Three-Step vs Six-Step PWM in Three-Phase Boost PFC Rectifier

Telechargé par Chaymae Zouheir
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Transactions on Power Electronics
Performance Comparison of Three-Step and Six-Step PWM
in Average-Current-Controlled
Three-Phase Six-Switch Boost PFC Rectifier
Laszlo Huber, Misha Kumar, and Milan M. Jovanović
Abstract – In this paper, a three-step PWM method for the
average-current-controlled three-phase six-switch boost PFC
rectifier is proposed. It is shown that the three-step PWM
compared to the conventional six-step PWM exhibits a lower
total harmonic distortion of input currents and higher power
factor. However, the three-step PWM, unlike the six-step
PWM, is adversely affected by duty-cycle limitations and has
unbalanced conduction losses of the upper and lower switches of
the three-phase rectifier bridge. The average-current control
with three-step and six-step PWM is illustrated with
Matlab/Simulink simulation waveforms and experimentally
verified on a 3-kW prototype.
Index Terms –Three-phase six-switch boost PFC rectifier,
average-current control, three-step PWM, six-step PWM,
discontinuous space-vector modulation (SVM), segment
detection, duty-cycle limitation, low-pass filtering and sampling,
zero-sequence signal (ZSS) injection, total harmonic distortion
(THD), power factor (PF)
I. INTRODUCTION
Today, active three-phase PFC rectifiers need to meet very
challenging performance requirements. In the majority of
applications, the input current of active three-phase PFC
rectifiers is required to have a total harmonic distortion
(THD) less than 5% and a power factor (PF) greater than 0.99
[1]. One of the most cost-effective topologies that can meet
these requirements is the three-phase six-switch boost PFC
rectifier [2], which is usually implemented without neutral-
point connection.
A number of control methods that can achieve a high
quality of input currents in the three-phase six-switch boost
PFC rectifier are available [3], [4]. Generally, approaches
using direct control of input current versus, for example,
direct power control, result in better quality of the input
currents [5]. Today, the control circuit is usually
implemented with digital technology. One direct current
control method, well suited for digital implementation, is the
average current control [6], [7].
In three-wire, three-phase applications, because the sum of
the phase currents is zero, the control can be implemented by
having only two out of three current controllers actively
shaping the current at a given time. The desired current in the
inactive-controller phase is obtained by the sum of currents of
the actively controlled phases. One implementation of this
control method is based on dividing the line cycle of the input
phase voltages into six 60o segments (six-step PWM) as
shown in Fig. 1(a) [8], [9]. In each 60o segment, the
controller in the phase with the highest absolute value voltage
is disabled, i.e., switches in the corresponding leg are turned
off, which results in reduced switching losses.
In this paper, another implementation of this control
method is proposed. It is based on dividing the line cycle of
the input phase voltages into three 120o segments (three-step
PWM) as shown in Fig. 2. In each 120o segment, the
controller in the phase with the most positive (or most
negative) phase voltage is disabled, i.e., the switches in the
corresponding leg are turned off. The three-step PWM is
equivalent to the discontinuous space-vector modulation
(SVM) with unbalanced conduction losses between the upper
and lower switches [10].
A detailed performance comparison of the three-step and
six-step PWM in the average-current controlled three-phase
six-switch boost PFC rectifier is also provided in the paper.
It is shown that the three-step PWM compared to the six-step
PWM exhibits lower THD of input currents and higher PF.
The operation of the three-step and six-step PWM is
illustrated with Matlab/Simulink simulation waveforms and
experimentally verified on a 3-kW prototype.
II. AVERAGE CURRENT CONTROL WITH THREE-STEP AND
SIX-STEP PWM
In the six-step PWM, a line cycle of input phase voltages is
divided into six 60o segments such that within a 60o segment
none of the three phase voltages changes sign, as shown in
Fig. 1(a). In each 60o segment, the controller in the phase
with the highest absolute value voltage is disabled, i.e.,
switches in the corresponding leg are turned off. For
example, in segment I, the controller in phase “a” is disabled,
i.e., switches Sap and San are turned off, as shown in Fig. 1(b).
