Iqbal et al., Cogent Engineering (2016), 3: 1134040 http://dx.doi.org/10.1080/23311916.2015.1134040 ELECTRICAL & ELECTRONIC ENGINEERING | RESEARCH ARTICLE Vector control of asymmetrical six-phase synchronous motor Arif Iqbal1*, G.K. Singh1 and Vinay Pant1 Received: 22 October 2015 Accepted: 09 December 2015 First Published: 19 January 2016 *Corresponding author: Arif Iqbal, Department of Electrical Engineering, Indian Institute of Technology Roorkee, Roorkee 247667, Uttarakhand, India E-mails: arif.iqbal.in@gmail.com, arif0548@gmail.com Reviewing editor: Wei Meng, Wuhan University of Technology, China Additional information is available at the end of the article Abstract: Vector control scheme has been well adopted for higher performance applications of AC motor. Therefore, this paper presents an extensive development and investigation of vector control scheme for asymmetrical six-phase synchronous motor in a new two-axis (M–T) coordinate system. Phasor diagram has also been developed in a simplified way, followed by its implementation technique. Analytical results have been presented for four-quadrant operation of synchronous motor, employing the developed vector control scheme. In analytical control model, common mutual leakage reactance between the two winding sets occupying same stator slot has been considered. Subjects: Automation Control; Mechatronics; Systems & Controls Keywords: six-phase synchronous motor; vector control; motor drive 1. Introduction The multiphase (more than three phase) AC motor drives are used as a substitute of conventional three-phase motor in different applications particularly, in propulsion system of ship and vehicle, textile and steel industries, rolling mills, power plants, etc. This is because it offers certain potential advantages when compared with its three-phase counterpart, like reduction in space and time harmonics, reduced torque pulsation, increased power handling capability, higher reliability, etc. (Levi, 2008; Singh, 2002). Field-oriented control (i.e. vector control) technique has been widely used in high performance of AC motor drives. In this regard, an abundant number of literatures are available for three-phase motor (Bose, 2002; Das & Chattopadhyay, 1997; Jain & Ranganathan, 2011; Krause, Wasynczuk, & Sudhoff, 2004), but a few for six-phase induction motor (Bojoi, Lazzari, Profumo, & Tenconi, 2003; Singh, Nam, & Lim, 2005), wherein d–q model of machine has been used in synchronously rotating Arif Iqbal ABOUT THE AUTHOR PUBLIC INTEREST STATEMENT Arif Iqbal received his BTech and MTech degrees both in electrical engineering in 2005 and 2007, respectively, from Aligarh Muslim University, Aligarh, India. After having experience in industry and teaching in the field AC drives and power system for a few years, he is currently pursuing his PhD from Indian Institute of Technology Roorkee, India. His area of interest is multiphase AC machine and drives, power electronics, and renewable energy system. It is always advantageous to use the electrical machine with its performance at higher level using a suitable technique. Among different techniques, vector control is widely used as it provides the decoupled control of torque and flux component of machine current. Therefore, the paper explores a detailed asymmetrical six-phase synchronous motor operation employing this technique. Analysis and simulation of complete drive system has been carried out in Matlab/ Simulink environment, where dynamic behavior of motor was found to be substantially improved. It is believed that the paper will serve as a source toward higher performance of six-phase synchronous motor. © 2016 The Author(s). This open access article is distributed under a Creative Commons Attribution (CC-BY) 4.0 license. Page 1 of 10 