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Proceedings of the Pakistan Academy of Sciences 51 (3): 201–208 (2014) Pakistan Academy of Sciences 
Copyright © Pakistan Academy of Sciences 
ISSN: 0377 - 2969 (print), 2306 - 1448 (online) 
Research Article 
Performance of Six-Pulse Line-Commutated Converter in 
DC Motor Drive Application 
Syed Riaz ul Hassnain1, Haider Zaman1, Zunaib Ali1, Muqadsa Iftikhar1, 
and Tariqullah Jan2* 
1University of Engineering & Technology Peshawar, Abbottabad Campus, Pakistan 
2University of Engineering & Technology, Peshawar, Pakistan 
Abstract: This paper presents the speed control of DC motor using six pulse controlled rectifier. The 
conventional Proportional Integral (PI) control is used for firing angle control. The armature current is fed 
back and compared with reference current representing desired speed values. The proposed system is 
simulated using SimPowerSystem and Control System Matlab toolbox. The time domain plot of reference 
and actual armature current are shown in results section. The results are satisfactory with deleterious effect 
on input current. The frequency plot of input current is provided to show the harmonic contents, generated 
as a result of control operation. 
Keywords: Silicon control rectifier (SCR), DC motor, proportional integral control, harmonics, displacement 
factor and distortion factor, line-commutated converter (LCC) 
1. INTRODUCTION 
The continuous popularity of DC motors is due to 
their efficient performance and control advantages 
over ac motors. The scope of DC motor varies 
from high speed automation to electric vehicles. 
The dc motors are increasingly used in 
applications where speed or torque needs to be 
varied and controlled with high accuracy. The 
most commonly used DC motors for variable 
speed are series and separately excited [1], but 
generally DC series motor is used for traction 
purposes. 
With the development of high power solid 
state switches, the DC motor control applications 
started to grow almost exponentially. Today, 
broadly two methods are employed (based on 
switches controllability) to set the applied voltage 
as a variable parameter. In the first method applied 
voltage can be made variable by using controlled 
rectifiers which provide variable DC from a fixed 
ac shown in Fig. 1(a) whereas in the second 
method uncontrolled rectifiers are used to produce 
a fixed DC from a fixed ac and at the output of 
rectifier a DC chopper circuit is used which 
provide variable DC just by changing the duty 
cycle shown in Fig. 1(b) [2]. 
In this paper our major focus is to discuss the 
use of SCR based converters for speed regulation 
i.e. to get variable DC voltage from a fixed ac 
voltage. The use of SCR allows simple voltage 
variability just by varying the firing angle and 
thereby the speed of the motor. For the speed 
regulation of DC motor, the speed needs to be 
monitored as the speed of DC motor changes with 
load torque [3]. The control circuit corrects the 
firing angle of SCR, which in-turn changes the 
armature voltage, thereby regulating the speed. 
The control circuit used here consists of PI current 
controller, which takes current as feedback, 
compares it to the reference and then generates 
firing angle of SCRs to minimize the error and 
regulate the speed [4-5]. The benefits of feedback 
network (which is also called closed loop control 
system) are of high level of accuracy, 
compensation of load variations and system 
nonlinearities, fast response and continuous 
monitoring of process [6]. The block diagram of 
DC motor fed with closed loop controlled rectifier 
is shown on Fig. 2. 
First, the mathematical model of DC motor is 
developed in section 2. Working principle of six 
———————————————— 
Received, July 2014; Accepted, August 2014 
*Corresponding Author: Tariqullah Jan, Email: tariqullahjan@nwfpuet.edu.pk
202 Syed Riaz ul Hassnain et al 
Fig. 1(a). Controlled rectifier fed motor. 
Fig. 1(b). Uncontrolled rectifier followed by DC-DC converter. 
Fig. 2. Block diagram of DC motor fed with closed loop controlled rectifier. 
Fig. 3. Separetly excited DC motor.
Performance of Six-Pulse Line-Commutated Converter in DC Motor Drive Application 203 
pulse line-commutated converter is described in 
section 3. The section 4 presents the complete 
system responses under a transient condition, 
followed by a conclusion. 
2. DC MOTOR MODELING 
The equivalent circuit of commonly used DC 
motor i.e. separately excited DC motor is shown in 
Fig. 3. In case of separately excited DC motor the 
armature circuit and field circuit is independent of 
each other. When the armature current ݅஺ is passed 
through the armature circuit placed in a magnetic 
field produced by field current ݅௙passing through 
the field circuit, the motor produces a back 
electromotive force ܧ஺ and induced torque ߬௜௡ௗ , 
which balance the load torque at a particular 
speed. For separately excited DC motor, the 
current passing through the field windings is 
independent of the current passing through 
armature windings. The transient and steady state 
analysis of separately excited DC motor is derived 
using Fig. 3. 