The simplified circuit diagram of the three-phase six-switch
boost PFC rectifier with six-step PWM in segment I is shown
in Fig. 1(c). Since in segment I, the leg in phase “a” is
disabled and phase current ia is positive, rectifier input aR is
connected to the positive output rail (through diode Dap). By
sinusoidal modulation of switches in legs “b” and “c”,
desired sinusoidal average phase-to-phase voltages vaRbR and
vaRcR can be generated between the rectifier inputs,
respectively. As the sum of the phase-phase voltages at the
rectifier inputs must be zero, desired voltage vbRcR is
0885-8993 (c) 2015 IEEE. Personal use is permitted, but republication/redistribution requires IEEE permission. See http://www.ieee.org/publications_standards/publications/rights/index.html for more information.
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Transactions on Power Electronics
automatically generated. To generate sinusoidal average
phase-to-phase voltages between rectifier inputs, the current
controllers are designed to control phase-phase currents. The
output of the phase-phase-current controllers determines the
phase-phase duty cycles dab, dbc, and dca so that in steady-state
operation vaRbR=dabVo, vbRcR=dbcVo, and vcRaR=dcaVo. Switch
duty cycles dap, dbp and dcp are obtained from phase-phase
duty cycles so that dab=dap-dbp, dbc=dbp-dcp, and dca=dcp-dap.
For example, in segment I, dap=1 and, therefore, dbp=1-dab and
dcp=1+dca. It should be noted that dap=1 means that rectifier
input aR is connected to the positive output rail due to the
conduction of diode Dap. The steady-state duty cycle of all
switches is summarized in Table I, whereas, the variation of
duty cycle dap during the whole line cycle is shown in Fig. 3
as an example. As can be seen in Fig. 3, duty cycle dap
exhibits abrupt changes at 60o-segment transitions, which
induces input-current transients at the segment transitions.
These transients, which can be seen as notches and glitches in
the input current waveforms and can be regarded as segment-
transition noise, may cause false segment detection in the six-
step PWM.
In the proposed three-step PWM, a line cycle of input
phase voltages is divided into three 120o segments such that
within a 120o segment one phase voltage is always greater or
smaller than the other two phase voltages, as shown in Figs.
2(a) and 2(b), respectively. Accordingly, the three-step
PWM is either referenced to the positive or to the negative
envelope of the phase voltages. In each 120o segment, the
controller in the phase with the most positive (or most
negative) phase voltage is disabled, i.e., the switches in the
corresponding leg are turned off. Similarly to the six-step
PWM, the control goal is to generate sinusoidal average
phase-to-phase voltages between the rectifier inputs aR, bR
and cR, and, therefore, the current controllers are designed to
control the phase-phase currents. The steady-state duty
cycles of the switches operating with three-step PWM
referenced to the positive and negative envelope of the phase
voltages are summarized in Tables II and III, respectively,
whereas, the variation of the corresponding duty cycle dap
during the whole line cycle is shown in Figs. 4(a) and 4(b).
As can be seen in Fig. 4, duty cycle dap does not exhibit
abrupt changes at 120o-segment transitions. As a result, the
three-step PWM exhibits much reduced notches and glitches
at the segment transitions so that segment detection is much
less sensitive to segment-transition noise compared to that in
the six-step PWM.
Comparing duty cycle dap in Figs. 3 and 4, it can be
concluded that practical duty-cycle limitations (in order to
meet the dead-time requirements for the IGBT module and
taking into account the propagation delay times of the
optocouplers in the interface circuit between the DSP and
IGBT module) only affect the three-step PWM. As can be
seen from Fig. 3, for a minimum duty cycle Dmin=0.05 and
maximum duty cycle Dmax=0.95, as an example, the duty-
cycle limitations do not have effect on the six-step PWM
circuit operation because the duty-cycles of the switches in
the two active phases are in the 0.265-0.735 range. In Fig. 3,
when the switches in leg “a” are turned off, dap=1 in segment
I and dap=0 in segment IV is achieved through the conduction
of diodes Dap and Dan, respectively. However, for the three-
step PWM implementation, the limited duty-cycle range
affects circuit operation and its performance. As can be seen
in Fig. 4(a), at the beginning of segment II duty cycle dap is
required to continuously decrease from unity, whereas at the
end of segment III dap is required to continuously increase to
unity. However, if the maximum duty cycle is limited to
ω
t
30
a0
v b0
v c0
v
-30 90 150 210 270 330
0
I II III IV
V VI
o o o o o o
o
p
n
v
a0
vb0
v
c0
C
p
C
n
o
V
La
La
S
bp S
cp
S
an S
bn S
cn
L
b
L
c
i
a>0
i
b
<0
i
c
<0
S
ap
0
DISABLED
PHASE
aR
bR
cR
(a) (b)
(c)
Fig. 1 Six-step PWM: (a) 60o segments, (b) circuit diagram in segment I, (c) simplified circuit diagram in
segment I.
