Solved Problems · Set 21

Ćuk, SEPIC and Fourth-Order Converters

Part 3 · DC–DC Converters — add a fourth reactive element and both terminal currents become continuous. Six problems on the converters that transfer energy through a capacitor.

Prof. Mithun Mondal 6 solved problems GATE · ESE · University

Set 21 — Ćuk, SEPIC and Fourth-Order Converters

Set 20 ended with a limitation none of the three basic converters escapes: a buck pulses its input, a boost pulses its output, and a buck–boost pulses both. Every pulsed terminal needs a filter that the converter does not provide, and in an automotive or telecom environment that filter is often larger than the converter it protects.

Adding a fourth reactive element fixes it. Put a capacitor between two inductors and the capacitor becomes the energy-transfer element while both inductors keep their terminal currents continuous. That is the Ćuk converter, and it is the only one of the four here with smooth current at both ends. Its cousins — SEPIC and Zeta — give up one of those for a non-inverted output. All four pay in a fourth-order resonance that must be damped.

Part 3 · Chapter 13 · 6 solved problems

i Method Recap
  • All three fourth-order converters share the buck–boost's ratio:

    \[ \frac{\left|V_o\right|}{V_{in}} = \frac{D}{1-D}, \qquad D = \frac{\left|V_o\right|}{V_{in}+\left|V_o\right|} \]
  • The transfer capacitor voltage identifies the topology:

    \[ \text{Ćuk: } V_{C1} = V_{in}+\left|V_o\right|; \qquad \text{SEPIC and Zeta: } V_{C1} = V_{in} \]
  • Each inductor is sized from the voltage it sees during the on-time, which is \(V_{in}\) for both:

    \[ L_1 = \frac{V_{in}D}{\Delta I_1f_s}, \qquad L_2 = \frac{V_{in}D}{\Delta I_2f_s} \]
  • The transfer capacitor carries the full throughput as AC:

    \[ \Delta V_{C1} = \frac{I_oD}{f_sC_1}, \qquad I_{C1,rms} = \sqrt{DI_o^2+(1-D)I_{in}^2} = \sqrt{I_{in}I_o} \]
  • Coupling the two inductors steers the ripple. With both windings seeing the same voltage:

    \[ \frac{di_1}{dt} = \frac{v\left(L_2-M\right)}{L_1L_2-M^2} \;\Longrightarrow\; \Delta I_1 = 0 \text{ when } M = L_2 \]
  • The input loop resonates and needs damping:

    \[ f_{res} = \frac{1}{2\pi\sqrt{L_1C_1}}, \qquad Z_0 = \sqrt{\frac{L_1}{C_1}}, \qquad Q = \frac{Z_0}{r} \]
Problem 1CoreThe Ćuk Converter

A Ćuk converter produces \(-15\) V at 2 A from 12 V at \(f_s = 200\) kHz — the same specification as the buck–boost of Set 20. Size both inductors for 20% ripple, the transfer capacitor for 5% ripple and the output capacitor for 50 mV, then compare every component with the buck–boost.

L1 C1 L2 SW D C2 Vin Vo both terminal currents are inductor currents — smooth at each end
The capacitor carries the energy; the inductors keep both ends continuous
Solution

The duty ratio is unchanged from the buck–boost, because the volt-second balance on \(L_1\) is the same:

\[ D = \frac{15}{12+15} = 0.556, \qquad I_{in} = I_o\frac{D}{1-D} = 2.5\ \text{A} \]

Now, crucially, \(L_1\) carries 2.5 A and \(L_2\) carries 2 A — the terminal currents themselves. Neither inductor carries the 4.5 A the buck–boost's single inductor had to.