Transient Analysis 
The instantaneous field current is given by 
differential equation: 
ܸ௙ ൌ ݅௙ܴ௙ ൅ ܮ௙ 
ௗ௜೑ 
ௗ௧ (1) 
The instantaneous armature current can be 
calculated from: 
ܸ஺ ൌ ݅஺ܴ஺ ൅ ܮ஺ 
ௗ௜ಲ 
ௗ௧ ൅ ܧ஺ (2) 
Where ܧ஺ is back emf of the motor and is given by 
ܧ஺ܭ߱݅௙ (3) 
The torque induced by the motor ߬௜௡ௗ is: 
߬௜௡ௗ ൌ ܭ݅௙݅஺ (4) 
The induced torque in terms of load torque is: 
߬௜௡ௗ ൌ ܬ ௗఠ 
ௗ௧ ൅ ܤɘ ൅ ߬௟௢௔ௗ (5) 
Where, 
߱ ൌ a‰—Žar s’‡‡d ሺrad⁄sሻ 
ܤ ൌ …‘s–a– ‘ˆ ˜‹s…‘—s ˆr‹…–‹‘ ൬N. 
m 
rad⁄s 
൰ 
ܭ ൌ ˜‘Ž–a‰‡ …‘s–a– ሺ⁄ െ radȀs) 
ܮ஺ ൌ arma–—r‡ …‹r…—‹– ‹d—…–a…‡ ሺሻ 
ܮ௙ ൌ ˆ‹‡Žd …‹r…—‹– ‹d—…–a…‡ ሺሻ 
ܴ஺ ൌ arma–—r‡ …‹r…—‹– r‡s‹s–a…‡ ሺπሻ 
ܴ௙ ൌ ˆ‹‡Žd …‹r…—‹– r‡s‹s–a…‡ ሺπሻ 
߬௟௢௔ௗ ൌ Ž‘ad –‘r“—‡ ሺN. mሻ 
ܬ ൌ ‘m‡– ‘ˆ ‹‡r–‹a 
Steady-state Analysis 
For the steady state analysis all the derivatives 
with respect to time are put to zero. The resulting 
steady state average quantities are: 
ܸ௙ ൌ ܫ௙ܴ௙ (6) 
ܸ஺ ൌ ܫ஺ܴ஺ ൅ ܧ஺ 
ൌ ܫ஺ܴ஺ ൅ ܭ߱ܫ௙ (7) 
߬௜௡ௗ ൌ ܭܫ௙ܫ஺ 
ൌ ɘ ൅ ߬௟௢௔ௗ (8) 
The power induced or developed is: 
ܲ௜௡ௗ ൌ ߬௜௡ௗ߱ (9) 
In modeling of DC motor, the main concern is to 
find the relationship between speed of DC motor 
and armature voltage. The speed of the separately 
excited DC motor in terms of armature voltage can 
be derived using ܧݍ. ሺ͹ሻ i.e. 
߱ ൌ ௏ಲିூಲோಲ 
௄ூ೑ 
(10) 
Using ܧݍ. ሺ͸ሻ,ܫ௙ ൌ ܸ௙⁄ܴ௙ 
߱ ൌ ௏ಲିூಲோಲ 
௄௏೑⁄ோ೑ (11) 
From ܧݍ. ሺͳͳሻ it is cleared that the speed of motor 
is directly related to armature voltage ܸ஺, larger 
the armature voltage greater will be the speed and 
vice versa[6]. The type of control in which the 
controlling parameter is voltage, is called voltage 
control. In practice, the armature and filed currents 
are kept constant to fulfill the demand of torque 
while armature voltage is made variable to control 
the speed. So, in this study a DC motor is fed with 
the output of a three phase SCR bridge. 
3. WORKING PRINCIPLE OF SIX PULSE 
CONVERTER 
The circuit diagram for 3-phase six pulse 
controlled rectifier is shown in the Fig. 4.The 
circuit consist of six thyristors, i.e.,
204 Syed Riaz ul Hassnain et al 
Fig. 4. Six pulse controlled rectifier. 
Fig. 5. The૜׎ line to line voltage waveform ࢂሺ࣓࢚ሻ, converter output voltage waveform ࢂ࢕ሺ࣓࢚ሻ, phase Dzࢇdz current 
waveform ࢏ࢇሺ࣓࢚ሻ.
Performance of Six-Pulse Line-Commutated Converter in DC Motor Drive Application 205 
ܶଵ,ܶଶ,ܶଷ,ܶସ,ܶହand ܶ଺ for rectification purpose. 
Three phase system consist of three sinusoidal 
input voltages (ܸ௔ǡ ܸ௕ܸ௖) with same frequency 
and magnitudes i.e. (݂௔ ൌ ݂௕ ൌ ݂௖ ൌ ݂)  
(ܸ௠௔ ൌ ܸ௠௕ ൌ ܸ௠௖ ൌ ܸ௠) but shifted 120° from 
each other. The operating principle of the circuit is 
that, the pair of SCR connected between the lines 
havinghighest amount of line-to-line voltage will 
conduct provided that the gate signal is applied to 
SCRs at that instant. i.e. SCR needs gate signal in 
addition to ܸ஺௄ ൐ 0. The input and output voltage 
wavefroms and input current waveform for phase 
“ܽ” are shown in Fig. 5. 
Between 0 ൑ ߱ݐ ൑ ߨ 
ൗ3 the highest line-to-line 
voltage is ܸ௖௕, with ܶସ ܶହ intially 
conducting. By firing ܶ଺ at delay angle of ߙ,results 
ܸ௖௕at load. It should be noted is that ܸ௖௕apperas 
across load till ߨ 
ൗ3 ൅ ߙ. Although beyond the 
point ߨ 
ൗ3 the line-to-line voltage ܸ௔௕ has the 
highest value but until ܶଵ is not fired, it will not 
appear across the load and the maximum voltage 
across load is still ܸ௖௕.As ܶଵ is fired, ܶହ turns off 
and now current passes through ܶଵ ܶ଺ i.e. ܸ௔௕ 
appears across the load. Another impotant 
conclusion is that, only one SCR needed to be 
fired at a time except for the first cycle. Because 
first SCR of the pair already conducts due to phase 
sequence. 
