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Pulse-Width Modulation (PWM) Techniques
1
PWM FOR CONVERTERS
iNTRODUCTION
PWM Methods
A. Sine PWM
B. Hysteresis (Bang-bang)
C. Space Vector PWM
References
2
9
Pulse-Width Modulation
 Objective of PWM
 Disadvantages of PWM
 Increase of switching losses due to high PWM frequency
 Reduction of available voltage
 EMI problems due to high-order harmonics
 Control of inverter output voltage
 Reduction of harmonics
 Pulse-Width Modulation (PWM)
Fig. 5 Pulse-width modulation.
10
 Inverter output voltage
 When vcontrol > vtri, VA0 = Vdc/2
 When vcontrol < vtri, VA0 = -Vdc/2
A01A0
10
Vofcomponentfrequecnylfundamenta:)(Vwhere,
,
2/
)(
dc
A
tri
control
V
Vofpeak
v
v
m 
 Modulation Index (m)
 Control of inverter output voltage
 Amplitude is controlled by the peak value of vcontrol
 Fundamental frequency is controlled by the frequency of vcontrol
 PWM frequency is the same as the frequency of vtri
11
II. PWM METHODS
A. Sine PWM (1)
Fig. 6 Three-phase Sine PWM inverter.
 Three-phase inverter
12
II. PWM METHODS
A. Sine PWM (2)
V
A0
V
B0
V
C0
V
AB
V
BC
V
CA
t
Fig. 7 Waveforms of three-phase sine PWM inverter.
 Three-phase sine PWM waveforms
vtri vcontrol_A vcontrol_
B
vcontrol_C
where, VAB = VA0 – VB0
VBC = VB0 – VC0
VCA = VC0 – VA0
 When vcontrol > vtri, VA0 = Vdc/2
 When vcontrol < vtri, VA0 = -Vdc/2
 Frequency of vtri = fs
 Frequency of vcontrol = f1
 Frequency of vtri and vcontrol
where, fs = PWM frequency
f1 = Fundamental frequency
 Inverter output voltage
13
II. PWM METHODS
A. Sine PWM (3)
 Amplitude modulation ratio (ma)
A01A0
10
Vofcomponentfrequecnylfundamenta:)(Vwhere,
,
2/
)(
dc
A
tri
control
a
V
Vofvaluepeak
vofamplitude
vofamplitudepeak
m 
 Frequency modulation ratio (mf)
frequencylfundamentafandfrequencyPWMfwhere,, 1s
1

f
f
m s
f
 mf should be an odd integer
 if mf is not an integer, there may exist sunhamonics at output voltage
 if mf is not odd, DC component may exist and even harmonics are present at output voltage
 mf should be a multiple of 3 for three-phase PWM inverter
 An odd multiple of 3 and even harmonics are suppressed
14
II. PWM METHODS
B. Hysteresis (Bang-bang) PWM (1)
 Three-phase inverter for hysteresis Current Control
Fig. 8 Three-phase inverter for hysteresis current control.
15
II. PWM METHODS
B. Hysteresis (Bang-bang) PWM (2)
 Hysteresis Current Controller
Fig. 9 Hysteresis current controller at Phase “a”.
16
II. PWM METHODS
B. Hysteresis (Bang-bang) PWM (3)
 Characteristics of hysteresis Current Control
 Advantages
 Drawbacks
17
 Excellent dynamic response
 Low cost and easy implementation
 Large current ripple in steady-state
 Variation of switching frequency
 No intercommunication between each hysterisis controller of three phases
and hence no strategy to generate zero-voltage vectors.
As a result, the switching frequency increases at lower modulation index and
the signal will leave the hysteresis band whenever the zero vector is turned on.
 The modulation process generates subharmonic components
 Output voltages of three-phase inverter (1)
Fig. 10 Three-phase power inverter.
II. PWM METHODS
C. Space Vector PWM (1)
where, upper transistors: S1, S3, S5
lower transistors: S4, S6, S2
switching variable vector: a, b, c
18
II. PWM METHODS
C. Space Vector PWM (2)
t
dc
ca
bc
ab
c]b[avectorvariableswitchingwhere,
c
b
a
101
110
011
V
V
V
V




































