iab
iac
ibc
v
aRbR
v
aRcR
p
n
C
p
C
n
o
V
La
S
bp S
cp
S
bn S
cn
L
b
L
c
i
a>0
i
b
<0
i
c
<0
D
ap
vab>0
v
ac >0
vbc
a
b
c
aR
bR
cR
acaba iii +=
bcabb iii −=
bcacc iii +=
ω
t
60
a0
v b0
v c0
v
0 180 300 360
I II III I
o o o o o
envp
v
(a)
ω
t
0 120 360
I II III
o o o 240
o
a0
v b0
v
c0
v envn
v
(b)
Fig. 2 Three-step PWM with 120o
segments referenced to: (a) positive
envelope, (b) negative envelope of input
phase voltages.
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Transactions on Power Electronics
Dmax=0.95, the phase current will be distorted at the I-to-II
and III-to-I segment transitions. Similarly, as can be seen in
Fig. 4(b), at the end of segment I duty cycle dap is required to
decrease to zero, whereas at the beginning of segment III dap
is required to increase from zero. However, if the minimum
duty cycle is limited to Dmin=0.05, the phase current will be
distorted at the I-to-II and II-to-III segment transitions.
It should be noted that for both six-step and three-step
PWM, identical operation can be achieved if instead of
phase-to-phase-current controllers, phase-current controllers
are used with appropriate zero-sequence-signal (ZSS)
injection. The implementation with phase-current controllers
and ZSS injection is described in the next section.
III. POWER STAGE AND CONTROL CIRCUIT
The simplified circuit diagram of the three-phase six-
switch boost PFC rectifier is shown in Fig. 5. The switches
are implemented with IGBTs in a six-pack module [11]. The
switching frequency is selected as fsw = 20 kHz, which is the
maximum recommended fsw for the IGBT module. The input
phase voltage range is 120 ± 15% Vrms, 45-65 Hz, the
nominal output voltage is 400 V, and the maximum output
power is 3 kW.
The block diagram of the control circuit common for both
six-step and three-step PWM implemented with phase-phase
current controllers is also shown in Fig. 5. Average-current
control is implemented using digital signal processor (DSP)
TMS320F2808 from TI [12]. For average-current control,
the input phase-phase voltages, phase currents, and the output
voltage are sensed and converted to digital signals through
the 12-bit analog-digital converter (ADC) of the DSP. The
input voltage range of the ADC is 0-3 V, i.e., the full-scale
range FSR = 3 V. As only positive voltages can be applied to
the input of the ADC, the bipolar phase-phase voltages and
phase currents are scaled to ±FSR/2 and level shifted by
FSR/2. The output signals of the DSP are the digital PWM
(DPWM) gate signals for the bottom switches Sxn, xϵ{a,b,c}.
The DPWM operates with a triangular carrier. As the clock
frequency of the DSP is fsysclock = 100 MHz, the peak value of
the triangular carrier is Cpk = 1/2·fsysclock/fsw = 2500. All the
sensed signals are sampled at the peak of the triangular
carrier, i.e., at the middle of the turn-on time of the upper
switches. It should be noted that by sampling the inductor
currents at the middle of the turn-on time of the upper
switches, the sampled values of the inductor currents are
equal to the average values during a switching period. Since
the value of the average inductor current is directly obtained
in each sample, i.e., it is not reconstructed from several
samples, no antialiasing filter is needed for the sampled
inductor currents. Instead, the sensed current signals need to
be conditioned by a low-pass filter to remove the switching
noise. The corner frequency of the input- and output-voltage
antialiasing filters is fAAFin = 3 kHz and fAAFout = 550 Hz,
respectively, whereas the corner frequency of the low-pass
filter of the sensed inductor-currents is fLPF = 92.5 kHz.