From Fig. 5 it can be seen that frequency 
of output pulsating voltage is ͸݂ and in this way 
the harmonic components are shifted to higher 
frequencyAs compare to three pulse converter, it 
reduces the need of filtering at the output[7-8].The 
output DC voltage of a controlled rectifier is a 
function of the firing angle ߙ and it can be 
calculated from Fig. 5. The relation is: 
ܸௗ௖ ൌ 
1 
ߨ 
ൗ3 
ఈାଶగ 
ൗଷ 
න √3ܸ௠ sinሺ߱ݐሻ ݀ሺ߱ݐሻ 
ఈାగ 
ൗଷ 
ሺ12ሻ 
ܸௗ௖ ൌ 
3√3ܸ௠ 
ߨ 
ఈାଶగ 
ൗଷ 
න sinሺ߱ݐሻ ݀ሺ߱ݐሻ 
ఈାగ 
ൗଷ 
ܸௗ௖ ൌ 
3√3ܸ௠ 
ߨ 
െcosሺ߱ݐሻ 
ߙ ൅ 2ߨ 
ێێێێ 
ۏ 
ൗ3 
ߙ ൅ ߨ 
ൗ3 
ܸௗ௖ ൌ 
െ3√3ܸ௠ 
ߨ 
ൗ3൯ െ cos൫ߙ ൅ ߨ 
ൣcos൫ߙ ൅ 2ߨ 
ൗ3൯൧ 
ܸௗ௖ ൌ 
3√3ܸ௠ 
ߨ 
cosሺߙሻ ሺ13ሻ 
ܸௗ௖ ൌ ܸௗ௠ cosሺߙሻ ሺ14ሻ 
ܸ௡ ൌ 
ܸௗ௖ 
ܸௗ௠ 
cosሺߙሻ ሺ1ͷሻ 
Where ܸௗ௠ is the average output voltage atߙ ൌ 
0and ܸ௡ is normanilzed average voltage.The plot 
in Fig. 6 shows the normalized output DC voltage 
verses the firing angle ߙ. 
It can be seen from Fig. 5 that for ߙ ൌ ߨ 
ൗ3 
the rectified output voltage reaches zero crossing. 
If ߙ is increased beyond ߨ 
ൗ3 i.e. ߙ ൐ ߨ 
ൗ3, the load 
voltage becomses discontinous for resistive load 
where as for inductive load the negative voltage 
appears across load. Fig. 6 shows that by varying 
ߙ between 0 ݐ݋ ߨ 
ൗ2 output varies between 1  0 
i.e. rectification region and by varying ߙ between 
ߨ 
ൗ2 ݐ݋ ߨ output varies between 0  െ 1 i.e. 
inversion region. Rectification region is 
represented by 1ୱ୲Quardant and inversion region 
by 4୲୦Quardant resulting in 2 Quardant 
operation. 
There is also an issue in using six pulse 
converter i.e. the effect of converter on input 
power factor. The power factor for highly 
inductive load (motor) can be calculated as: 
ܲ௔௩ 
ܲ. ܨ ൌ 
3 ܸ௜௥௠௦ ܫ௜௥௠௦ 
ܲ. ܨ ൌ 
͸ ܸ௠ ܫ௢ 
3 ܫ௢ߨ ή ܸ௠⁄√2 
cosሺߙሻ 
ܲ. ܨ ൌ 0.9 cosሺߙሻ ሺ1͸ሻ 
From ܧݍ. ሺ1͹ሻ it can be seen that by varying ߙ 
between 0 ݐ݋ߨ , the power factor also vary 
between 0.9  0for rectification region and 
0  െ 0.9 for inversion region. 
4. RESULTS AND DISCUSSION 
The circuit consist of sixpulse line-commutated 
converter (LCC), DC motor and the control 
system; consisting of PI controller is simulated 
using Simulink. The simulated system is shown in 
the Fig. 7. The Synchronized 6-Pulse Generator
206 Syed Riaz ul Hassnain et al 
Rectification Region Inversion Region 
0 0.5 1 1.5 2 2.5 3 
1 
0.5 
0 
-0.5 
-1 
α (rad) 
Normalized Average Voltage 
Fig. 6. Normalized average voltage as function of ࢻǤ 
Source Impedence DC motor equivalent circuit 
Iref 
IA 
Fig. 7. Model for speed control of DC motor. 
208 V rms L-L 
3-phase Source 
DIstortion Factor 
30 
25 
20 
15 
10 
5 
Fig. 8. Variation of Motor Current Corresponding to Reference Current. 