The input inductor. With the switch on, the full input voltage appears across it:

\[ \Delta I_1 = 0.20(2.5) = 0.5\ \text{A} \;\Longrightarrow\; L_1 = \frac{(12)(0.556)}{(0.5)\left(200\times10^{3}\right)} = 66.7\ \mu\text{H} \]

The output inductor sees the same voltage, which is not obvious. With the switch on, \(L_2\) sees \(V_{C1}-\left|V_o\right|\):

\[ V_{C1} = V_{in}+\left|V_o\right| = 27\ \text{V} \;\Longrightarrow\; v_{L2,on} = 27-15 = 12\ \text{V} = V_{in} \]
\[ \Delta I_2 = 0.20(2) = 0.4\ \text{A} \;\Longrightarrow\; L_2 = \frac{(12)(0.556)}{(0.4)\left(200\times10^{3}\right)} = 83.3\ \mu\text{H} \]
\[ \text{check off-interval: } (12)(0.556) = 6.67 = (15)(0.444)\ \checkmark \]

Both inductors see \(V_{in}\) during the on-time and \(-\left|V_o\right|\) during the off-time. That identical excitation is what makes the coupled-inductor trick of Problem 3 possible.

The transfer capacitor, which is discharged by \(I_{L2}\) during the on-time and recharged by \(I_{L1}\) during the off-time:

\[ \Delta V_{C1} = 0.05(27) = 1.35\ \text{V} \;\Longrightarrow\; C_1 = \frac{I_oD}{f_s\Delta V_{C1}} = \frac{(2)(0.556)}{\left(200\times10^{3}\right)(1.35)} = 4.1\ \mu\text{F} \]
\[ \text{check: } \frac{I_{in}(1-D)}{f_sC_1} = \frac{(2.5)(0.444)}{\left(200\times10^{3}\right)\left(4.1\times10^{-6}\right)} = 1.35\ \text{V}\ \checkmark \]

The two intervals give the same swing, as charge balance requires. Note that \(C_1\) is not a filter — a 5% ripple on it is entirely acceptable, because it is the energy-transfer element and its ripple never reaches the output.

And now the payoff — the output capacitor. Because \(L_2\) feeds the output directly, the capacitor sees only a triangular ripple, as in a buck:

\[ C_2 = \frac{\Delta I_2}{8f_s\Delta V} = \frac{0.4}{(8)\left(200\times10^{3}\right)(0.050)} = 5.0\ \mu\text{F} \]

Five microfarads, against 55.6 for the buck–boost at the same specification — eleven times smaller. And its RMS current is \(\Delta I_2/\sqrt{12} = 0.12\) A rather than the buck–boost's 2.2 A, so ESR is no longer a constraint at all.

The full comparison:

ComponentBuck–boostĆuk
Inductors1 × 24.7 µH at 4.5 A2 × (66.7 + 83.3) µH at 2.5, 2 A
Output capacitor55.6 µF, 2.2 A rms5.0 µF, 0.12 A rms
Transfer capacitor4.1 µF, 2.24 A rms
Switch voltage27 V27 V
Switch RMS current3.35 A3.35 A
Input currentpulsedcontinuous
Output currentpulsedcontinuous
Order2nd4th — needs damping

Identical switch stresses, both terminals now smooth, and the output capacitor eleven times smaller. What has happened is that the difficult capacitor has moved inside the converter, where a 5% ripple is harmless, instead of sitting on the output where it is not.

The Ćuk converter does not remove the pulsed current — it relocates it. The transfer capacitor still carries 2.24 A of AC, exactly as the buck–boost's output capacitor did. But it carries it where a volt of ripple does not matter, leaving both terminals fed by inductors. That relocation is the whole idea, and Problem 5 shows what it costs.
Answera\(L_1 = 66.7,\ L_2 = 83.3\ \mu\text{H}\)   b\(C_1 = 4.1\ \mu\text{F}\) at 27 V   c\(C_2 = 5.0\ \mu\text{F}\) — eleven times smaller   d both terminals continuous
Problem 2CoreSEPIC, and What It Gives Up

The same specification is met by a SEPIC producing \(+15\) V at 2 A from 12 V. Find the transfer capacitor voltage, the device stresses and the output capacitance required, and explain what the non-inverted output costs.

