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By Andrew Levido
Power
Electronics
Part 5: power factor correction & EMI filtering
In last month’s article, we mentioned the importance of power factor for an efficient
electrical grid. This time, we will look at some active techniques that can help in this
regard. We will also cover EMI filtering, which is related in the sense that it is also
concerned with the mitigation of unwanted current harmonics.
E
lectromagnetic interference (EMI)
is a general term for any disturbance caused by an electromagnetic field that negatively impacts
the performance of electrical or electronic equipment. EMI can be radiated
through space or conducted from one
device to another through signal or
power cables.
While you can (and should) take
steps to make sure your designs are not
susceptible to EMI produced by other
devices, your main focus should be on
making sure your designs are not producing unacceptable levels of EMI that
could affect other equipment.
EMI standards such as EN55032
require radiated emissions in the
30MHz to 1GHz range to be below
certain field strength thresholds when
tested with a standard antenna at a distance of 10m. Mitigating radiated EMI
requires close attention to shielding
of enclosures, grounding, minimising
conductor loop areas, optimising PCB
layout, the use of ground planes and
controlling the slew rate of signals.
Conducted EMI
We will focus on conducted EMI,
specifically signals that are conducted
back into the power source by switching converters. The standards are generally concerned with frequencies
in the 150kHz to 30MHz range, and
require the level of signals within to
fall below specified thresholds over
different parts of the band, typically
measured using a spectrum analyser.
To give you an idea of what is
required, conducted EMI for a Class
A device must be below 79dBµV from
150kHz to 500kHz and below 73dBµV
from 500kHz to 30MHz when measured with a ‘quasi-peak’ detector. The
dBµV units describe the amplitude of
the conducted emissions with respect
to a 1µV reference. 79dBµV is therefore about 9mV RMS and 73dBµV is
about 4.5mV RMS.
Requirements for Class B devices
are considerably lower.
EMI is usually managed by the
addition of filters on the lines. The
switching frequency of many modern
converters is higher than 150kHz, so
the converter’s input filter plays a critical role in meeting conducted EMI
specifications. Fig.1 shows a standard
buck converter with a simple capacitive input filter Cf and with source
impedance Zs.
Our task is to analyse this filter and
ensure that the voltage amplitude of
the switching-frequency ripple (and
its harmonics) is below the required
threshold.
So far in this series, we have used
average value analysis to understand
the converter’s periodic steady-state
(PSS) operation and complex frequency analysis to determine the converter’s dynamic performance. Neither
of these will help us now, so we will
revert to good old AC time-domain
analysis.
This is a technique which, as its
name suggests, ignores the DC component of the signal and focuses on
the AC component. For example, the
PSS model shows us that the input current (ix) of the converter in Fig.1 has
a rectangular shape with a duty cycle
D and an amplitude of Il as shown in
the upper chart there.
If we remove the DC component of
the input current, we get the alternative picture shown in the lower chart.
I have shown the current here with
a duty cycle of 0.5, which gives the
highest AC RMS current. If the duty
cycle moves away from 0.5 in either
direction, the RMS current decreases,
Fig.1: the AC time-domain
analysis equivalent circuit of
this buck converter replaces
everything to the right of the
input filter capacitor with an AC
current source.
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reaching zero at the extremes when D
= 0 or D = 1.
This is a common approximation
because we usually want to design
EMI filters for the worst-case situation. It is also easiest to calculate the
harmonics of the AC waveform if it is
a true square wave.
The lower circuit in Fig.1 shows the
AC analysis model of the buck converter. Everything to the right of the
input filter capacitor is replaced with
an AC current source ix(ac), and the DC
voltage source is eliminated altogether.
In this case, the current source will be
a variable duty cycle rectangular wave
with a peak-to-peak amplitude of Il.
We will use this model to design
a suitable input filter in a moment.
First, we should think about how we
are going to measure the conducted
EMI in this circuit.
The voltage that our spectrum
analyser would see, vs(ac), is obviously highly dependent on the source
impedance, Zs. We can assume this is
quite low at DC, but who knows what
it will look like over the 150kHz to
30MHz band of interest.
Fig.2: to measure conducted EMI
consistently, we need to use a line
impedance stabilisation network (LISN)
like this. The component values are
provided in the relevant EMI standard.