Continuous 
[A] 
phase a Current 
+ i-ia 
alpha plot 
Vo  IA+Iref 
v +- 
Vo 
v +- 
Vca 
Vc 
v +- 
Vbc 
Vb 
v +- 
Vab 
Va 
g 
A 
B 
C 
+ 
- 
Thyristor Converter 
alpha_deg 
AB 
BC 
CA 
Block 
pulses 
Synchronized 
6-Pulse Generator 
Input Current 
DSPF 
Power Factor 
Power Factor Calculation 
0.5043 
Power Factor 
alpha_deg Dif f 
PI Controller 
Mux 
Iref 
+ i- 
Id 
0.9589 
Distortion Factor 
0.526 
Displacement Factor 
0 
[A] 
Vo 
0 0.02 0.04 0.06 0.08 0.1 
0 
Time (sec) 
Motor and Reference Current 
Motor Current Id 
Reference Current Idref
Performance of Six-Pulse Line-Commutated Converter in DC Motor Drive Application 207 
0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 0.1 
120 
100 
80 
60 
40 
Fig. 9. Variation in ࢻ to achieve desired Reference Current. 
300 
250 
200 
150 
100 
50 
0 
-50 
Fig. 10. Variation inconverter output to achieve desired Reference Current. 
100 
80 
60 
40 
20 
Fig. 11. Frequency Specturm for ࢻ ൌ ࣊ 
ൗ૟ 
20 
Time (sec) 
α (degree) 
0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 0.1 
-100 
Time (sec) 
LCC Output 
0 60 120 180 240 300 360 420 480 540 600 660 
0 
α=π/6 
Frequency Hz 
Normalized Harmonic Magnitude
208 Syed Riaz ul Hassnain et al 
block is used here to fire the six thyristors 
(Thyristor Bridge) of a six-pulse converter. The 
output of the block is a vector of six pulses 
individually synchronized on the six thyristor 
voltages. The DC motor is modelled as series 
connected RL and a DC source, where the DC 
source representing the back emf. 
In this paper the speed is controlled by 
conrolling the current through the motor. For a 
desired value of speed, the reference current is 
provided and using PI controlled the reference 
current is achieved in a little time. Thetime 
domain plot for variation of motor armature 
current ܫ஺ for corresponding reference current ܫ௥௘௙ 
is shown in Fig. 8. The pattern of firing angle ߙ 
and LCC output voltage for desired ܫ௥௘௙ is shown 
in Fig. 9 and Fig. 10, respectively. Fig. 8 shows 
that intially, the current through the motor was 
zero but when the value of reference current is set 
as 10, the motor current started increasing from 
zero level and reached the same level as reference 
current within microseconds. As the reference 
current is achieved, current through the motor 
remained constant for the rest of time. Again, 
when after sometime the reference current is 
varied from 10 ݐ݋ ʹͷ, the motor achieved and 
maintained the same current, which implies that 
the current is regulated. The current regulation 
directly implies that the speed is also regulated. 
One of the important issue needed to be 
analyzed, is the effect of converter on input power 
factor because according to ܧݍǤ ሺ1͹ሻ the power 
factor is the function of firing angle ߙ. The power 
factor block in Fig. 7 is used to compute the power 
factor . Power factor is product of displacement 
factor(due to phase difference between voltage and 
fundamental component of input current) and 
distortion factor(due to distortion in input current). 
For different values of ߙ, the value of distortion 
and displacement factor is listed in Table.1. For 
ߙ ൌ ߨ 
ൗ6 specturm of input current is shown in 
Fig. 11 
Table 1. Six pulse converter power factor, 
distortion factor and displacement factor for 
different α’s. 
ࢻ Displacement 
Factor 
Distortion 
Factor 
Power 
Factor 
ߨ 
ൗ6 0.758 0.975 0.739 
ߨ 
ൗ4 0.639 0.967 0.618 
ߨ 
ൗ3 0.487 0.955 0.465 
5. CONCLUSIONS 
The line-commutated converter with conventional 
PI control was used for speed regulation of DC 
motor. The system was tested for the step change 
in reference current and it provided satisfactory 
results. When the load torque increases due to 
extra load i.e.߬௟௢௔ௗ ൐ ߬௜௡ௗ, the motor speed 
ultimately decreases, this will increase the 
error ݁. To minimize the error the PI controller 
changes the firing angle of SCR to increase the 
voltage ܸ஺ applied to the armature of DC motor, 
which increases the armature current ܫ஺, thereby 
increasing the speed of DC motor. The problem 
arises at low speed values (i.e. large values ofߙ) as 
displacement factor reduces by keeping ߙ large. 
6. REFRENCES 
1. Kushwah, R.  S. Wadhwani. Speed control of 
separately excited DC motor using fuzzy logic 
controller. International Journal of Engineering 
Trends and Technology 4(6): 2518-2523 (2013). 
2. Afrasiabi, N.  M.H. Yazdi. DC motor control using 
chopper. Global Journal of Science Engineering and 
Technology 8: 67-73 (2013). 
3. Shastri, S.  P. Pandey. A comparative analysis of 
firing angle based speed control scheme of DC motor. 
International Journal of Engineering Research and 
Applications 3(4): 232-235 (2013). 
4. Jaiswal, M.  M. Phadnis. Speed control of DC 
motor using genetic algorithm based PID controller. 
International Journal of Advanced Research in 
Computer Science and Software Engineering 3(7): 
247-253 (2013). 
5. Pal, A.K.  R.K. Mudi. Speed control of DC motor 
using relay feedback tuned PI, fuzzy PI and self-tuned 
fuzzy pi controller. Control Theory and Informatics 
2(1): 24-32 (2012). 