c
b
a
211
121
112
V
3
1
V
V
V
dc
cn
bn
an
 Output voltages of three-phase inverter (2)
 S1 through S6 are the six power transistors that shape the ouput voltage
 When an upper switch is turned on (i.e., a, b or c is “1”), the corresponding lower
switch is turned off (i.e., a', b' or c' is “0”)
 Line to line voltage vector [Vab Vbc Vca]t
 Line to neutral (phase) voltage vector [Van Vbn Vcn]t
 Eight possible combinations of on and off patterns for the three upper transistors (S1, S3, S5)
19
II. PWM METHODS
C. Space Vector PWM (3)
 Output voltages of three-phase inverter (3)
 The eight inverter voltage vectors (V0 to V7)
20
II. PWM METHODS
C. Space Vector PWM (4)
 Output voltages of three-phase inverter (4)
 The eight combinations, phase voltages and output line to line voltages
21
II. PWM METHODS
C. Space Vector PWM (5)
 Principle of Space Vector PWM
 This PWM technique approximates the reference voltage Vref by a combination
of the eight switching patterns (V0 to V7)
 The vectors (V1 to V6) divide the plane into six sectors (each sector: 60 degrees)
 Vref is generated by two adjacent non-zero vectors and two zero vectors
 CoordinateTransformation (abc reference frame to the stationary d-q frame)
: A three-phase voltage vector is transformed into a vector in the stationary d-q coordinate
frame which represents the spatial vector sum of the three-phase voltage
 Treats the sinusoidal voltage as a constant amplitude vector rotating
at constant frequency
22
II. PWM METHODS
C. Space Vector PWM (6)
 Basic switching vectors and Sectors
Fig. 11 Basic switching vectors and sectors.
 6 active vectors (V1,V2, V3, V4, V5, V6)
 Axes of a hexagonal
 DC link voltage is supplied to the load
 Each sector (1 to 6): 60 degrees
 2 zero vectors (V0, V7)
 At origin
 No voltage is supplied to the load
23
II. PWM METHODS
C. Space Vector PWM (7)
 Comparison of Sine PWM and Space Vector PWM (1)
Fig. 12 Locus comparison of maximum linear control voltage
in Sine PWM and SV PWM.
24
II. PWM METHODS
C. Space Vector PWM (8)
 Comparison of Sine PWM and Space Vector PWM (2)
 Space Vector PWM generates less harmonic distortion
in the output voltage or currents in comparison with sine PWM
 Space Vector PWM provides more efficient use of supply voltage
in comparison with sine PWM
 Sine PWM
: Locus of the reference vector is the inside of a circle with radius of 1/2 Vdc
 Space Vector PWM
: Locus of the reference vector is the inside of a circle with radius of 1/3 Vdc
 Voltage Utilization: Space Vector PWM = 2/3 times of Sine PWM
25
II. PWM METHODS
C. Space Vector PWM (9)
 Realization of Space Vector PWM
 Step 1. Determine Vd, Vq, Vref, and angle ()
 Step 2. Determine time duration T1, T2, T0
 Step 3. Determine the switching time of each transistor (S1 to S6)
26


































cn
bn
an
q
d
V
V
V
2
3
2
3
0
2
1
2
1
1
3
2
V
V
frequency)lfundamentaf(where,
t2ππtω)
V
V
(tanα
VVV
s
ss
d
q1
2
q
2
dref




II. PWM METHODS
C. Space Vector PWM (10)
Fig. 13 Voltage Space Vector and its components in (d, q).
cnbnan
cnbnq
cnbnan
cnbnand
V
2
3
V
2
3
V
cos30Vcos30V0V
V
2
1
V
2
1
V
cos60Vcos60VVV




 Step 1. Determine Vd, Vq, Vref, and angle ()
 Coordinate transformation
: abc to dq
27
II. PWM METHODS
C. Space Vector PWM (11)
Fig. 14 Reference vector as a combination of adjacent vectors at sector 1.
 Step 2. Determine time duration T1, T2, T0 (1)
28
II. PWM METHODS
C. Space Vector PWM (12)
 Switching time duration at Sector 1
















dc
ref
s
z210
2
1
V
3
2
V
aand
f
1
Twhere,),(
)3/(sin
)(sin
)3/(sin
)3/(sin
TTTT
aTT
aTT
z
z
z




)60α0(where,
)3/(sin
)3/(cos
V
3
2
T
0
1
V
3
2
T
)(sin
)(cos
VT
)VTV(TVT
VdtVdtVV
dc2dc1
refz
2211refz
T
TT
0
TT
T1
2
T
0
T
0
1ref
z
21
21z 1






