The LISN
To make meaningful and repeatable EMI measurements, we have to
specify a standard source impedance
at the frequency of interest. For this
reason we use a line impedance stabilisation network (LISN) when making
conducted EMI measurements. LISNs
are used with both DC and AC sources.
Fig.2 shows the AC model connected to a voltage source with impedance Zs via a LISN inside the dotted
box. I have reinstated the source voltage to indicate that the converter is
powered through the LISN, which has
a low impedance at DC or mains frequency but presents a load of 50W to
the converter input at the frequencies
of interest.
The LISN’s inductor and capacitor
values are chosen so that Cs is effectively a short circuit and Llisn is effectively open-circuit at the measurement frequencies. The impedance at
the converter’s input is therefore the
50W input impedance of the spectrum
analyser. Clisn blocks any DC or mains-
frequency AC from reaching the analyser, since the converter has to be powered up to make the measurements.
The LISN’s component values are
specified in the relevant EMI standard,
but typical values might be Cs = 1µF,
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Fig.3: we have to be concerned with both differential-mode
and common-mode EMI currents – each of which poses
unique filtering challenges.
Llisn = 50µH and Clisn = 100nF. Most
LISNs use air-cored inductors to keep
stray capacitances low, and there may
be a resistor in series with Cs to damp
resonances (more on this below).
There will probably also be a highvalue resistor (≥1kW) between the measurement terminal and common so
that the measurement terminal does
not float when no spectrum analyser
is connected.
Commercial LISNs may also include
additional filter stage(s) on the source
side to limit the influence that EMI
entering from the source has on the
measurement.
The LISN network shown in Fig.2
is repeated on the positive and negative lines in a DC LISN, and on each
phase and the Neutral conductor of
an AC LISN so that common-mode
and differential-mode measurements
can be made.
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Common mode versus
differential mode
So far we have been analysing converters and their input filters using a
huge assumption: we have assumed
that all current flowing into one input
terminal flows out of the other one as
per the upper diagram in Fig.3. This
has been a reasonable thing to do for
everything we have done so far, but it
does not stand up when we are looking at higher frequencies.
The lower diagram represents an
alternative high-frequency current
path where there is some parasitic
capacitance to Earth, for example
between the drain tab of a TO-220
Mosfet and an Earthed heatsink. This
current enters via the positive input
terminal but returns to the source via
Earth – there is no corresponding current coming out of the negative input
terminal.
March 2026 41
Fig.4: an LC differential-mode filter like this one may require damping to eliminate oscillations caused by gain
peaking at the LC resonant frequency.
This is just one possible alternative
path for current to flow; there will be
many in a real converter, including
some related to the negative terminal.
In reality, both types of current flow
will be happening at the same time, so
the currents labelled i1 and i2 will be
the sum of the two. The current that
flows into one terminal and out the
other is termed the differential-mode
current (idm), and the current that only
flows into one terminal is the common-
mode current, icm.
The differential-mode current includes the normal operating current
of the converter, including all of its
harmonics, while the common-mode
current is related to leakage paths.
Mathematically, idm is defined to
be ½(i1 – i2) and icm is i1 + i2. Note that
both i1 and i2 flow into the converter
in this model. These definitions give
a clue to the names; differential-mode
current is related to the difference in
currents flowing into the converter,
while common-mode currents are
related to the total current flowing into
both terminals.
It is perhaps more intuitive to look
at these equations from the other direction – in terms of the currents into
the positive terminal and that coming
out of the negative one, ie, i1 and -i2,
respectively.
In this case, i1 = idm + ½icm and -i2 =
idm – ½icm. In other words, differential-
mode current flows into one terminal
and out the other, while common-
mode current flows equally into both
terminals and out somewhere else.
Differential-mode input filter
EMI standards put limits on both
differential-mode and common-mode
interference, so both have to be filtered. These two filtering problems are
different in nature and have different
challenges and solutions. We’ll start
with the differential-mode filter.
To do this, we will go back to the
AC analysis model we created in Fig.1.
The input filter was a simple capacitor,
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and we saw that its effectiveness was
dependent on the source impedance.