The voltage controller is implemented with PI
compensation (for better regulation of the output voltage),
whereas, the current controller is implemented with P
compensation which exhibits better performance compared to
that with PI compensation. Namely, as it was shown in [13],
[14] for the three-phase six-switch boost PFC rectifier with
average-current control and with mismatched input-voltage
and input-current sensing gains, the current controller with P
compensation exhibits lower THD of input currents and
higher PF compared to that of PI compensation. The
average-current control implementation also includes voltage
TABLE I - STEADY-STATE DUTY-CYCLE OF SWITCHES FOR SIX-STEP PWM
60° Segment dap d
an d
bp d
bn d
cp d
cn
I 1 0
1-dab d
ab 1+dca -dca
II -dca 1+dca d
bc 1-dbc 0 1
III 1+dab -dab 1 0
1-dbc d
bc
IV 0 1
-dab 1+dab d
ca 1-dca
V 1-dca d
ca 1+dbc -dbc 1 0
VI dab 1-dab 0 1
-dbc 1+dbc
TABLE II - STEADY-STATE DUTY-CYCLE OF SWITCHES FOR THREE-STEP
PWM REFERENCED TO POSITIVE ENVELOPE OF PHASE VOLTAGES
120° Segment dap d
an d
bp d
bn d
cp d
cn
I 1 0 1-dab d
ab 1+dca -dca
II 1+dab -dab 1 0
1-dbc dbc
III 1- dca d
ca 1+dbc -dbc 1 0
TABLE III - STEADY-STATE DUTY-CYCLE OF SWITCHES FOR THREE-STEP
PWM REFERENCED TO NEGATIVE ENVELOPE OF PHASE VOLTAGES
120° Segment dap d
an d
bp d
bn d
cp d
cn
I -dca 1+ dca d
bc 1-dbc 0 1
II 0 1
-dab 1+dab d
ca 1- dca
III dab 1-dab 0 1
-dbc 1+dbc
ω
t
30
ap
d
-30 90 150 210 270 330
0
I II III
IV V VI
o o o o o o o
1
ca
d ab
d
ab
d
1 ca
d
1
0
0.735
0.265
0.95
0.05
max
D
min
D
Fig. 3 Duty cycle of upper switch in phase “a” for six-step PWM at
120Vrms input voltage.
ω
t
60
ap
d
120 180 240 300 360
0
I II III
o o o o o o o
1
I
0
ab
d
1 ca
d
1
max
D
0.95
(
a
)
ω t
ap
d
120 240 360
0
I II III
o o o o
1
0
ca
d ab
d
60
o 180
o 300
o
min
D
0.05
(b)
Fig. 4 Duty cycle of upper switch in phase “a” for three-step PWM
referenced to: (a) positive envelope, (b) negative envelope of input phase
voltages (120Vrms).
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Transactions on Power Electronics
feedforward (VFF) [6] and duty-cycle feedforward (DFF)
[15]. Generally, VFF can make the output voltage practically
insensitive to line-voltage variations. However, VFF with P-
compensated current controller is effective only if DFF is
also implemented, as shown in [13], [14].
The 60o-segments for six-step PWM are detected by using
comparators to determine the sign of the phase voltages,
whereas, the 120o-segments for three-step PWM are detected
by comparing the phase voltages. Because in the six-step
PWM strong transient input-current noise is generated at 60o-
segment transitions, additional measures are taken to improve
the reliability of the 60o-segment detection. First, the
segment detection is disabled if the absolute value of the sum
of the sensed and sampled phase voltages is significantly
greater than zero, i.e., if |va0+vb0+vc0| > ΔVzero. Second, after
a new segment is detected, the segment detection is disabled
for a specified blanking time Tblank to prevent noise-induced
segment change due to false segment detection. In the
experimental circuit, the segment detection is implemented
with ΔVzero = 13V and Tblank = 9Tsw = 450 μs.
It should be noted that in order to meet the dead-time
requirements for the IGBT module [11] and taking into
account the propagation delay times of the optocouplers in
the interface circuit between the DSP and IGBT module [16],
the duty cycle range is limited from Dmin=0.05 to Dmax =0.95.