Iqbal et al., Cogent Engineering (2016), 3: 1134040 http://dx.doi.org/10.1080/23311916.2015.1134040 reference frame. But the utilization of this scheme has not been reported for field excited six-phase synchronous motor. Therefore, the paper is dedicated to explore and develop the control technique for asymmetrical six-phase synchronous motor. In the control scheme, a new two axis (M–T coordinate) has been introduced along which the decoupled control of flux and torque is achieved. Following the inclusion of control technique, a detailed analytical results have been presented for motor operation in four quadrants. 2. Mathematical modeling For the purpose of realizing the six-phase motor, it is a common practice to split the existing threephase stator winding into two, namely a b c and a′b′c′. Both splitted stator winding sets (a b c and a′b′c′) are physically displaced 30° apart to realize asymmetrical six-phase winding configuration. Asymmetrical six-phase winding configuration yields the reduced torque pulsation (Singh, 2002, 2011) due to the elimination of lower order harmonics. On the rotor side, it is equipped with field winding fr together with the damper windings Kd and Kq along d and q-axis, respectively. The equation of the motor can be written using machine variables. But this will yield a set of nonlinear differential equations. Nonlinearity is due to the existence of inductance term which is time varying in nature. Such equations are computationally complex and time-consuming. Therefore, to simplify the motor equations with constant inductance term, it will be conveniently written in rotor reference frame using Park’s variables (Iqbal, Singh, & Pant, 2014, in press; Schiferl & Ong, 1983; Singh, 2011). v dqk = r sk i dqk + 𝜔r p 𝝍 + 𝝍 𝜔b dqk 𝜔b dqk v dqr = r dqr i dqk + p 𝝍 𝜔b dqr [ vdqk = vdk vqk rdqk = rdk { for k = [ vdqr = (3) ]T 𝜓dk [ 1, 2, vKd vfr = exfd rfr xmd (4) −𝜓qk rqk ]T (5) for winding set a b c for winding set a� b� c� vKq vfr ]T ]T rdqk = 𝜓Kd [ rKd 𝜓Kq rKq 𝜓fr rfr (6) (7) [3, 12] [ 𝜓dqr = (2) ]T [ 𝜓dqk = (1) ]T (8) (9) Equations of motor flux linkage per second may be conveniently written as the function of currents, 𝜓 = xi (10) Page 2 of 10 Iqbal et al., Cogent Engineering (2016), 3: 1134040 http://dx.doi.org/10.1080/23311916.2015.1134040 where i = [ idqk idqk ]T ,𝜓 = ]T [ 𝜓dqk 𝜓dqk x is defined in Appendix 1. The developed motor torque is expressed as 𝜏e = 𝜏e1 + 𝜏e2 (11) where τe1 and τe2 are the developed motor torque associated with winding sets a b c and a′b′c′, respectively, and expressed as 𝜏e1 = c(iq1 𝜓d1 − id1 𝜓q1 ) (12) 𝜏e2 = c(iq2 𝜓d2 − id2 𝜓q2 ) (13) with c = 3P 1 2 2 𝜔b The rotor dynamics having P number of poles is expressed as ] [ ) 𝜔r 1 1 P 1( = 𝜏e − 𝜏 l 𝜔b p 𝜔b 2 J (14) wherein, τl is the load torque, p represents the derivative function w.r.t. time and all symbols stand to their usual meaning (Iqbal et al., in press). Evaluation of motor parameters is determined from the standard test procedure (Aghamohammadi & Pourgholi, 2008; Alger, 1970; Jones, 1967). 3. Vector control scheme The operating performance of vector-controlled motor is greatly improved and similar to that of a separately excited DC motor (Bose, 2002). This is because of decoupled control of both flux component and torque component of stator current. The inclusion of vector control scheme is not similar to that of induction motor drive. The main difference lies on the fact that the air gap flux is attributed by both stator flux as well as field flux. Therefore, the resultant air gap flux will align along the axis which is different from conventional d-axis. Hence, a new (M–T) coordinate axis has been introduced wherein, the resultant flux vector and torque current component will align along M and T axis, respectively. Machine