6. Rashid, M.H. Multilevel inverters. In: Alice Dworkin, 
and Dona King. Power Electronics Circuits, Devices 
and Applications, 3rd ed. Pearson Education, p. 409- 
419 (2003). 
7. Pyakuryal, S.  M.A. Matin, Feedback controller for 
a 3-phase 6-pulse rectifier. The International Journal 
of Engineering and Science 2(8): 23-27 (2013). 
8. Pyakuryal, S.  M. Matin. Harmonic analysis for a 6- 
pulse rectifier. International Organization of 
Scientific Research Journal of Engineering 3 (3): 57- 
60 (2013). 
9. Nedeljkovic, M.  Z. Stojiljkovic. Fast current 
control for thyristor rectifiers. IEE Proceedings- 
Electric Power Applications 15(6): 636- 638 (2003). 
10. Gupta, R., R. Lamba  S. Padhee. Thyristor based 
speed control techniques of DC motor: A 
Comparative Analysis. International Journal of 
Scientific and Research Publications 2(6): 1-6 (2012).

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Performance of Six-Pulse Line-Commutated Converter in DC Motor Drive Application

  • 1. Proceedings of the Pakistan Academy of Sciences 51 (3): 201–208 (2014) Pakistan Academy of Sciences Copyright © Pakistan Academy of Sciences ISSN: 0377 - 2969 (print), 2306 - 1448 (online) Research Article Performance of Six-Pulse Line-Commutated Converter in DC Motor Drive Application Syed Riaz ul Hassnain1, Haider Zaman1, Zunaib Ali1, Muqadsa Iftikhar1, and Tariqullah Jan2* 1University of Engineering & Technology Peshawar, Abbottabad Campus, Pakistan 2University of Engineering & Technology, Peshawar, Pakistan Abstract: This paper presents the speed control of DC motor using six pulse controlled rectifier. The conventional Proportional Integral (PI) control is used for firing angle control. The armature current is fed back and compared with reference current representing desired speed values. The proposed system is simulated using SimPowerSystem and Control System Matlab toolbox. The time domain plot of reference and actual armature current are shown in results section. The results are satisfactory with deleterious effect on input current. The frequency plot of input current is provided to show the harmonic contents, generated as a result of control operation. Keywords: Silicon control rectifier (SCR), DC motor, proportional integral control, harmonics, displacement factor and distortion factor, line-commutated converter (LCC) 1. INTRODUCTION The continuous popularity of DC motors is due to their efficient performance and control advantages over ac motors. The scope of DC motor varies from high speed automation to electric vehicles. The dc motors are increasingly used in applications where speed or torque needs to be varied and controlled with high accuracy. The most commonly used DC motors for variable speed are series and separately excited [1], but generally DC series motor is used for traction purposes. With the development of high power solid state switches, the DC motor control applications started to grow almost exponentially. Today, broadly two methods are employed (based on switches controllability) to set the applied voltage as a variable parameter. In the first method applied voltage can be made variable by using controlled rectifiers which provide variable DC from a fixed ac shown in Fig. 1(a) whereas in the second method uncontrolled rectifiers are used to produce a fixed DC from a fixed ac and at the output of rectifier a DC chopper circuit is used which provide variable DC just by changing the duty cycle shown in Fig. 1(b) [2]. In this paper our major focus is to discuss the use of SCR based converters for speed regulation i.e. to get variable DC voltage from a fixed ac voltage. The use of SCR allows simple voltage variability just by varying the firing angle and thereby the speed of the motor. For the speed regulation of DC motor, the speed needs to be monitored as the speed of DC motor changes with load torque [3]. The control circuit corrects the firing angle of SCR, which in-turn changes the armature voltage, thereby regulating the speed. The control circuit used here consists of PI current controller, which takes current as feedback, compares it to the reference and then generates firing angle of SCRs to minimize the error and regulate the speed [4-5]. The benefits of feedback network (which is also called closed loop control system) are of high level of accuracy, compensation of load variations and system nonlinearities, fast response and continuous monitoring of process [6]. The block diagram of DC motor fed with closed loop controlled rectifier is shown on Fig. 2. First, the mathematical model of DC motor is developed in section 2. Working principle of six ———————————————— Received, July 2014; Accepted, August 2014 *Corresponding Author: Tariqullah Jan, Email: tariqullahjan@nwfpuet.edu.pk
  • 2. 202 Syed Riaz ul Hassnain et al Fig. 1(a). Controlled rectifier fed motor. Fig. 1(b). Uncontrolled rectifier followed by DC-DC converter. Fig. 2. Block diagram of DC motor fed with closed loop controlled rectifier. Fig. 3. Separetly excited DC motor.
