurements and less overshoots were observed. SIMULATION PARAMETERS The permanent magnet linear synchronous motor chosen for the simulation studies has the following parameters: (Stator direct-axis inductance) = 0.0131 mh (Stator quadrature-axis inductance) = 0.0131 mh R s (Stator winding resistance) = 2.1 0hmS λ PM Permanent magnet flux linkage = 0.1391 webers τ = pole pitch = 20 mm M (mass of the mover) = 4.5 kgs VIII. NOTATIONS USED V ds, V qs i ds, i qs d& q AXIS STATOR VOLTAGES RESPECTIVELY d& q AXIS STATOR CURRENTS RESPECTIVELY λ ds, λ qs d &q AXIS STATOR MAGNETIC FLUXS RESPECTIVELY λ PM PERMANENT MAGNET FLUX LINKAGE Copyright to IJAREEIE www.ijareeie.com 561

, d& q AXIS STATOR INDUCTANCES RESPECTIVELY RS M F e, F L f e τ V v e, v e V m B P STATOR RESISTANCE TOTAL MASS OF THE MOVING ELEMENT SYSTEM ELECTROMAGNETIC, EXTERNAL DISTURBANCE (OR) THRUSTS RESPECTIVELY ELECTRIC FREQUENCY POLE PITCH LINEAR VELOCITY OF THE MOVER ELECTRIC, REFERENCE ELECTRIC LINEAR VELOCITYS RESPECTIVELY MECHANICAL LINEAR VELOCITY VISCOUS FRICTION AND IRON-LOSS COEFFICIENT NUMBER OF POLE PAIRS ACKNOWLEDGEMENT This work is supported by All India council of Technical Education(AICTE), New Delhi under Research Promotion Scheme, File no 8023/RID/RPS-78/2010-11 REFERENCES [1] J. Yang,G. He, and J. Cui, Analysis of PMLSM direct thrust control system based on sliding mode variable structure, in Proc. IPEMC 06, pp. 1-5, 2006. [2] Oskar Wallmark, Modelling of Permanent-Magnet Synchronous Motors Machines with Non-Sinusoidal Flux Linkage, Chalmers University of Technology, Sweden. [3] Maloney, L. D., Linear Motors Hit Their Stride, Design News (Reed Business), 2005, [4] W. Leonard, Control of Electrical Drives, Springer-Verlag, Berlin, 1996. [5] Alice Mary, K., Nonlinear Modeling, Control System Design and Implementation for an Inverter-fed Synchronous Motor Drive, Ph.D. Thesis, Department of Electrical Engineering, I.I.T. Kharagpur, 1998. [6] John Wiley & Sons, Parker, R.J., Advances in Permanent Magnetism, 1990. [7] Jacek F. Gieras, Zbigniew J. Piech, Bronislaw Tomcz Linear Synchronous Motors: Transportation and Automation Systems (Electric Power Engineering Series)],2000 CRC press. BIOGRAPHY Dr. K. Alice Mary was born on 24 th day of April 1959, received BE from Govt.BDT CE&T, Davanagere, Karnataka, India in 1981, ME in the year 1989 from IIT-Roorkee and PhD from IIT-Kharaghpur in the year 1998. She is in teaching profession from 1981 onwards and now working as Professor and Principal of Vignan s institute of information technology, Visakhapatnam. To her credit, she received many prestigious awards for her achievements in academic performance at national level. Her research interests are control system applications to power electronics and machine drives. B.Arundhati was born on 19 th day of March 1968, received BE from University college of Engineering, Burla, Sambalpur, Orissa, India in 1991, M.Tech in the year 2005 from JNTU,Hyderabad and pursuing PhD from JNTU, Hyderabad. Presently working as Asso. Professor and HOD-EEE of Vignan s institute of information technology, Visakhapatna,India. Her research interests are Linear motors & control system applications to power electronics and machine drives. Padma.Maridi was born on 4 th day of august 1988, received B.E from Sir C.R.Reddy college of engineering, eluru,a.p, India in 2009. She is pursuing M.TECH in the Vignan s Institute of Information Technology,Vizag, JNTUK, India. Her current research interests include permanent magnet linear synchronous motor drive system, and motor control. Copyright to IJAREEIE www.ijareeie.com 562