variables in newly defined coordinate axis (M–T axis) may be readily transformed to its equivalent d–q or vice versa by relation [ Mk Tk ] [ = cos𝛿k sin𝛿k −sin𝛿k cos𝛿k ][ dk qk ] (15) In above relation, the torque angle δ1 and δ2 are associated with winding sets a b c and a′b′c′, respectively, and defined as 𝛿1 = 𝛿 0 (16) 𝛿1 = 𝛿0 + � + 𝜉 (17) δ0 is the initial value of load angle, whereas ∅ is the phase difference between voltage fed to phase a and a′. Hence, torque attributed by each stator winding sets a b c and a′b′c′ is given by Equations (12) and (13) may be readily written in M–T axes, 𝜏e1 = c(𝜓M1 IT1 − 𝜓T1 IM1 ) (18) Page 3 of 10 Iqbal et al., Cogent Engineering (2016), 3: 1134040 http://dx.doi.org/10.1080/23311916.2015.1134040 Figure 1. Phasor diagram of vector-controlled six-phase synchronous motor. T2 T1 , Va = Va e qs j M1 Va s1 IM1 Is1 I T1 I T2 Is2 ØI M2 I m1 I T1 1 I m2 I T2 2 , r 1 2 I fr a M2 s2 a , fr ds 𝜏e2 = c(𝜓M2 IT2 − 𝜓T2 IM2 ) (19) where, the flux linkage ψMk and ψTk, and stator current IMk and ITk are aligned along Mk–Tk axes respectively, for winding sets a b c (for k = 1) and a′b′c′ (for k = 2). Since, the resultant armature air gap flux is only aligned along flux axis (i.e. Mk axis). Therefore, ψT1 = 0 and ψM1 = ψs1, where √ 2 2 + 𝜓T1 𝜓s1 = 𝜓M1 (20) ψT2 = 0 and ψM2 = ψs2, where √ 2 2 + 𝜓T2 𝜓s2 = 𝜓M2 (21) Hence, motor torque equation may be simplified as 𝜏e = 𝜏e1 + 𝜏e2 = c(𝜓s1 IT1 + 𝜓s2 IT2 ) (22) The developed motor torque is dependent on flux linkage ψs1 (and ψs2) and current IT1 (and IT2) which are orthogonal. This is the introduction of vector-controlled six-phase synchronous motor. The motor operation during steady state has been shown in the developed phasor diagram in Figure 1. 4. Implementation of vector control scheme The implementation of developed vector-controlled synchronous motor drive system has been shown in Figure 2. In this paper, motor operation has been investigated in constant torque region up to base speed, but same may be extended in field weakening region above base speed. In the figure, ∗ the outer speed loop is used to generate the reference value torque component of stator current ITk ∗ through a speed controller (PI controller), whereas the reference value magnetizing current Imk is generated by the flux controller (PI controller) associated with each winding sets a b c (for k = 1) and a′b′c′ (for k = 2). The reference magnetizing current is used to establish the required flux ψsk in air gap, which related to field current by the relation, � Im1 = Ifr cos 𝛿1 � Im2 = Ifr cos 𝛿2 } (23) In phasor diagram, current component IT1 (and IT2) is in the direction of T1 (and T2) axis along which the voltage vector is also aligned. Further, the magnetizing component of current Im1 (and Im2) is Page 4 of 10 Iqbal et al., Cogent Engineering (2016), 3: 1134040 http://dx.doi.org/10.1080/23311916.2015.1134040 Figure 2. Schematic diagram of vector-controlled six-phase synchronous motor drive. aligned along M1 (and M2) axis which is used to establish the flux vector ψs1 (and ψs2). At steady state, both the stator flux and armature flux vectors are orthogonal to each other, i.e. ψs1 (and ψs2) is perpendicular to ψa1 (and ψa2) as shown in phasor diagram. Therefore, at steady state, both the vectors ITk and Isk are equal i.e. IT1 = Is1 for winding set a b c (and IT2 = Is2 for winding set a′b′c′) and becomes in phase with voltage vector, signifying the motor operation at unity power factor. In control scheme, it may be noted that the magnetizing current component Im1 (and Im2) is related to field current Ifrk ∗� ∗� associated with winding sets a b c and a′b′c′. Field current commands Ifr1 and Ifr2 are synthesized using Equation (23) in feedback loop. In field control loop, the field current error is