For EMI measurements, we can use a
LISN to standardise the source impedance, but for everyday operation, we
are stuck with an unknown impedance.
We can reduce this dependence by
employing an LC filter like that shown
in the AC equivalent circuit of Fig.4.
I have drawn this filter as it appears
in the converter, with its input on the
right and its output on the left. You
might be wondering why, if this is
the case, the inductor is on the output
side of the filter and not on the input
side, as is usual for LC filters. This is
a current-sourced filter, so the source
has a much higher impedance than
the load (Zs).
In a typical voltage-sourced filter,
the source has a lower impedance
than the load. In both cases, the filter
works most effectively if the inductor
is on the low-impedance side, since its
impedance increases with frequency.
The graphs to the right of the schematic show the current transfer function of the filter (ratio of output current
is to input current ix), which looks like
that of any typical LC low-pass filter.
The cutoff frequency is 1 ÷ (2π√Lf Cf),
and the roll-off is -40dB per decade.
To the right of that is the filter’s impedance characteristic.
At frequencies well below fc, the
impedance is dominated by the inductance; at frequencies above fc, it is dominated by the capacitance.
With ideal components, as we
approach the cutoff frequency, the
magnitude of the transfer function
and impedance are theoretically
infinite. With real components, there
will always be some degree of natural
damping, but LC filters often exhibit
significant peaking at the resonant
frequency, as shown dotted in the
diagrams.
LC filters tend to oscillate because
of this peaking, especially if excited
by a harmonic-rich square wave. This
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problem is compounded in power
electronics because switching converters often have a negative input
resistance. This negative resistance
provides ‘negative damping’ and
increases the likelihood of oscillation.
To understand how a switching
converter can exhibit negative input
resistance, consider a DC-DC converter with a fixed output voltage and
load. Under these circumstances, some
amount of power is being delivered to
the load and consequently drawn from
the input source.
If the input voltage were to rise a little bit, the control loop would adjust
the duty cycle to keep the output
voltage constant. The output power
remains constant, so therefore does
the input power, causing the input
current to drop slightly.
Ohm’s Law dictates that the input
resistance is the change in voltage
(positive in our example) divided by
the change in current (negative), so
the incremental input resistance must
be negative.
Damping
For these reasons, it is quite common to require some form of damping
on the input LC filter of a switching
converter. Fig.5 shows one common
way to do this. The damping capacitor Cd is larger than the filter capacitor, so it appears close to a short circuit at the undamped filter’s resonant
frequency. This puts Rd effectively in
parallel with Cf, providing the necessary damping. This series resistor/
capacitor combination is often referred
to as a ‘snubber’.
Selecting the damping resistor value
is an optimisation problem. If it is too
small, the damping capacitor appears
in parallel with Cf, shifting the cutoff
frequency but not contributing much
damping. If it is too large, it also does
not provide much damping. The optimum resistor value depends on the
ratio of Cd to Cf, which is usually
denoted by the Greek letter xi (ξ).
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Their derivation is a bit complicated, but you can use the expressions
to the right of Fig.5 to calculate the
optimum value of the damping resistor and the resulting maximum impedance of the filter. The latter is important because we need to keep it low to
reduce the impact of the converter’s
negative input impedance.
A realistic example
It is probably easier to follow if we
work through a simple example. Let’s
assume we have a 60W buck converter
with a 12V input and 6V/10A output
operating at a frequency of 500kHz.
The worst-case duty cycle is 0.5, so the
AC input current will be a square wave
with a peak-to-peak amplitude of 10A.
Let us suppose that we want to
design an input filter that reduces this
current ripple by a factor of 100, to no
more than 100mA peak-to-peak.
We first have to work out the cutoff frequency of an undamped LC
filter that will give us the required
attenuation. We do this by initially
assuming that most of the energy in
the square wave occurs at the fundamental frequency. We know a square
wave only has odd harmonics, and that
their amplitude is given by In(pk-pk) =
2I(pk-pk) ÷ nπ, where n is the harmonic
number.
The peak-to-peak amplitude of the
fundamental component of current
will therefore be 6.37A. Just as a check,
the next harmonic (the third) would
have an amplitude 1/3 of that, or 2.12A,
and each subsequent harmonic will
have a proportionally lower amplitude.