Solution

The duty ratio and inductor currents are unchanged:

\[ D = 0.556, \qquad I_{L1} = I_{in} = 2.5\ \text{A}, \qquad I_{L2} = I_o = 2\ \text{A} \]

But the transfer capacitor sits at a different voltage. In a SEPIC the capacitor is in series between the two inductors on the input side of the diode, and volt-second balance on \(L_2\) gives:

\[ V_{C1} = V_{in} = 12\ \text{V} \]

Against 27 V for the Ćuk. A lower-voltage capacitor is cheaper and smaller, which is a genuine if minor advantage — and it means the SEPIC's capacitor voltage rating is set by the input alone, so a wide-input design does not need a 27 V part.

Device stresses are the same as the Ćuk's:

\[ V_S = V_D = V_{in}+V_o = 27\ \text{V} \]

Both converters place the sum across the devices, because both must block the input and the output simultaneously. There is no escaping that in any topology derived from the buck–boost.

Now the difference that matters. In a SEPIC the diode feeds the output capacitor directly — there is no inductor between them — so the output current is pulsed, exactly as in a boost:

\[ C_2 = \frac{I_oD}{f_s\Delta V} = \frac{(2)(0.556)}{\left(200\times10^{3}\right)(0.050)} = 111\ \mu\text{F} \]

Against 5 µF for the Ćuk — twenty-two times larger, and with a substantial ESR requirement on top. That single row is the price of the non-inverted output.

The four options compared:

TopologyPolarityInput currentOutput current\(V_{C1}\)
Buck–boostinvertingpulsedpulsed
Ćukinvertingsmoothsmooth\(V_{in}+V_o\)
SEPICnon-invertingsmoothpulsed\(V_{in}\)
Zetanon-invertingpulsedsmooth\(V_{in}\)

SEPIC and Zeta are mirror images: each keeps one terminal smooth and pulses the other, and each gives a positive output. Only the Ćuk keeps both, and only the Ćuk inverts. That trade appears to be structural — no known fourth-order arrangement gives a non-inverted output with both terminals continuous.

Choosing between SEPIC and Zeta. The rule follows from which terminal matters more:

If the priority isChooseBecause
Low conducted EMI on the supplySEPICcontinuous input current
Low output rippleZetacontinuous output current
Driving LEDseither — SEPIC usualLED current is what is regulated
Battery input, sensitive loadĆuk if inversion is acceptableboth smooth

SEPIC dominates in practice, and the reason is regulatory rather than technical: conducted emissions limits are enforced at the supply terminals, so a continuous input current saves an input filter that would otherwise be mandatory. The output ripple is the designer's own problem and can be fixed with a capacitor.

SEPIC buys a positive output by pulsing it. Twenty-two times the output capacitance is the bill, and it is worth paying whenever a negative rail would need level shifting — which is most of the time. The Ćuk's dual-smooth behaviour is the better converter and the worse product.
Answera\(V_{C1} = 12\ \text{V}\)   b devices at 27 V, as the Ćuk   c\(C_2 = 111\ \mu\text{F}\) — 22× the Ćuk's   d the cost of a non-inverted output
Problem 3Exam levelSteering the Ripple Away

The two inductors of a Ćuk converter, \(L_1 = 100\ \mu\text{H}\) and \(L_2 = 80\ \mu\text{H}\), are wound on a single core. Derive the condition for zero ripple in one winding, find the coupling coefficient required to null the input ripple, and explain why the output ripple cannot be nulled with these values.

Solution

The starting observation from Problem 1: both inductors see identical voltage waveforms — \(+V_{in}\) during the on-time and \(-\left|V_o\right|\) during the off-time. So if they are wound on the same core with the same turns orientation, they can be coupled:

\[ v = L_1\frac{di_1}{dt}+M\frac{di_2}{dt}, \qquad v = L_2\frac{di_2}{dt}+M\frac{di_1}{dt} \]

Solve the pair simultaneously:

\[ \frac{di_1}{dt} = \frac{v\left(L_2-M\right)}{L_1L_2-M^2}, \qquad \frac{di_2}{dt} = \frac{v\left(L_1-M\right)}{L_1L_2-M^2} \]

Two independent nulls are available. Setting \(M = L_2\) makes the input ripple vanish; setting \(M = L_1\) makes the output ripple vanish. Both cannot be satisfied unless \(L_1 = L_2\).