fed to the field controller (PI controller) to establish the required field excitation. It may be noted here that the magnitude of field current magnitude associated with each winding set a b c and a′b′c′ is assumed � to be same Ifr (= 0.5Ifr ). Now, the flux component of stator current is generated by � ∗ ∗ IM1 = Im1 − Ifr cos 𝛿1 � ∗ ∗ IM2 = Im2 − Ifr cos 𝛿2 } (24) Above relation will yield a finite value of IM1and IM2. But at steady state, it becomes zero (i.e. ∗ ∗ ∗ and IMk = IM2 = 0) and Equation (23) will be satisfied. As soon as stator current component ITk are synthesized for winding sets a b c (k = 1) and a′b′c′ (k = 2), the reference value of current in stationary reference frame is generated. For this purpose, following two-step transformation is carried out. ∗ ∗ ∗ IM1 (1) Current component ITk and IMk are transformed to d–q component in stationary reference frame, using angle αk in transformation in relation (15). ∗ ∗ (2) Above obtained stationary d–q component of current is transformed into its equivalent threephase current (Krause et al., 2004). The reference current generated in above steps in stationary reference frame are then compared with actual phase current of stator windings which results in current error. This current error is fed to the hysteresis current controller to regulate switching of inverter circuit feeding the motor. Page 5 of 10 Iqbal et al., Cogent Engineering (2016), 3: 1134040 http://dx.doi.org/10.1080/23311916.2015.1134040 5. Simulation results The developed system of vector-controlled six-phase synchronous motor drive was implemented in Matlab/Simulink environment. For this purpose, a 3.7-kW motor (parameters are given in Appendix 1) was operated in four quadrant. Initially, speed command was given at time t = 0.1 s. in ramp way, following to which motor starts to run at synchronous speed after time t = 0.65 s, showing its operation in first quadrant. A load of 50% of base torque was applied at time t = 1.5 s which results a small dip in speed by 0.03 rad/s, but regains its original speed (i.e. synchronous speed) after time t = 0.5 s, as shown in Figure 3. In order to examine the motor operation in second quadrant, the direction of load torque was reversed at time t = 3 s, resulting in a small increase in rotor speed by 0.05 rad/s. A small change in rotor speed due to sudden change in load torque signifies the disturbance rejection property of the drive system. A zoomed view of speed variation has been shown in Figure 3(a). Following to the change in load torque, not only the variation in q-component of stator current but also resulted a small variation in d-component of current, as shown in Figure 5. Change in stator current is also reflected in T-axis component of motor current flowing in winding sets a b c and a′b′c′, in Figures 4 and 6. In order to shift the motor operation to third quadrant, a speed reversal command was initiated at time t = 4 s in ramp way. The motor is then finally operates in reverse motoring mode after time t = 5 s at synchronous speed. Further, at time t = 6 s the load torque is reversed to operate the drive in fourth quadrant. It is important to note here that the switching of motor operation to different quadrant results in a large variation in d-component stator current whose effect is compensated by rotor field current, as shown in Figure 7(b). But the field circuit has a larger time constant, making the response slow (Das & Chattopadhyay, 1997; Jain & Ranganathan, 2011; Krause et al., 2004). This sluggish response of field circuit is substantially improved due to the magnetizing current injection along flux direction, as depicted by reference value of current in Figure 4(b and c) as well as in actual current in Figure 6(c and d). Input phase voltage fed to winding sets a b c and a′b′c′, is shown in Figure 8(a) and (b), respectively. 