The desired attenuation factor of
100 means we require the peak-topeak amplitude of the fundamental
component of the filter’s output to be
63.7mA or lower. We will use a lower
value, say 25mA, to account for the
fact that we have only considered the
fundamental component.
We can now calculate the required
cut-off frequency to achieve this level
of attenuation from the relationship is
÷ ix = fc2 ÷ fsw2. Rearranging and substituting in the switching frequency
and currents gives us a filter cut-off
frequency of 31.3kHz. We can use this
to choose the filter components using
the equation fc = 1 ÷ 2π√Lf Cf.
However, we can’t just chose any
values for L and C, because we also
want to make sure that the filter’s
impedance Zf = √Lf ÷ Cf is significantly
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smaller in magnitude that the converter’s (negative) input impedance to
minimise the probability of unwanted
behaviour.
The converter’s input impedance
is easily calculated by Ohm’s law to
be -2.4W (-12V ÷ 5A). If we therefore
choose Zf to be 0.2W and use both equations, we end up with a value for Lf of
1.01µH and for Cf of 25.4µF. We can
safely round these to 1µH and 25µF,
respectively.
Just out of interest, I simulated the
circuit with these values and without
any damping. I used a simple square
wave current source (no negative
impedance) and set the source impedance to zero, as per Fig.6(a). The result
is shown in Fig.6(b).
The switching frequency is certainly
attenuated significantly (you can’t
really see it), but the filter oscillates
with a peak-to-peak amplitude of 12A
at the resonant frequency. Clearly, we
do need to add the damping capacitor
and resistor.
Given the filter capacitance Cf is
25µF, would be convenient to set ξ to
4, making Cd a nice round 100µF. The
formulae in Fig.5 give us an optimum
value for Rd of 0.14W and a maximum
filter impedance of 0.17W.
This is not a huge amount of damping resistance, so it is possible that
some or all of it can come from the
damping capacitor’s ESR if you were
to use an electrolytic here – for once,
the ESR of a capacitor comes in handy!
I simulated the damped filter, with
the results as shown in Fig.7. Note
the difference in scales between the
damped and undamped responses.
You can see that the switching frequency ripple has been reduced to
about 50mA peak-to-peak, inline with
our design criteria, but there is some
Fig.5: the addition of a
damping resistor and
capacitor, as shown here,
is often necessary to
minimise the oscillation
in an LC filter. The
optimum values can be
determined from the
equations on the right.
Fig.6: the simulation
circuit (left) to check
the oscillation of an LC
filter. Without damping
(Cd and Rd omitted),
the filter oscillates at
its resonant frequency
and with an amplitude
of 12A peak-to-peak
(below).
Australia's electronics magazine
March 2026 43
residual ripple (200mA peak-to-peak)
at the filter’s resonant frequency.
Fortunately, this is well below the
bottom end of the EMI frequency
range, so it might be something we
could live with.
Common-mode input filters
A differential mode filter like this
will have no effect on common-mode
signals because there is a low impedance path for common-mode signals
through it via the ‘ground’ line. A
common-mode filter therefore has to
be effective on both conductors. This is
often achieved with the use of coupled
inductors, as shown in Fig.8. These
are also often called common-mode
inductors or common-mode chokes.
The windings are arranged such that
the flux produced by differential-mode
current cancels out, as shown at the
left of the figure, while that due to
common-mode currents adds up.
With perfect coupling, the differential-mode current, which includes
the relatively high operating current,
does not produce any flux in the core.
No flux means no differential-mode
inductance and no flux density, so
the core can be much smaller than it
would otherwise have to be.
With perfect coupling, common-
mode inductors present an inductance
to common-mode signals but appear
‘invisible’ to differential-mode signals.
Because the windings on these
inductors are often at high voltages
with respect to each other, they tend
to be wound on opposite sides of a
toroidal core, which means there will
be some leakage inductance, so in
reality there will be some meaningful
level of differential-mode inductance,
although lower than the common-
mode inductance.
You can see the common-mode
inductor with the blue core in Fig.14
towards the top of the picture. The
two windings and the spacing between
them are clearly visible.