Convert to a coupling coefficient:

\[ k = \frac{M}{\sqrt{L_1L_2}}: \qquad \Delta I_1 = 0 \Rightarrow k = \frac{L_2}{\sqrt{L_1L_2}} = \sqrt{\frac{L_2}{L_1}} \]
\[ k = \sqrt{\frac{80}{100}} = \sqrt{0.80} = 0.894 \]

A perfectly achievable value — 0.894 is loose coupling by transformer standards and is set by deliberately spacing the windings or by the leakage of a gapped core. The design is tuned by adjusting that leakage.

Why the other null is unavailable here:

\[ \Delta I_2 = 0 \Rightarrow k = \sqrt{\frac{L_1}{L_2}} = \sqrt{\frac{100}{80}} = 1.118 \;>\; 1 \]

Impossible — a coupling coefficient cannot exceed unity, since that would mean more mutual flux than either winding produces. So the null is only available in the winding with the smaller inductance. Nulling the output instead simply requires \(L_2 > L_1\), which is a design choice made before the core is wound.

What this achieves and what it costs:

BenefitCost
Input ripple → near zerothe other winding's ripple increases
Conducted EMI collapsesnull is sensitive to \(k\) tolerance
Input filter can be tiny or absentone core replaces two — but a larger one
Fewer components overallcoupling must hold over temperature

The first cost is the important one: the ripple does not disappear, it moves. With \(M = L_2\) the output winding takes all of it, so \(L_2\) and \(C_2\) must be sized for the increase. And because the null depends on a ratio of inductances, a 5% coupling error leaves roughly 5% of the original ripple — still a twentyfold improvement, which is why the technique works in production despite the sensitivity.

Where it is used. The same principle applies beyond the Ćuk:

\[ \text{any two inductors with identical voltage waveforms can be coupled and steered} \]

Which includes the SEPIC (whose inductors also see matched waveforms) and the Zeta. In a SEPIC, coupling the two windings on one core is near-universal practice — it saves a component and halves the ripple in both windings even without deliberate tuning, because the effective inductance of each doubles.

Ripple steering is conservation, not cancellation. The volt-seconds still have to go somewhere; coupling decides which winding absorbs them. Choosing the input gives a converter that is nearly invisible to the supply — which is worth far more than the same improvement at the output, because the output is the designer's to filter and the supply is everyone's.
Answera\(\Delta I_1 = 0\) when \(M = L_2\)   b\(k = 0.894\)   c nulling the output would need \(k = 1.118 > 1\) — impossible
Problem 4Exam levelA Resonance Nobody Asked For

For the Ćuk converter of Problem 1 (\(L_1 = 66.7\ \mu\text{H}\), \(C_1 = 4.1\ \mu\text{F}\)), find the input-loop resonant frequency and its quality factor with a total series resistance of 50 mΩ. Design a damping network and state the consequence for the control loop.

Solution

Where the resonance comes from. The converter now has four reactive elements, so its transfer function is fourth order — two complex pole pairs rather than one. The lower pair comes from \(L_1\) ringing against \(C_1\):

\[ f_{res} = \frac{1}{2\pi\sqrt{L_1C_1}} = \frac{1}{2\pi\sqrt{\left(66.7\times10^{-6}\right)\left(4.1\times10^{-6}\right)}} \]
\[ = \frac{1}{2\pi\left(1.654\times10^{-5}\right)} = 9.61\ \text{kHz} \]

Awkwardly placed — well above the loop's likely crossover but well below the switching frequency, so it lies inside the band where the compensator has to work.

And it is barely damped. The characteristic impedance is:

\[ Z_0 = \sqrt{\frac{L_1}{C_1}} = \sqrt{\frac{66.7}{4.1}} = 4.03\ \Omega \]
\[ Q = \frac{Z_0}{r} = \frac{4.03}{0.050} = 81 \]

A \(Q\) of eighty means a 38 dB peak in the transfer function at 9.6 kHz, with the phase swinging through 180° in a fraction of a decade. No compensator can be designed around that; the resonance must be damped in the power stage.