  • 3. Performance of Six-Pulse Line-Commutated Converter in DC Motor Drive Application 203 pulse line-commutated converter is described in section 3. The section 4 presents the complete system responses under a transient condition, followed by a conclusion. 2. DC MOTOR MODELING The equivalent circuit of commonly used DC motor i.e. separately excited DC motor is shown in Fig. 3. In case of separately excited DC motor the armature circuit and field circuit is independent of each other. When the armature current ݅஺ is passed through the armature circuit placed in a magnetic field produced by field current ݅௙passing through the field circuit, the motor produces a back electromotive force ܧ஺ and induced torque ߬௜௡ௗ , which balance the load torque at a particular speed. For separately excited DC motor, the current passing through the field windings is independent of the current passing through armature windings. The transient and steady state analysis of separately excited DC motor is derived using Fig. 3. Transient Analysis The instantaneous field current is given by differential equation: ܸ௙ ൌ ݅௙ܴ௙ ൅ ܮ௙ ௗ௜೑ ௗ௧ (1) The instantaneous armature current can be calculated from: ܸ஺ ൌ ݅஺ܴ஺ ൅ ܮ஺ ௗ௜ಲ ௗ௧ ൅ ܧ஺ (2) Where ܧ஺ is back emf of the motor and is given by ܧ஺ܭ߱݅௙ (3) The torque induced by the motor ߬௜௡ௗ is: ߬௜௡ௗ ൌ ܭ݅௙݅஺ (4) The induced torque in terms of load torque is: ߬௜௡ௗ ൌ ܬ ௗఠ ௗ௧ ൅ ܤɘ ൅ ߬௟௢௔ௗ (5) Where, ߱ ൌ a‰—Žar s’‡‡d ሺrad⁄sሻ ܤ ൌ …‘s–a– ‘ˆ ˜‹s…‘—s ˆr‹…–‹‘ ൬N. m rad⁄s ൰ ܭ ൌ ˜‘Ž–a‰‡ …‘s–a– ሺ⁄ െ radȀs) ܮ஺ ൌ arma–—r‡ …‹r…—‹– ‹d—…–a…‡ ሺሻ ܮ௙ ൌ ˆ‹‡Žd …‹r…—‹– ‹d—…–a…‡ ሺሻ ܴ஺ ൌ arma–—r‡ …‹r…—‹– r‡s‹s–a…‡ ሺπሻ ܴ௙ ൌ ˆ‹‡Žd …‹r…—‹– r‡s‹s–a…‡ ሺπሻ ߬௟௢௔ௗ ൌ Ž‘ad –‘r“—‡ ሺN. mሻ ܬ ൌ ‘m‡– ‘ˆ ‹‡r–‹a Steady-state Analysis For the steady state analysis all the derivatives with respect to time are put to zero. The resulting steady state average quantities are: ܸ௙ ൌ ܫ௙ܴ௙ (6) ܸ஺ ൌ ܫ஺ܴ஺ ൅ ܧ஺ ൌ ܫ஺ܴ஺ ൅ ܭ߱ܫ௙ (7) ߬௜௡ௗ ൌ ܭܫ௙ܫ஺ ൌ ɘ ൅ ߬௟௢௔ௗ (8) The power induced or developed is: ܲ௜௡ௗ ൌ ߬௜௡ௗ߱ (9) In modeling of DC motor, the main concern is to find the relationship between speed of DC motor and armature voltage. The speed of the separately excited DC motor in terms of armature voltage can be derived using ܧݍ. ሺ͹ሻ i.e. ߱ ൌ ௏ಲିூಲோಲ ௄ூ೑ (10) Using ܧݍ. ሺ͸ሻ,ܫ௙ ൌ ܸ௙⁄ܴ௙ ߱ ൌ ௏ಲିூಲோಲ ௄௏೑⁄ோ೑ (11) From ܧݍ. ሺͳͳሻ it is cleared that the speed of motor is directly related to armature voltage ܸ஺, larger the armature voltage greater will be the speed and vice versa[6]. The type of control in which the controlling parameter is voltage, is called voltage control. In practice, the armature and filed currents are kept constant to fulfill the demand of torque while armature voltage is made variable to control the speed. So, in this study a DC motor is fed with the output of a three phase SCR bridge. 3. WORKING PRINCIPLE OF SIX PULSE CONVERTER The circuit diagram for 3-phase six pulse controlled rectifier is shown in the Fig. 4.The circuit consist of six thyristors, i.e.,
  • 4. 204 Syed Riaz ul Hassnain et al Fig. 4. Six pulse controlled rectifier. Fig. 5. The૜׎ line to line voltage waveform ࢂሺ࣓࢚ሻ, converter output voltage waveform ࢂ࢕ሺ࣓࢚ሻ, phase Dzࢇdz current waveform ࢏ࢇሺ࣓࢚ሻ.