Although it only produces a small
amount of flux, the differential-mode
current still flows through the windings, so they must be dimensioned
appropriately. Common-mode chokes
are not restricted to two windings;
three-winding common-mode chokes
are used to build filters for three-phase
systems, for example.
When we designed the differential-
mode filter above, we started with a
clear model of the source current ix
and worked from there. The source of
the common-mode currents is leakage
through circuit parasitics, so developing such a model is not really feasible.
The ‘right’ way to start the design
is to build the circuit without a filter
and measure the raw common-mode
noise across the spectrum of interest.
We could then use the limits in the
appropriate EMI standard to determine the required filter characteristic
and proceed from there.
Most of the time, this is not practical, and there are some practical
limitations on the design of mains
common-mode filters that mean that
many decisions are made for you. You
can usually therefore do a good enough
job by selecting ‘reasonable’ component values and validating through
testing.
Fig.9 shows a typical example of
a single-stage common-mode filter
designed for mains use, with the supply on the left and the converter (the
source of the common-mode noise current) on the right. The common-mode
inductance of L and the two Cy capacitors forms the common-mode filter. The leakage inductance of L and
the capacitor labelled Cx2 form a
differential-mode filter.
Capacitor Cx1 (not always present)
provides some filtering of noise coming into the converter and reduces the
input source impedance at higher frequencies. The resistor is there to discharge the capacitors when the mains
is removed so the mains plug does not
pose a shock hazard.
Class-X & Class-Y capacitors
Fig.7: adding the damping components reduced the ripple to 100mA peak-topeak. The 500kHz switching ripple is attenuated to approximately half of that.
Fig.8: a common-mode inductor has two windings arranged so that the
fluxes produced by differential-mode currents cancel and those due to
common-mode currents add.
44
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It is no accident that I have labelled
the capacitors X and Y. It is mandatory to use safety-certified “Class X”
capacitors across the mains and “Class
Y” capacitors from Active (or Line) to
Earth. Apart from having appropriate
voltage ratings, these capacitors are
designed to fail safely.
Class Y capacitors have the most
stringent requirements; they are
required to fail open-circuit so that the
mains is never shorted to the device
enclosure, endangering the user. Class
X capacitors, on the other hand, are
often designed to fail short-
circuit.
You can use an appropriately rated
Class Y capacitor across the mains,
but you should never ever use a Class
X capacitor between Active/Live (or
Neutral) and Earth.
Safety-rated capacitors come in various sub-classes that denote the peak
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voltage they can tolerate. Lower subclass numbers mean higher voltage
capability. For our 230V mains voltage in Australia, you should use the
X2 and Y2 subclasses as a minimum.
The higher-rated X1 and Y1 subclasses
are also OK, but not strictly necessary.
Never use lower-subclass components or ones without the proper certification. You can easily recognise
safety-rated capacitors because their
cases are usually smothered in logos
from certification bodies.
The Class Y capacitors in a common-
mode filter provide a leakage path from
Active to Earth, so their maximum
value is dictated by the acceptable
leakage current at mains frequency.
Industrial products can usually have
a leakage current of no more than
0.5mA (at 250V AC), limiting Cy to a
maximum value of about 6nF. This is
why you will often see 2.2nF or 4.7nF
ceramic Class Y caps in these filters.
Class X capacitors can be larger;
220nF, 470nF or even 1µF values are
not unusual. Much larger than this,
and you run into problems discharging them fast enough. You can decrease
the value of the discharge resistor only
so far before its power dissipation
becomes a problem.
The higher Class X capacitance
means that these filters can provide
appreciable differential-mode filtering, even though the differential mode
inductance is lower. Typical filters
use common-mode inductors in the
0.33mH to 10mH range. If more attenuation is required, it is common to add
a second or even third stage in series,
rather than using larger inductors.
Power factor correction (PFC)
EMI filtering is concerned with
high-frequency harmonics, but you
will recall from the last article that
with a sinusoidal voltage source,
only the fundamental component of
the source current contributes usable
power (real power), designated ‹p›,
with units of watts.
The higher harmonic components of
current do however contribute to the
RMS value of current and therefore to
the ‘apparent power’, S, defined as the
product of RMS voltage and RMS current and having units of volt-amperes
(VA). The ratio of real power to apparent power, ‹p› ÷ S, is the definition of
power factor.