Why the parasitics do not save it. Unlike the output \(LC\) of a buck, this loop is not loaded by the output resistance:

\[ \text{buck: } Q = R\sqrt{\frac{C}{L}} \quad\text{— damped by the load} \]
\[ \text{Ćuk input loop: } Q = \frac{1}{r}\sqrt{\frac{L_1}{C_1}} \quad\text{— damped only by losses} \]

And every design improvement makes it worse. A lower-DCR inductor, a lower-ESR capacitor, a better switch — all reduce \(r\) and raise \(Q\). This is a resonance that gets sharper as the converter gets better.

The damping network. The standard solution is a series \(R_d\)\(C_d\) branch in parallel with \(C_1\):

\[ R_d \approx Z_0 = 4.0\ \Omega \]
\[ C_d \ge 4C_1 = 16.5\ \mu\text{F} \quad\to\quad \text{choose } 22\ \mu\text{F} \]

\(C_d\) must be several times \(C_1\) so that it looks like a short circuit at the resonant frequency — putting \(R_d\) across the loop where it can dissipate — while blocking DC so that \(R_d\) does not carry the 12 V transfer capacitor voltage continuously. With these values \(Q\) falls to roughly unity.

What the damper costs:

\[ P_{R_d} \approx I_{C1,ac}^2R_d \times \text{(fraction at resonance)} \ll I_{C1,rms}^2R_d \]

Small in practice, because at the switching frequency \(C_1\) itself is a much lower impedance than the damper branch, so most of the 2.24 A of Problem 5 flows in \(C_1\) rather than through \(R_d\). The damper only acts near 9.6 kHz, where there is little energy in normal operation — and a great deal during a transient, which is exactly when it is wanted.

Alternatives, and why the RC damper usually wins:

MethodVerdict
Series \(R_d\) in the loopworks, but dissipates the full DC current — unacceptable
Parallel \(R_dC_d\)standard — frequency-selective, low loss
High-ESR \(C_1\)works by accident; ESR is uncontrolled and ages
Current-mode controlhelps, but does not remove the input-loop pair
Notch in the compensatorfragile — depends on component tolerance

The third row is worth noting because it is how many designs get away without a damper: an electrolytic transfer capacitor has enough ESR to damp the loop by itself. Replacing it with a ceramic — an apparently obvious improvement — removes the damping and makes the converter ring.

The fourth element brings a fourth-order resonance that improves with every component upgrade. A \(Q\) of 81 is not a parasitic effect to be ignored; it is a 38 dB peak sitting between the crossover and the switching frequency. Fourth-order converters need a damping network as a matter of design, not as a fix.
Answera\(f_{res} = 9.61\ \text{kHz}\)   b\(Z_0 = 4.03\ \Omega,\ Q = 81\)   c\(R_d = 4.0\ \Omega,\ C_d \ge 16.5\ \mu\text{F}\)
Problem 5ChallengeThe Capacitor That Does the Work

Find the RMS current in the transfer capacitor of the Problem 1 converter, verify its DC charge balance, and determine what type of capacitor is required. Explain why this component, rather than any semiconductor, is what limits fourth-order converters at high power.

Solution

The capacitor's current in each interval. During the on-time it supplies \(I_{L2}\); during the off-time it is charged by \(I_{L1}\):

\[ i_{C1} = -I_o = -2\ \text{A for }DT_s; \qquad i_{C1} = +I_{in} = +2.5\ \text{A for }(1-D)T_s \]
\[ \text{charge balance: } (0.556)(-2)+(0.444)(2.5) = -1.111+1.111 = 0\ \checkmark \]

Which is the condition that sets the duty ratio in the first place — a useful independent route to \(D\) that does not use volt-second balance at all.