The block diagram of the control circuit common for both
six-step and three-step PWM implemented with phase-
current controllers and ZSS injection is shown in Fig. 6. ZSS
signal vZSS for the six-step PWM, shown in Fig. 7, is obtained
from the input phase voltages and the output reference
voltage as
<−−
≥−
=
envnenvpenvn
oref
envnenvpenvp
oref
ZSS vvifv
V
vvifv
V
v
2
2 , (1)
while ZSS signals for the three-step PWM referenced to the
positive and negative envelope of input phase voltages,
shown in Figs. 8(a) and (b), respectively, are defined as
envp
oref
ZSS v
V
v−= 2
, (2)
and
envn
oref
ZSS v
V
v−−= 2
. (3)
It can be observed in Figs. 7 and 8 that the sum of phase
voltage va0 and ZSS voltage vZSS, when divided by Voref and
level shifted by ½ will result in the same duty cycle dap as
obtained with the phase-phase-current controllers shown in
Figs. 3 and 4, respectively.
Finally, it should be noted that both the six-step PWM and
three-step PWM implemented with phase-current controllers
and ZSS injection can be equivalently implemented with
space vector modulation with appropriate distribution of the
zero switching state vectors [17], [18].
IV. PERFORMANCE COMPARISON OF THREE-STEP AND SIX-
STEP PWM
Figures 9(a) and (b) show the measured steady-state
waveforms of phase currents ia, ib, and ic at nominal phase
voltage of 120 Vrms and for 2-kW load for the six-step and
three-step PWM referenced to the negative envelope of the
phase voltages, respectively. As can be seen in Figs. 9(a) and
(b), for both six-step and three-step PWM, the phase currents
n
LINE VOLTAGE
SENSING
PHASE CURRENT
SENSING
OUTPUT VOLTAGE
SENSING
p
Sap Sbp Scp
San Scn
v
o
v
a0
v
b0
v
c0
L
L
L
i
a
i
b
i
c
Sbn
+
-
a
b
c
C
p
C
n
ANT IALIASING
FILTER
LOW-PASS
FILTER
ANTIALIASING
FILTER
Phase-Phase AB
ADC
1
FSR
ADC
v
ab
*
A C
v caSh
*
v abSh
*
v
o
*
1
FSR
*
v
ab AVG
DPWM
S
an Sap
ADC
VOLTAGE
CONT ROLLER
v
oref
*
vEA
*
K AB
C
2
mB
1.5V
i abref
*
i*
aSh
1
FSR
CURRENT
CONT ROLLER
Offset Offset
1.5V
1
3
i
bSh
*
i*
ab
d*
ab
STEP
LOGIC
d*
ca
2
FSR
v
a0
*
SEGMENT
DETECT ION
v
b0
*
v
c0
*
1
3
SEG *
SEG*
DUTY-CYCLE
FEEDFORWARD
v
ab
*
v
oref
*
VOLTAGE
FEEDFORWARD
DSP
Phase-Phase BC
Phase-Phase CA
* - notation for digital values
Fig. 5 Simplified circuit diagram of power stage (La=Lb=Lc=1mH, Cp=Cn=2240µF) and
block diagram of control circuit.
Fig. 6 Block diagram of control circuit for implementation of six-
step and three-step PWM with phase-current controllers and ZSS
injection.
n
Phase A
VOLTAGE
CONTROLLER
ADC
1
FSR
1
3
ADC
Phase B
Phase C
v
oref
*
vEA
*
i aref
*
i*
aK AB
C
2
m
v
a0
*
B
A
C
v ca
*
v ab
*
v
o
*
ADC
1
FSR
1
FSR
*
v
a0 AVG
CURRENT
CONT ROLLER
DPWM
Sap
vZSS
*
v
a0
*
ZSS INJECTION
DUTY-CYCLE
FEEDFORWARD +
ZSS
v
a0
* v*
v
oref
*
+
GENERATOR
ZERO-SEQUENCE
SIGNAL (ZSS)
vZSS
*
v
b0
*
v
c0
*
FSR
2
1*
2
Dan
*
S
an
DCCa
*
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Transactions on Power Electronics
are distorted at segment transitions. However, these
distortions are more pronounced for the six-step PWM.
Consequently, the six-step PWM has higher THD of phase
currents and lower PF compared to the three-step PWM, as
shown by respective THD and PF measurements in Figs. 9(a)
and (b).
The phase-current distortions at segment transitions are
primarily caused by the low-pass filtering and sampling of
the inductor currents. In the three-step PWM, they are also
affected by duty-cycle limitations.