For unity power factor, the current
must not only have a purely sinusoidal
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Fig.9: a typical common-mode
filter includes safety-rated Y-Class
capacitors from
Active to Earth
and X-Class
between Active
and Neutral. It is
really important
to use the correct
parts in these
critical locations.
Fig.10: a power factor correction circuit ‘spreads out’ the spiky current
waveform produced when the capacitor charges at the peak of the mains.
shape; it also has to be in phase with
the voltage. For example, an inductive load such as a motor will not
have unity power factor even though
the current is sinusoidal, because of
the phase shift between voltage and
current.
In this case, correcting the power
factor can be as simple as adding a
capacitor of appropriate value across
the load to bring the phase shift
between voltage and current back to
zero. This is known as passive power
factor correction.
Things are not this simple with
AC-DC converters, as we saw last time.
The most common arrangement of a
full bridge followed by a capacitive
filter results in a current waveform
with narrow spikes near the voltage
peaks, corresponding to the period in
which the capacitor is charged. This
is illustrated in Fig.10.
Active power factor correction aims
to spread these peaks and make the
overall source current waveform more
sinusoidal in shape. Pushing current
into the filter capacitor while the input
voltage (shown dotted in red) is lower
than the DC voltage implies that the
PFC circuit must be capable of producing an output voltage higher than
its input. The obvious candidate is a
boost converter.
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Fig.11 shows the typical circuit of
an active power factor corrector. A
boost converter is interposed between
the rectified mains input and the load
(often another DC-DC converter). The
boost converter is driven by a current-
mode modulator, as shown in the diagram at the bottom of Fig.11. Crucially,
its input reference current is forced
into a ‘rectified sine’ shape.
Thus, the boost converter produces a
steady DC voltage across C1, but draws
a roughly rectified-sinewave-shaped
current through L1, and thus a nearsinewave-shaped current from the
source.
The current-mode modulator monitors the inductor current and controls
the Mosfet’s on-time to make the current track the reference current, which
is the output of the error amplifier/
compensator multiplied by the rectified sine signal. This latter is derived
from the mains so that the input current is in phase with the voltage, resulting in a very good power factor.
The load voltage must be higher
than the peak of the mains, so it is normally set to about 400V. This allows
for a wide range of AC input voltages
– say, from 90V AC to 280V AC.
You don’t have to use a boost converter, although this is by far the most
popular topology due to its simplicity.
March 2026 45
Fig.11: the PFC converter uses a
current-mode boost converter to
generate the output voltage. The
reference current is modulated
to shape the inductor
current into a ‘rectified
sinewave’ shape so
the input current is
sinusoidal.
Fig.12: there are several alternative PFC topologies like these, but
they all work on the same basic principle as that shown in Fig.11.
You obviously can’t use a buck converter because it does not work when
its input voltage is lower than its output, a state that will occur near every
zero-crossing.
PFC variants
There are of course many variations
on this theme, several of which I have
shown in Fig.12. On the left is the
interleaved power factor correction
circuit. You can see that this is really
two parallel boost converters, which
are normally driven 180° out of phase
with each other, feeding a common filter capacitor.
This has the advantage of higher
output power and effectively doubles
the switching frequency as seen at the
input, simplifying the input filtering.
The next variant is described a
“bridgeless” PFC converter, but this is
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a bit of a misnomer since the upper two
diodes plus Mosfets and their body
diodes clearly form a bridge rectifier.
The functions of the rectifier and boost
converter are integrated, providing
better efficiency since several diode
drops are eliminated.
It can also be thought of as two boost
converters in parallel, although this
time each one is operating on alternate half-cycles. In theory, you can get
away with a single inductor in one leg,
but at the cost of increased common-
mode EMI.
An even more efficient variant is the
so-called “totem-pole” architecture.
Here, one Mosfet acts as a synchronous rectifier each half-cycle while the
other is switching. This is more efficient than the bridgeless PFC because
a Mosfet can have a much lower voltage drop than a diode.
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An even more efficient version uses
four Mosfets, eliminating diodes altogether. There is a penalty to pay in
terms of complexity with totem-pole
PFC converters because they require
a high-side driver.