  • 5. Performance of Six-Pulse Line-Commutated Converter in DC Motor Drive Application 205 ܶଵ,ܶଶ,ܶଷ,ܶସ,ܶହand ܶ଺ for rectification purpose. Three phase system consist of three sinusoidal input voltages (ܸ௔ǡ ܸ௕ܸ௖) with same frequency and magnitudes i.e. (݂௔ ൌ ݂௕ ൌ ݂௖ ൌ ݂) (ܸ௠௔ ൌ ܸ௠௕ ൌ ܸ௠௖ ൌ ܸ௠) but shifted 120° from each other. The operating principle of the circuit is that, the pair of SCR connected between the lines havinghighest amount of line-to-line voltage will conduct provided that the gate signal is applied to SCRs at that instant. i.e. SCR needs gate signal in addition to ܸ஺௄ ൐ 0. The input and output voltage wavefroms and input current waveform for phase “ܽ” are shown in Fig. 5. Between 0 ൑ ߱ݐ ൑ ߨ ൗ3 the highest line-to-line voltage is ܸ௖௕, with ܶସ ܶହ intially conducting. By firing ܶ଺ at delay angle of ߙ,results ܸ௖௕at load. It should be noted is that ܸ௖௕apperas across load till ߨ ൗ3 ൅ ߙ. Although beyond the point ߨ ൗ3 the line-to-line voltage ܸ௔௕ has the highest value but until ܶଵ is not fired, it will not appear across the load and the maximum voltage across load is still ܸ௖௕.As ܶଵ is fired, ܶହ turns off and now current passes through ܶଵ ܶ଺ i.e. ܸ௔௕ appears across the load. Another impotant conclusion is that, only one SCR needed to be fired at a time except for the first cycle. Because first SCR of the pair already conducts due to phase sequence. From Fig. 5 it can be seen that frequency of output pulsating voltage is ͸݂ and in this way the harmonic components are shifted to higher frequencyAs compare to three pulse converter, it reduces the need of filtering at the output[7-8].The output DC voltage of a controlled rectifier is a function of the firing angle ߙ and it can be calculated from Fig. 5. The relation is: ܸௗ௖ ൌ 1 ߨ ൗ3 ఈାଶగ ൗଷ න √3ܸ௠ sinሺ߱ݐሻ ݀ሺ߱ݐሻ ఈାగ ൗଷ ሺ12ሻ ܸௗ௖ ൌ 3√3ܸ௠ ߨ ఈାଶగ ൗଷ න sinሺ߱ݐሻ ݀ሺ߱ݐሻ ఈାగ ൗଷ ܸௗ௖ ൌ 3√3ܸ௠ ߨ െcosሺ߱ݐሻ ߙ ൅ 2ߨ ێێێێ ۏ ൗ3 ߙ ൅ ߨ ൗ3 ܸௗ௖ ൌ െ3√3ܸ௠ ߨ ൗ3൯ െ cos൫ߙ ൅ ߨ ൣcos൫ߙ ൅ 2ߨ ൗ3൯൧ ܸௗ௖ ൌ 3√3ܸ௠ ߨ cosሺߙሻ ሺ13ሻ ܸௗ௖ ൌ ܸௗ௠ cosሺߙሻ ሺ14ሻ ܸ௡ ൌ ܸௗ௖ ܸௗ௠ cosሺߙሻ ሺ1ͷሻ Where ܸௗ௠ is the average output voltage atߙ ൌ 0and ܸ௡ is normanilzed average voltage.The plot in Fig. 6 shows the normalized output DC voltage verses the firing angle ߙ. It can be seen from Fig. 5 that for ߙ ൌ ߨ ൗ3 the rectified output voltage reaches zero crossing. If ߙ is increased beyond ߨ ൗ3 i.e. ߙ ൐ ߨ ൗ3, the load voltage becomses discontinous for resistive load where as for inductive load the negative voltage appears across load. Fig. 6 shows that by varying ߙ between 0 ݐ݋ ߨ ൗ2 output varies between 1 0 i.e. rectification region and by varying ߙ between ߨ ൗ2 ݐ݋ ߨ output varies between 0 െ 1 i.e. inversion region. Rectification region is represented by 1ୱ୲Quardant and inversion region by 4୲୦Quardant resulting in 2 Quardant operation. There is also an issue in using six pulse converter i.e. the effect of converter on input power factor. The power factor for highly inductive load (motor) can be calculated as: ܲ௔௩ ܲ. ܨ ൌ 3 ܸ௜௥௠௦ ܫ௜௥௠௦ ܲ. ܨ ൌ ͸ ܸ௠ ܫ௢ 3 ܫ௢ߨ ή ܸ௠⁄√2 cosሺߙሻ ܲ. ܨ ൌ 0.9 cosሺߙሻ ሺ1͸ሻ From ܧݍ. ሺ1͹ሻ it can be seen that by varying ߙ between 0 ݐ݋ߨ , the power factor also vary between 0.9 0for rectification region and 0 െ 0.9 for inversion region. 4. RESULTS AND DISCUSSION The circuit consist of sixpulse line-commutated converter (LCC), DC motor and the control system; consisting of PI controller is simulated using Simulink. The simulated system is shown in the Fig. 7. The Synchronized 6-Pulse Generator
  • 6. 206 Syed Riaz ul Hassnain et al Rectification Region Inversion Region 0 0.5 1 1.5 2 2.5 3 1 0.5 0 -0.5 -1 α (rad) Normalized Average Voltage Fig. 6. Normalized average voltage as function of ࢻǤ Source Impedence DC motor equivalent circuit Iref IA Fig. 7. Model for speed control of DC motor. 208 V rms L-L 3-phase Source DIstortion Factor 30 25 20 15 10 5 Fig. 8. Variation of Motor Current Corresponding to Reference Current. Continuous [A] phase a Current + i-ia alpha plot Vo IA+Iref v +- Vo v +- Vca Vc v +- Vbc Vb v +- Vab Va g A B C + - Thyristor Converter alpha_deg AB BC CA Block pulses Synchronized 6-Pulse Generator Input Current DSPF Power Factor Power Factor Calculation 0.5043 Power Factor alpha_deg Dif f PI Controller Mux Iref + i- Id 0.9589 Distortion Factor 0.526 Displacement Factor 0 [A] Vo 0 0.02 0.04 0.06 0.08 0.1 0 Time (sec) Motor and Reference Current Motor Current Id Reference Current Idref
  • 7. Performance of Six-Pulse Line-Commutated Converter in DC Motor Drive Application 207 0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 0.1 120 100 80 60 40 Fig. 9. Variation in ࢻ to achieve desired Reference Current. 300 250 200 150 100 50 0 -50 Fig. 10. Variation inconverter output to achieve desired Reference Current. 100 80 60 40 20 Fig. 11. Frequency Specturm for ࢻ ൌ ࣊ ൗ૟ 20 Time (sec) α (degree) 0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 0.1 -100 Time (sec) LCC Output 0 60 120 180 240 300 360 420 480 540 600 660 0 α=π/6 Frequency Hz Normalized Harmonic Magnitude