   

π
π
α
α
 Step 2. Determine time duration T1, T2, T0 (2)
29
II. PWM METHODS
C. Space Vector PWM (13)
 Switching time duration at any Sector
 Step 2. Determine time duration T1, T2, T0 (3)














 
















 
































 



60α0
6)toSector1is,(that6through1nwhere,
,
3
1
cossin
3
1
sincos
3
3
1
sin
3
sin
3
coscos
3
sin
3
3
sin
3
3
1
3
sin
3
210
2
1
TTTT
nn
V
refVT
n
V
refVT
T
nn
V
refVT
n
V
refVT
n
V
refVT
T
z
dc
z
dc
z
dc
z
dc
z
dc
z






30
II. PWM METHODS
C. Space Vector PWM (14)
Fig. 15 Space Vector PWM switching patterns at each sector.
(a) Sector 1. (b) Sector 2.
 Step 3. Determine the switching time of each transistor (S1 to S6) (1)
31
II. PWM METHODS
C. Space Vector PWM (15)
Fig. 15 Space Vector PWM switching patterns at each sector.
(c) Sector 3. (d) Sector 4.
 Step 3. Determine the switching time of each transistor (S1 to S6) (2)
32
II. PWM METHODS
C. Space Vector PWM (16)
Fig. 15 Space Vector PWM switching patterns at each sector.
(e) Sector 5. (f) Sector 6.
 Step 3. Determine the switching time of each transistor (S1 to S6) (3)
33
II. PWM METHODS
C. Space Vector PWM (17)
Table 1. Switching Time Table at Each Sector
 Step 3. Determine the switching time of each transistor (S1 to S6) (4)
34
III. REFERENCES
[1] N. Mohan, W. P. Robbin, and T. Undeland, Power Electronics: Converters,
Applications, and Design, 2nd ed. New York: Wiley, 1995.
[2] B. K. Bose, Power Electronics and Variable Frequency Drives:Technology
and Applications. IEEE Press, 1997.
[3] H.W. van der Broeck, H.-C. Skudelny, and G.V. Stanke, “Analysis and
realization of a pulsewidth modulator based on voltage space vectors,”
IEEE Transactions on Industry Applications, vol.24, pp. 142-150, 1988.
35

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Pwm techniques for converters