A practical PFC converter
It is a bit beyond the scope of this
article to run through the complete
design of a PFC converter, but we can
do the next best thing and take a look
at a real example from an evaluation
board; in this case, an EVL-4986-350W
from ST Microelectronics (Fig.14).
This is a 350W boost-converter type
PFC based on the L4986 IC, a very
typical example of the type of chip
that is readily available these days.
The circuit, redrawn from the EVL4986-350W data brief, is reproduced
in Fig.13.
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Fig.13: this circuit of the EVL4986-350W PFC evaluation board
redrawn from its data brief. See the
text for a full description.
The mains input on the left is fused
by F1 and protected by metal-oxide
varistor (MOV) RV1. It is then fed
through a common-mode filter consisting of two X2 capacitors and common-
mode choke L3. This filter is missing
its Class Y capacitors because this circuit has no mains Earth connection.
There will be some common-mode
rejection due to the voltage divider
formed common-mode impedance of
L3 and the common-mode load impedance (50W during EMI measurement).
Diodes D8 and D9 connect the AC
input to the HV pin on the controller. This pin is capable of withstanding up to 800V AC and serves several
purposes.
Firstly, it is involved in the startup
of the controller. If a voltage exceeding
about 29V is sensed on this pin, the
capacitors on the Vcc pin are charged
from it via an internal current limiter
until it reaches a voltage sufficient for
the control chip to start.
Once the PFC converter is up and
running, the Vcc pin is supplied by the
auxiliary winding on the boost inductor L1, via a 100W series resistor, 100nF
AC-coupling capacitor and diode D7.
Zener diode D6 limits the Vcc voltage
to a maximum of about 18V.
The HV pin is also used to sense
the AC voltage for the undervoltage/
brownout protection circuit and to
provide the modulation required to
shape the input current. The HV pin
can also detect when the mains is
removed and switch in a current sink
to discharge the X-capacitors, obviating the need for a discharge resistor
and its associated power dissipation.
That’s a lot of functions for one pin!
The AC input is rectified by a 15A
600V bridge rectifier (D3) mounted on
one of the two heatsinks. The rectifier is followed by a differential-mode
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filter comprising L2 and a 1μF capacitor, which reduces the fundamental
of the 65kHz switching noise at the
input by a factor of around eight and
the higher harmonics by a proportionally greater factor.
The boost converter consists of the
inductor L1, Mosfet Q1 and diode
D1, with one 470nF and two 100μF
capacitors forming its output filter.
Diode D2 precharges these capacitors
when the mains is first applied so that
the boost converter can start up much
faster than it would if it had to charge
them from zero.
The 1W cold resistance of the NTC
thermistor limits the capacitor inrush
current, but as current flows through
it in operation, the resistance drops
by a couple of orders of magnitude
and it can be more-or-less ignored.
The Mosfet current is sensed
across the three parallel 0.22W
shunt resistors below L2. The
resulting (negative) shunt
voltage is fed via a 51W resistor to the
controller IC, where it is compared to
the current reference to determine the
Mosfet switch-off instant. If the CS pin
voltage falls below -0.49V, an internal
overcurrent comparator overrides the
modulator, limiting the peak current
to about 6.7A.
The Mosfet gate is driven via 3.9W
and 6.8W resistors, plus diode D4. This
network allows for separate control of
the Mosfet’s switch-on and switch-off
times. Q1’s gate is charged (to switch it
on) via just the 6.8W resistor but is discharged via both resistors
in parallel, compensating for the
Fig.14: the PFC evaluation
board described in the text.
The input connector is hidden
behind the large boost inductor,
and the output connector is at the front right.
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47
Type II compensator, which has
two poles and one zero. For
more details, see the second
article in this series, published
in the December 2025 issue
(siliconchip.au/Article/19370).
The compensator poles and
zeroes are positioned to provide
dominant-pole compensation to
the overall open-loop gain.