The RMS value:

\[ I_{C1,rms} = \sqrt{DI_o^2+(1-D)I_{in}^2} = \sqrt{(0.556)(4)+(0.444)(6.25)} \]
\[ = \sqrt{2.22+2.78} = \sqrt{5.00} = 2.24\ \text{A} \]

And there is a neat closed form, since \(D = I_{in}/(I_{in}+I_o)\):

\[ I_{C1,rms} = \sqrt{I_{in}I_o} = \sqrt{(2.5)(2)} = 2.24\ \text{A}\ \checkmark \]

The geometric mean of the two terminal currents — an elegant result and a useful one, because it can be evaluated before any component is chosen.

What that demands of the part. Compare the candidates at 4.1 µF, 27 V, 2.24 A RMS at 200 kHz:

TypeESRLoss at 2.24 AVerdict
Aluminium electrolytic~500 mΩ2.5 Wfails — overheats
Polymer electrolytic~30 mΩ0.15 Wmarginal, ages
Film (polypropylene)~10 mΩ0.05 Wideal — but bulky
Ceramic (X7R)~5 mΩ0.03 Wgood — but removes damping

The first row is why Ćuk converters have a reputation for unreliability among people who used an electrolytic there. And the last row is the trap of Problem 4: the best capacitor electrically is the one that leaves the input loop with a \(Q\) of eighty.

Why this scales badly. The capacitor's RMS current is \(\sqrt{I_{in}I_o}\), so it rises linearly with power at fixed voltages:

\[ P = 30\ \text{W} \Rightarrow 2.24\ \text{A}; \qquad P = 300\ \text{W} \Rightarrow 22.4\ \text{A}; \qquad P = 3\ \text{kW} \Rightarrow 224\ \text{A} \]

Two hundred amps of ripple current at 200 kHz through a capacitor is not a component that exists in any convenient form. Semiconductors scale far better — paralleling MOSFETs is routine — so the capacitor becomes the binding constraint long before the switches do.

Which sets the practical ceiling:

PowerFourth-order converter
< 50 Wroutine — ceramics handle it easily
50–300 Wpractical with film or stacked ceramics
300 W – 1 kWdifficult — capacitor bank dominates the design
> 1 kWuse an isolated topology instead

Above a kilowatt the answer is a transformer — which provides the same input-to-output isolation of the current path that \(C_1\) was providing, and does it with magnetic coupling instead of a component carrying the full throughput as AC.

In a fourth-order converter the capacitor is the power component. It carries \(\sqrt{I_{in}I_o}\) of RMS current continuously — the whole throughput of the converter, as AC, at the switching frequency. Semiconductors parallel easily and capacitors do not, which is why these topologies are excellent below a few hundred watts and absent above a kilowatt.
Answera\(I_{C1,rms} = 2.24\ \text{A} = \sqrt{I_{in}I_o}\)   b charge balance verified   c film or ceramic only   d the capacitor caps the topology near 1 kW
Problem 6ChallengeAn Automotive LED Driver

A SEPIC drives a 12 V, 1 A LED string from an automotive supply of 9 to 16 V at \(f_s = 300\) kHz. Size both inductors for 30% ripple, the transfer and output capacitors, and every device, working at the worst case for each. Explain why a SEPIC rather than a buck or a boost.

Solution

Why nothing simpler will do. The output sits inside the input range:

\[ 9\ \text{V} \;<\; V_o = 12\ \text{V} \;<\; 16\ \text{V} \]

A buck cannot reach 12 V from 9; a boost cannot reach it from 16. And an automotive supply is worse than these numbers suggest — cold-crank dips to 6 V and load-dump transients to 40 V are routine. The converter must cross the output voltage, which leaves a SEPIC, a Zeta, a Ćuk or a four-switch buck–boost.

The duty ratio range and inductor currents:

\(V_{in}\)\(D\)\(I_{L1} = I_{in}\)\(I_{L2} = I_o\)\(V_S\)
9 V0.5711.33 A1.00 A21 V
12 V0.5001.00 A1.00 A24 V
16 V0.4290.75 A1.00 A28 V

Note that the worst cases fall at opposite ends: the currents are worst at low input, the voltages at high input. Every component has to be checked at the correct extreme, and they are not the same extreme.