  • 1. Pulse-Width Modulation (PWM) Techniques 1 PWM FOR CONVERTERS
  • 2. iNTRODUCTION PWM Methods A. Sine PWM B. Hysteresis (Bang-bang) C. Space Vector PWM References 2
  • 3. 9 Pulse-Width Modulation  Objective of PWM  Disadvantages of PWM  Increase of switching losses due to high PWM frequency  Reduction of available voltage  EMI problems due to high-order harmonics  Control of inverter output voltage  Reduction of harmonics
  • 4.  Pulse-Width Modulation (PWM) Fig. 5 Pulse-width modulation. 10
  • 5.  Inverter output voltage  When vcontrol > vtri, VA0 = Vdc/2  When vcontrol < vtri, VA0 = -Vdc/2 A01A0 10 Vofcomponentfrequecnylfundamenta:)(Vwhere, , 2/ )( dc A tri control V Vofpeak v v m   Modulation Index (m)  Control of inverter output voltage  Amplitude is controlled by the peak value of vcontrol  Fundamental frequency is controlled by the frequency of vcontrol  PWM frequency is the same as the frequency of vtri 11
  • 6. II. PWM METHODS A. Sine PWM (1) Fig. 6 Three-phase Sine PWM inverter.  Three-phase inverter 12
  • 7. II. PWM METHODS A. Sine PWM (2) V A0 V B0 V C0 V AB V BC V CA t Fig. 7 Waveforms of three-phase sine PWM inverter.  Three-phase sine PWM waveforms vtri vcontrol_A vcontrol_ B vcontrol_C where, VAB = VA0 – VB0 VBC = VB0 – VC0 VCA = VC0 – VA0  When vcontrol > vtri, VA0 = Vdc/2  When vcontrol < vtri, VA0 = -Vdc/2  Frequency of vtri = fs  Frequency of vcontrol = f1  Frequency of vtri and vcontrol where, fs = PWM frequency f1 = Fundamental frequency  Inverter output voltage 13
  • 8. II. PWM METHODS A. Sine PWM (3)  Amplitude modulation ratio (ma) A01A0 10 Vofcomponentfrequecnylfundamenta:)(Vwhere, , 2/ )( dc A tri control a V Vofvaluepeak vofamplitude vofamplitudepeak m   Frequency modulation ratio (mf) frequencylfundamentafandfrequencyPWMfwhere,, 1s 1  f f m s f  mf should be an odd integer  if mf is not an integer, there may exist sunhamonics at output voltage  if mf is not odd, DC component may exist and even harmonics are present at output voltage  mf should be a multiple of 3 for three-phase PWM inverter  An odd multiple of 3 and even harmonics are suppressed 14
  • 9. II. PWM METHODS B. Hysteresis (Bang-bang) PWM (1)  Three-phase inverter for hysteresis Current Control Fig. 8 Three-phase inverter for hysteresis current control. 15
  • 10. II. PWM METHODS B. Hysteresis (Bang-bang) PWM (2)  Hysteresis Current Controller Fig. 9 Hysteresis current controller at Phase “a”. 16
  • 11. II. PWM METHODS B. Hysteresis (Bang-bang) PWM (3)  Characteristics of hysteresis Current Control  Advantages  Drawbacks 17  Excellent dynamic response  Low cost and easy implementation  Large current ripple in steady-state  Variation of switching frequency  No intercommunication between each hysterisis controller of three phases and hence no strategy to generate zero-voltage vectors. As a result, the switching frequency increases at lower modulation index and the signal will leave the hysteresis band whenever the zero vector is turned on.  The modulation process generates subharmonic components
  • 12.  Output voltages of three-phase inverter (1) Fig. 10 Three-phase power inverter. II. PWM METHODS C. Space Vector PWM (1) where, upper transistors: S1, S3, S5 lower transistors: S4, S6, S2 switching variable vector: a, b, c 18
  • 13. II. PWM METHODS C. Space Vector PWM (2) t dc ca bc ab c]b[avectorvariableswitchingwhere, c b a 101 110 011 V V V V                                                                     c b a 211 121 112 V 3 1 V V V dc cn bn an  Output voltages of three-phase inverter (2)  S1 through S6 are the six power transistors that shape the ouput voltage  When an upper switch is turned on (i.e., a, b or c is “1”), the corresponding lower switch is turned off (i.e., a', b' or c' is “0”)  Line to line voltage vector [Vab Vbc Vca]t  Line to neutral (phase) voltage vector [Van Vbn Vcn]t  Eight possible combinations of on and off patterns for the three upper transistors (S1, S3, S5) 19
  • 14. II. PWM METHODS C. Space Vector PWM (3)  Output voltages of three-phase inverter (3)  The eight inverter voltage vectors (V0 to V7) 20
  • 15. II. PWM METHODS C. Space Vector PWM (4)  Output voltages of three-phase inverter (4)  The eight combinations, phase voltages and output line to line voltages 21