The red line in Fig.15 shows the
frequency response of the PFC’s
Fig.15: the compensator for the PFC
modulator and output filter. This
converter is similar to that for a
has a single pole at fco, determined
conventional DC-DC converter. The
by the converter’s output capaccrossover frequency must be lower than
itance and its load resistance,
100Hz or the control loop will try to
and a zero formed by the output
eliminate the modulation we need to
capacitance and its ESR. The outshape the input current.
put capacitance is 200µF and the
fact that the STF36N60M6 has a much
minimum load resistance is 457W
slower inherent switch-off time (50ns) (400V2 ÷ 350W), so the pole occurs at
than its switch-on time (15ns).
about 1.74Hz.
Output voltage feedback is proWe don’t need to worry about the
vided to the FB pin on the controller frequency of the zero formed by the
IC (U1) by the divider formed by the output capacitance and its ESR for reathree 2.2MW resistors, together with sons that will become apparent soon.
the series/parallel combination of four
The cyan/blue line shows the
different-
value resistors to ground desired open-loop gain required for
(16kW, 100kW, 30kW & 360kW).
stability, rolling off at a steady -20dB
This feedback voltage is internally per decade from the origin (effectively
compared to a 2.5V reference to cre- DC), then taking a turn down to -40dB
ate the error signal. Like the current per decade at frequency fp.
sense input, an independent comparIn a normal converter, we would
ator shuts the boost converter off if the position this pole to cancel the filfeedback voltage exceeds the reference ter’s ESR zero to maximise the bandby more than about 7%.
width of the control loop. However,
If the voltage at the feedback pin for PFC converters, we have to limit
falls below about 0.5V, the controller the loop bandwidth so the crossover
enters ‘external burst mode’, in which frequency (the frequency where loop
switching is inhibited. This prevents gain falls to 0dB) is below twice the
the output voltage from rising uncon- mains frequency.
trollably in the case that the voltage
We have to do this so the control
sense resistors become open-circuit loop does not respond to the 100Hz
and also allows an external control- ripple on the output and try to counler to switch the converter off via Q4. teract the very modulation we are relyThis feature might be used to reduce
ing on to shape the current.
power when a following converter was
The compensator’s second pole (the
disabled or had a very light load. Dis- first is at the origin) is therefore typiabling and enabling the PFC in this cally placed at some frequency, fp, that
way is fast because the control chip forces the crossover frequency to be
does not go through the whole start-up
Fig.16; the upper
procedure each time.
trace
shows the PFC
The voltage feedback divider douconverter’s input current
bles as an input for the controller’s
at near full load. The
power-good comparator. If the voltage
current is similar in
at the PGIN terminal exceeds 2.375V,
shape to the input
the open collector ‘power good’ (PG)
voltage shown below.
pin is asserted low.
The measured power
Compensation
less than 100Hz. The filter zero caused
by the output capacitance and its ESR
is therefore more-or-less irrelevant
since the control loop is not effective
at this frequency.
The evaluation board’s compensator
has its zero set by the 62kW resistor and
1.5µF capacitor near to 1.71Hz – pretty
much bang on the output capacitance/
load resistance pole. The upper pole
is set to 17.1Hz by the 62kW resistor
and 150nF capacitor, well below the
100Hz ripple frequency.
I have not mentioned transistor Q3
and its associated base drive components yet. The controller chip has a
threshold detector on the COMP pin
that shuts down the PFC converter if
the voltage is below about 0.5V. This
can be used to stop and start the converter, but unlike Burst Mode control,
the converter goes through a full softstart cycle when enabled.
Testing
I tested the PFC evaluation board on
my bench with a 500W load. The current and voltage waveforms are shown
in Fig.16. The current (green trace) is
certainly close to a sinusoid, but has
some visible vestiges of switching ripple. Its shape tracks the input voltage
(yellow trace) almost exactly, including its slightly flat top caused by all
those non-PFC converters on my line.
The RMS current and voltage measurements on the right must each be
scaled by a factor of 10 for 243V and
1.33A respectively, giving an apparent
power of 323W. The average DC voltage and current in the load measured
396.7V and 0.785A, respectively, for
a real power of 311.4W. The resulting
power factor is 0.96, which is about as
good as we could expect.
We have now covered DC-DC converters and AC-DC converters in a fair
bit of depth. Next time, we will dive
into the interesting world of DC-AC
SC
converters.
factor was 0.96.
The internal error amplifier’s compensation is set by the network hanging off its pin 8. This forms a classic
48
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