The inductors, at 9 V where the currents peak:

\[ \Delta I_1 = 0.30(1.33) = 0.40\ \text{A} \;\Longrightarrow\; L_1 = \frac{(9)(0.571)}{(0.40)\left(300\times10^{3}\right)} = 42.9\ \mu\text{H} \]
\[ \Delta I_2 = 0.30(1.00) = 0.30\ \text{A} \;\Longrightarrow\; L_2 = \frac{(9)(0.571)}{(0.30)\left(300\times10^{3}\right)} = 57.1\ \mu\text{H} \]

Both under 60 µH at low currents, so a single coupled component is practical — and standard for a SEPIC, as Problem 3 noted. A 47 µH coupled pair would suit, with the coupling itself halving both ripples.

The devices, at 16 V where the voltage peaks:

\[ V_S = V_D = 16+12 = 28\ \text{V} \]

But automotive load dump forces a much higher rating:

\[ V_{in,transient} = 40\ \text{V} \Rightarrow V_S = 52\ \text{V} \quad\to\quad \text{100 V devices, or a load-dump clamp upstream} \]
\[ I_{S,rms} = \left(I_{L1}+I_{L2}\right)\sqrt{D} = (2.33)\sqrt{0.571} = 1.76\ \text{A}\ \text{at }9\ \text{V} \]
\[ I_{D,avg} = I_o = 1.00\ \text{A} \]

The two capacitors:

\[ I_{C1,rms} = \sqrt{I_{in}I_o} = \sqrt{(1.33)(1)} = 1.15\ \text{A}, \qquad V_{C1} = V_{in} \le 16\ \text{V} \]
\[ C_2 = \frac{I_oD}{f_s\Delta V} = \frac{(1)(0.571)}{\left(300\times10^{3}\right)(0.120)} = 15.9\ \mu\text{F} \]

A 1% output ripple is generous for LEDs, whose brightness follows current and whose eye response is slow — so the pulsed output that made the SEPIC expensive in Problem 2 costs almost nothing here. That is why LED drivers are the SEPIC's natural home.

Why SEPIC rather than the alternatives:

OptionVerdict here
Buck or boostcannot cross the output voltage
Buck–boostinverting — needs a floating LED string
Zetaworks, but pulsed input — worse automotive EMI
Ćukinverting; also the best EMI — used where polarity allows
Four-switch buck–boostbetter efficiency, but four drivers and mode logic
SEPICnon-inverting, continuous input, one switch

The continuous input current is decisive in a vehicle, where CISPR 25 conducted emissions limits are enforced on the supply leads and an input filter costs more than the converter. At 12 W the efficiency penalty against a four-switch design is a fraction of a watt.

Every component's worst case is at a different end of the input range. The currents peak at 9 V and the voltages at 16 — and the real voltage rating comes from a 40 V transient that never appears in steady-state analysis at all. A wide-input design is not one design at one operating point; it is a set of independent worst cases.
Answera\(L_1 = 42.9,\ L_2 = 57.1\ \mu\text{H}\)   b devices 28 V steady, 100 V for load dump; \(I_{S,rms} = 1.76\ \text{A}\)   c\(I_{C1} = 1.15\ \text{A},\ C_2 = 15.9\ \mu\text{F}\)
Formulas