  • 8. 208 Syed Riaz ul Hassnain et al block is used here to fire the six thyristors (Thyristor Bridge) of a six-pulse converter. The output of the block is a vector of six pulses individually synchronized on the six thyristor voltages. The DC motor is modelled as series connected RL and a DC source, where the DC source representing the back emf. In this paper the speed is controlled by conrolling the current through the motor. For a desired value of speed, the reference current is provided and using PI controlled the reference current is achieved in a little time. Thetime domain plot for variation of motor armature current ܫ஺ for corresponding reference current ܫ௥௘௙ is shown in Fig. 8. The pattern of firing angle ߙ and LCC output voltage for desired ܫ௥௘௙ is shown in Fig. 9 and Fig. 10, respectively. Fig. 8 shows that intially, the current through the motor was zero but when the value of reference current is set as 10, the motor current started increasing from zero level and reached the same level as reference current within microseconds. As the reference current is achieved, current through the motor remained constant for the rest of time. Again, when after sometime the reference current is varied from 10 ݐ݋ ʹͷ, the motor achieved and maintained the same current, which implies that the current is regulated. The current regulation directly implies that the speed is also regulated. One of the important issue needed to be analyzed, is the effect of converter on input power factor because according to ܧݍǤ ሺ1͹ሻ the power factor is the function of firing angle ߙ. The power factor block in Fig. 7 is used to compute the power factor . Power factor is product of displacement factor(due to phase difference between voltage and fundamental component of input current) and distortion factor(due to distortion in input current). For different values of ߙ, the value of distortion and displacement factor is listed in Table.1. For ߙ ൌ ߨ ൗ6 specturm of input current is shown in Fig. 11 Table 1. Six pulse converter power factor, distortion factor and displacement factor for different α’s. ࢻ Displacement Factor Distortion Factor Power Factor ߨ ൗ6 0.758 0.975 0.739 ߨ ൗ4 0.639 0.967 0.618 ߨ ൗ3 0.487 0.955 0.465 5. CONCLUSIONS The line-commutated converter with conventional PI control was used for speed regulation of DC motor. The system was tested for the step change in reference current and it provided satisfactory results. When the load torque increases due to extra load i.e.߬௟௢௔ௗ ൐ ߬௜௡ௗ, the motor speed ultimately decreases, this will increase the error ݁. To minimize the error the PI controller changes the firing angle of SCR to increase the voltage ܸ஺ applied to the armature of DC motor, which increases the armature current ܫ஺, thereby increasing the speed of DC motor. The problem arises at low speed values (i.e. large values ofߙ) as displacement factor reduces by keeping ߙ large. 6. REFRENCES 1. Kushwah, R. S. Wadhwani. Speed control of separately excited DC motor using fuzzy logic controller. International Journal of Engineering Trends and Technology 4(6): 2518-2523 (2013). 2. Afrasiabi, N. M.H. Yazdi. DC motor control using chopper. Global Journal of Science Engineering and Technology 8: 67-73 (2013). 3. Shastri, S. P. Pandey. A comparative analysis of firing angle based speed control scheme of DC motor. International Journal of Engineering Research and Applications 3(4): 232-235 (2013). 4. Jaiswal, M. M. Phadnis. Speed control of DC motor using genetic algorithm based PID controller. International Journal of Advanced Research in Computer Science and Software Engineering 3(7): 247-253 (2013). 5. Pal, A.K. R.K. Mudi. Speed control of DC motor using relay feedback tuned PI, fuzzy PI and self-tuned fuzzy pi controller. Control Theory and Informatics 2(1): 24-32 (2012). 6. Rashid, M.H. Multilevel inverters. In: Alice Dworkin, and Dona King. Power Electronics Circuits, Devices and Applications, 3rd ed. Pearson Education, p. 409- 419 (2003). 7. Pyakuryal, S. M.A. Matin, Feedback controller for a 3-phase 6-pulse rectifier. The International Journal of Engineering and Science 2(8): 23-27 (2013). 8. Pyakuryal, S. M. Matin. Harmonic analysis for a 6- pulse rectifier. International Organization of Scientific Research Journal of Engineering 3 (3): 57- 60 (2013). 9. Nedeljkovic, M. Z. Stojiljkovic. Fast current control for thyristor rectifiers. IEE Proceedings- Electric Power Applications 15(6): 636- 638 (2003). 10. Gupta, R., R. Lamba S. Padhee. Thyristor based speed control techniques of DC motor: A Comparative Analysis. International Journal of Scientific and Research Publications 2(6): 1-6 (2012).