  • 16. II. PWM METHODS C. Space Vector PWM (5)  Principle of Space Vector PWM  This PWM technique approximates the reference voltage Vref by a combination of the eight switching patterns (V0 to V7)  The vectors (V1 to V6) divide the plane into six sectors (each sector: 60 degrees)  Vref is generated by two adjacent non-zero vectors and two zero vectors  CoordinateTransformation (abc reference frame to the stationary d-q frame) : A three-phase voltage vector is transformed into a vector in the stationary d-q coordinate frame which represents the spatial vector sum of the three-phase voltage  Treats the sinusoidal voltage as a constant amplitude vector rotating at constant frequency 22
  • 17. II. PWM METHODS C. Space Vector PWM (6)  Basic switching vectors and Sectors Fig. 11 Basic switching vectors and sectors.  6 active vectors (V1,V2, V3, V4, V5, V6)  Axes of a hexagonal  DC link voltage is supplied to the load  Each sector (1 to 6): 60 degrees  2 zero vectors (V0, V7)  At origin  No voltage is supplied to the load 23
  • 18. II. PWM METHODS C. Space Vector PWM (7)  Comparison of Sine PWM and Space Vector PWM (1) Fig. 12 Locus comparison of maximum linear control voltage in Sine PWM and SV PWM. 24
  • 19. II. PWM METHODS C. Space Vector PWM (8)  Comparison of Sine PWM and Space Vector PWM (2)  Space Vector PWM generates less harmonic distortion in the output voltage or currents in comparison with sine PWM  Space Vector PWM provides more efficient use of supply voltage in comparison with sine PWM  Sine PWM : Locus of the reference vector is the inside of a circle with radius of 1/2 Vdc  Space Vector PWM : Locus of the reference vector is the inside of a circle with radius of 1/3 Vdc  Voltage Utilization: Space Vector PWM = 2/3 times of Sine PWM 25
  • 20. II. PWM METHODS C. Space Vector PWM (9)  Realization of Space Vector PWM  Step 1. Determine Vd, Vq, Vref, and angle ()  Step 2. Determine time duration T1, T2, T0  Step 3. Determine the switching time of each transistor (S1 to S6) 26
  • 21.                                   cn bn an q d V V V 2 3 2 3 0 2 1 2 1 1 3 2 V V frequency)lfundamentaf(where, t2ππtω) V V (tanα VVV s ss d q1 2 q 2 dref     II. PWM METHODS C. Space Vector PWM (10) Fig. 13 Voltage Space Vector and its components in (d, q). cnbnan cnbnq cnbnan cnbnand V 2 3 V 2 3 V cos30Vcos30V0V V 2 1 V 2 1 V cos60Vcos60VVV      Step 1. Determine Vd, Vq, Vref, and angle ()  Coordinate transformation : abc to dq 27
  • 22. II. PWM METHODS C. Space Vector PWM (11) Fig. 14 Reference vector as a combination of adjacent vectors at sector 1.  Step 2. Determine time duration T1, T2, T0 (1) 28
  • 23. II. PWM METHODS C. Space Vector PWM (12)  Switching time duration at Sector 1                 dc ref s z210 2 1 V 3 2 V aand f 1 Twhere,),( )3/(sin )(sin )3/(sin )3/(sin TTTT aTT aTT z z z     )60α0(where, )3/(sin )3/(cos V 3 2 T 0 1 V 3 2 T )(sin )(cos VT )VTV(TVT VdtVdtVV dc2dc1 refz 2211refz T TT 0 TT T1 2 T 0 T 0 1ref z 21 21z 1                            π π α α  Step 2. Determine time duration T1, T2, T0 (2) 29
  • 24. II. PWM METHODS C. Space Vector PWM (13)  Switching time duration at any Sector  Step 2. Determine time duration T1, T2, T0 (3)                                                                        60α0 6)toSector1is,(that6through1nwhere, , 3 1 cossin 3 1 sincos 3 3 1 sin 3 sin 3 coscos 3 sin 3 3 sin 3 3 1 3 sin 3 210 2 1 TTTT nn V refVT n V refVT T nn V refVT n V refVT n V refVT T z dc z dc z dc z dc z dc z       30
  • 25. II. PWM METHODS C. Space Vector PWM (14) Fig. 15 Space Vector PWM switching patterns at each sector. (a) Sector 1. (b) Sector 2.  Step 3. Determine the switching time of each transistor (S1 to S6) (1) 31
  • 26. II. PWM METHODS C. Space Vector PWM (15) Fig. 15 Space Vector PWM switching patterns at each sector. (c) Sector 3. (d) Sector 4.  Step 3. Determine the switching time of each transistor (S1 to S6) (2) 32
  • 27. II. PWM METHODS C. Space Vector PWM (16) Fig. 15 Space Vector PWM switching patterns at each sector. (e) Sector 5. (f) Sector 6.  Step 3. Determine the switching time of each transistor (S1 to S6) (3) 33
  • 28. II. PWM METHODS C. Space Vector PWM (17) Table 1. Switching Time Table at Each Sector  Step 3. Determine the switching time of each transistor (S1 to S6) (4) 34
  • 29. III. REFERENCES [1] N. Mohan, W. P. Robbin, and T. Undeland, Power Electronics: Converters, Applications, and Design, 2nd ed. New York: Wiley, 1995. [2] B. K. Bose, Power Electronics and Variable Frequency Drives:Technology and Applications. IEEE Press, 1997. [3] H.W. van der Broeck, H.-C. Skudelny, and G.V. Stanke, “Analysis and realization of a pulsewidth modulator based on voltage space vectors,” IEEE Transactions on Industry Applications, vol.24, pp. 142-150, 1988. 35