Key Formulas

QuantityRelationNotes
Conversion ratio\(\left|V_o\right|/V_{in} = D/(1-D)\)All four topologies
Inductor currents\(I_{L1} = I_{in},\ I_{L2} = I_o\)The terminal currents themselves
Ćuk \(V_{C1}\)\(V_{in}+\left|V_o\right|\)
SEPIC / Zeta \(V_{C1}\)\(V_{in}\)Lower-voltage part
Both inductors\(L = \dfrac{V_{in}D}{\Delta I f_s}\)Same excitation — enables coupling
Transfer capacitor\(C_1 = \dfrac{I_oD}{f_s\Delta V_{C1}}\)5% ripple acceptable
Its RMS current\(I_{C1,rms} = \sqrt{I_{in}I_o}\)The binding component
Ćuk output cap\(C_2 = \dfrac{\Delta I_2}{8f_s\Delta V}\)Buck-like — small
SEPIC output cap\(C_2 = \dfrac{I_oD}{f_s\Delta V}\)Boost-like — 22× larger
Device stress\(V_S = V_D = V_{in}+\left|V_o\right|\)Both topologies
Switch RMS\(\left(I_{in}+I_o\right)\sqrt{D}\)Carries both inductors
Coupled slopes\(\dfrac{di_1}{dt} = \dfrac{v(L_2-M)}{L_1L_2-M^2}\)Problem 3
Zero input ripple\(M = L_2,\ k = \sqrt{L_2/L_1}\)Needs \(L_2 < L_1\)
Zero output ripple\(M = L_1,\ k = \sqrt{L_1/L_2}\)Needs \(L_1 < L_2\)
Input resonance\(f_{res} = \dfrac{1}{2\pi\sqrt{L_1C_1}}\)Not damped by the load
Its \(Q\)\(Q = \dfrac{1}{r}\sqrt{L_1/C_1}\)Worsens as components improve
Damper\(R_d \approx Z_0,\ C_d \ge 4C_1\)Problem 4
Pitfalls

Common Mistakes

  1. Assuming both inductors carry the same current. \(L_1\) carries \(I_{in}\) and \(L_2\) carries \(I_o\) — Problem 1.

  2. Using the Ćuk's transfer capacitor voltage for a SEPIC. It is \(V_{in}\) in a SEPIC and \(V_{in}+V_o\) in a Ćuk — Problem 2.

  3. Sizing a SEPIC's output capacitor like a Ćuk's. A SEPIC's output current is pulsed — 111 µF against 5 — Problem 2.

  4. Believing ripple steering makes the ripple disappear. It moves to the other winding, which must be sized for the increase — Problem 3.

  5. Trying to null the ripple in the larger inductor. That needs \(k > 1\) — the null is only available in the smaller one — Problem 3.

  6. Assuming the load damps the input resonance. It does not; only series losses do, giving \(Q = 81\) here — Problem 4.

  7. Replacing an electrolytic transfer capacitor with a ceramic. The apparent upgrade removes the accidental damping and makes the converter ring — Problem 4.

  8. Choosing an electrolytic for \(C_1\) in the first place. 2.24 A through 500 mΩ is 2.5 W in the capacitor — Problem 5.

  9. Scaling a fourth-order converter to high power. \(I_{C1} = \sqrt{I_{in}I_o}\) rises linearly with power and reaches impossible values above a kilowatt — Problem 5.

  10. Checking every component at one operating point. Currents peak at minimum input, voltages at maximum, and the real voltage rating came from a transient — Problem 6.

Looking Ahead

Six problems and the non-isolated toolkit is complete. A fourth reactive element bought continuous current at both terminals, an output capacitor eleven times smaller, and — with coupled windings — an input ripple that can be driven essentially to zero. The bill was a fourth-order resonance with a \(Q\) of eighty that needs a deliberate damper, and a transfer capacitor carrying \(\sqrt{I_{in}I_o}\) of RMS current, which is what stops these topologies at a few hundred watts.

Three limitations remain that no arrangement of inductors and capacitors can fix. There is no galvanic isolation, so a mains-connected supply is impossible. The gain is capped by the parasitic ceiling of Set 19, so 375 V to 12 is out of reach. And multiple outputs each need their own converter. All three are answered by the same component: a transformer, which provides a turns ratio at no efficiency cost, an isolation barrier, and as many secondaries as wanted.

Next: Set 22 — Isolated Converters: Flyback, Forward and Bridge, where a 60 W flyback is designed from an 85–265 V AC input, the forward converter's transformer reset sets a hard duty limit, the full bridge halves the switch stress for kilowatt power, and the leakage inductance that no transformer avoids is turned into a snubber design.