To explain the distortions in the phase currents caused by
the low-pass filtering and sampling, Simulink simulations are
employed. Specifically, simulations for the six-step and
three-step PWM were performed for a decreased low-pass
corner frequency of 20 kHz, instead of 92.5 kHz used in the
experimental circuit, to amplify the effect of the low-pass
filtering for the sake of a more clear explanation. The
simulations were done without limiting the duty cycle, i.e., by
allowing the full duty-cycle range from zero to unity. The
effect of a limited duty-cycle range is addressed by a separate
set of simulations.
The results of the simulations are presented in Fig. 11,
which shows the sampled inductor-current waveforms before
and after the filtering. Specifically, in Figs. 11(c) and (e), the
waveforms of the sampled filtered and unfiltered inductor
current for the six-step and three-step PWM are compared,
respectively. The definition of sampled filter inductor current
I
xfs
, xϵ{a,b,c}, and sampled unfiltered inductor current I
xs
,
xϵ{a,b,c}, is given in Fig. 10.
As it can be observed in Fig. 11(c) for the six-step PWM,
in every 60
o
-segment, the sampled filtered inductor currents
in two actively controlled phases are greater than the
corresponding sampled unfiltered inductor currents. For
example, in the highlighted 60
o
-segment in Fig. 11(c), I
afs
>I
as
and I
cfs
>I
cs
. To facilitate the understanding of this effect, the
waveforms of input phase voltages v
x0
, xϵ{a,b,c}, and
inductor currents of phase “a”, i.e., i
a
, i
af
, i
afs
, and i
as
in Figs.
11(a)-11(c) are zoomed in around instant T
1
, where sampled
currents i
as
and i
afs
have a negative slope, and instant T
2
,
where sampled currents i
as
and i
afs
have a positive slope, as
shown in Figs. 12(a) and 12(b), respectively. As can be seen
in Fig. 12, filtered inductor current i
af
lags behind inductor
current i
a
. At the sampling instant (at the middle of a
switching period, i.e., at the middle of the turn-on time of the
upper switches), i
af
> i
a
, and, therefore, the sampled filtered
inductor current is greater than the sampled unfiltered
inductor current, i.e., i
afs
>i
as
.
The current controllers shape the sampled filtered-inductor
currents to follow the reference currents so that i
afs
+i
bfs
+i
cfs
=0.
At the same time, the sum of the three phase currents flowing
in the circuit must be zero, i.e., the sum of the sampled
unfiltered-inductor currents is also zero i
af
+i
bf
+i
cf
=0.
Therefore, if i
afs
>i
as
and i
cfs
>i
cs
, it follows that i
bfs
< i
bs
, as
shown in Fig. 11(c). Since the current in the phase of non-
active (passive) controller is greater than the actively-
controlled phase currents, at the 60
o
-segment transitions
when the role of actively and non-actively controlled currents
changes, the current of the phase transitioning to passive
control and the phase transitioning to active control exhibit
step changes. These current changes at the 60
o
-segment
transitions are primarily responsible for increased current
THD.
At 120
o
-segment transitions of the three-step PWM, the
difference between sampled filtered and sampled unfiltered
Fig. 7 ZSS signal for six-step PWM.
0
π
2
π
[ωt]
0
v
ZSS
V
a0
+v
ZSS
V
a0
2
/
V
ore
f
m
V
m
V
−
2
/
V
ore
f
−
(a)
(b)
Fig. 8 ZSS signal for three-step PWM referenced to: (a) positive envelope,
(b) negative envelope.
0
π
2
π
[ωt]
0
v
ZSS
V
a0
+v
ZSS
V
a0
2
/
V
ore
f
m
V
m
V
−
0π
2
π
[ωt]
0
vZSS
Va0
+v
ZSS
Va0
2
/
ore
f
−
m
V
m
V
−
Fig. 9 Experimental waveforms during steady-state operation (120Vrms,
2kW): phase currents I
a
, I
b
, I
c
[A] with
(a) six-step PWM, (b) three-step
PWM referenced to negative envelope of input phase voltages.
THDa=8.52%
PFa=0.9926
THDa=3.79%
PFa=0.9982
THDb=3.29%
PFb=0.9976
THDc=3.56%
PFc=0.9976
THDb=6.83%
PFb=0.9926
THDc=8.19%
PFc=0.9923
(a)
(b)
Ia Ic
Ib
Ia Ic
Ib
1 / 8 100%
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