6. Conclusion The scheme of vector control applicable for asymmetrical six-phase synchronous motor has been developed and extensively investigated in four quadrant operation. In this control technique, stator current is maintained for motor operation at unity power factor, which minimizes the stator current Figure 3. Motor response (a) rotor speed ωr and (b) torque Te. (a) (b) Page 6 of 10 Iqbal et al., Cogent Engineering (2016), 3: 1134040 http://dx.doi.org/10.1080/23311916.2015.1134040 Figure 4. Reference current in ∗ ∗ M–T coordinate (a) IT1 , (b) IM1 ∗ and (c) IM2. (a) (b) (c) Figure 5. Stator current in d–q coordinate (a) iq1 (b) id1 (c) iq2 (d) id2. (a) (b) (c) (d) Figure 6. Actual current in M–T coordinate (a) IT1, (b) IT2 (c) IM1 and (d) IM2. (a) (b) (c) (d) Page 7 of 10 Iqbal et al., Cogent Engineering (2016), 3: 1134040 http://dx.doi.org/10.1080/23311916.2015.1134040 Figure 7. Voltage–current in field circuit (a) reference Ifr∗ , (b) actual Ifr (c) voltage Efr. (a) (b) (c) Figure 8. Inverter output voltage (a) phase a (b) phase a'. (a) (b) and hence less losses. The dynamic behavior of six-phase synchronous motor in different quadrant operation was found to be substantially improved because of the decoupled/independent control of flux as well as torque component of current along M–T axis, respectively. Furthermore, sluggish response of the rotor field circuit was also noted to be improved because of the magnetizing current injection from armature side. The present work may be further extended and investigated under different practical application with their experimental validation. Funding The authors received no direct funding for this research. Author details Arif Iqbal1 E-mail: arif.iqbal.in@gmail.com, arif0548@gmail.com ORCID ID: http://orcid.org/0000-0002-7113-6007 G.K. Singh1 E-mail: gksngfee@gmail.com Vinay Pant1 E-mail: vpantfee@gmail.com 1 Department of Electrical Engineering, Indian Institute of Technology Roorkee, Roorkee 247667, Uttarakhand, India. Page 8 of 10 Iqbal et al., Cogent Engineering (2016), 3: 1134040 http://dx.doi.org/10.1080/23311916.2015.1134040 Citation information Cite this article as: Vector control of asymmetrical six-phase synchronous motor, Arif Iqbal, G.K. Singh & Vinay Pant, Cogent Engineering (2016), 3: 1134040. References Aghamohammadi, M. R., & Pourgholi, M. (2008). Experience with SSSFR test for synchronous generator model identification using Hook–Jeeves optimization method. International Journal of System Applications, Engineering and Development, 2, 122–127. Alger, P. L. (1970). Induction machine. New York, NY: Gorden and Breach. Bojoi, R., Lazzari, M., Profumo, F., & Tenconi, A. 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IEEE Transactions on Industrial Electronics, 52, 1177–1184. http://dx.doi.org/10.1109/TIE.2005.851593 Appendix 1 Motor parameter of 3.7 kW, 6 poles, 36 slots are r1 = 0.210 Ω xmq = 3.9112 Ω rfr = 0.056 Ω r2 = 0.210 Ω xmd = 6.1732 Ω xldq = 0 rKq = 2.535 Ω xlKq = 0.66097 Ω xlm = 0.001652 Ω rKd = 140.0 Ω xlKd = 1.550 Ω xlfr = 0.2402 Ω xl1 = xl2 = 0.1758 Ω � ⎡ ⎢ ⎢ ⎢ ⎢ ⎢ ⎢ x=⎢ ⎢ ⎢ ⎢ ⎢ ⎢ ⎢ ⎣ xl1 + xlm + xmd 0 � � xlm + xmd xldq � 0 � � xl1 + xlm + xmd � � xlm + xmd −xldq � � xl2 + xlm + xmd xldq � � xlm + xmq 0 � xmd 0 0 xmq xmd 0 0 xmq � −xldq � � xlm + xmq 0 xmd 0 xmd 0 xmd 0 xmq 0xmq 0 0 xmd 0 xmd 0 xl2 + xlm + xmq � xlKd + xmd � 0 xmd � � xlKq + xmq � � xlfr + xmd xmd ⎤ 0 ⎥⎥ xmd ⎥ ⎥ 0 ⎥ ⎥ ⎥ ⎥ ⎥ ⎥ 0 ⎥⎥ ⎥ ⎦ Page 9 of 10 Iqbal et al., Cogent Engineering (2016), 3: 1134040 http://dx.doi.org/10.1080/23311916.2015.1134040 © 2016 The Author(s). This open access article is distributed under a Creative Commons Attribution (CC-BY) 4.0 license. 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