Set 13 — Semiconverters, Freewheeling and Discontinuous Conduction
Set 12 introduced the semiconverter and left it half-analysed, and diagnosed discontinuous conduction without giving a criterion for it. Both loose ends matter more than they look.
The freewheeling interval is what makes the semiconverter's power factor good, and it is also a third conduction state that has to be accounted for in every device current. And the continuous-conduction assumption behind \(V_{dc} = (2V_m/\pi)\cos\alpha\) is not a mild one: a real drive with a back EMF falls out of continuous conduction at light load, where the output rises, the speed rises with it, and the controller's gain changes underneath the loop. Problems 2 and 6 find exactly where that boundary sits.
The semiconverter output never goes negative, because the freewheeling path clamps it at zero:
\[ V_{dc} = \frac{V_m}{\pi}\left(1+\cos\alpha\right), \qquad \text{freewheeling for }\alpha\text{ of each half cycle} \]Three conduction states, three sets of device currents. With a constant load current:
\[ I_{T,avg} = I_{dc}\frac{\pi-\alpha}{2\pi}, \qquad I_{FWD,avg} = I_{dc}\frac{\alpha}{\pi}, \qquad I_{rms} = I_{dc}\sqrt{\frac{\text{conduction}}{2\pi}} \]With a back EMF the current may not survive the half cycle. In continuous conduction the periodic steady state requires \(i(\alpha) = i(\alpha+\pi) = I_{min}\), giving:
\[ I_{min} = \frac{-\dfrac{V_m}{Z}\sin(\alpha-\phi)-\dfrac{E}{R}+\left(-\dfrac{V_m}{Z}\sin(\alpha-\phi)+\dfrac{E}{R}\right)e^{-\pi/\tan\phi}}{1-e^{-\pi/\tan\phi}} \]Conduction is continuous only while \(I_{min} \ge 0\); setting it to zero gives the critical inductance — Problem 2.
In discontinuous conduction the current is a single pulse from \(\alpha\) to \(\beta\):
\[ i(\theta) = \frac{V_m}{Z}\left[\sin(\theta-\phi)-\sin(\alpha-\phi)e^{-(\theta-\alpha)/\tan\phi}\right]-\frac{E}{R}\left[1-e^{-(\theta-\alpha)/\tan\phi}\right] \]The DCM output includes the idle interval, during which the load terminal sits at the back EMF:
\[ V_{dc} = \frac{V_m}{\pi}\left(\cos\alpha-\cos\beta\right)+\frac{E\left(\pi-\beta+\alpha\right)}{\pi} \]The check that closes every one of these problems:
\[ I_{dc} = \frac{V_{dc}-E}{R} \]True in both modes, because an inductor carries no average voltage in steady state.
A single-phase semiconverter with a separate freewheeling diode supplies a highly inductive load drawing a constant 20 A from 230 V, 50 Hz at \(\alpha = 45^\circ\). Find the output voltage and power, the conduction interval and current ratings of every device, the supply currents, and the power factor.
The output. Conduction from the supply runs from \(\alpha\) to \(\pi\); beyond that the freewheeling diode clamps the load to zero rather than letting the output reverse:
Account for all three intervals. Each half cycle contains 135° of supply conduction and 45° of freewheeling, and every ampere has to be assigned to a device:
| Device | Conducts per cycle | \(I_{avg}\) | \(I_{rms}\) |
|---|---|---|---|
| Each thyristor | 135° | 7.5 A | 12.25 A |
| Each bridge diode | 135° | 7.5 A | 12.25 A |
| Freewheeling diode | 90° | 5.0 A | 10.0 A |
Check the averages sum correctly: two thyristors at 7.5 plus the freewheeling diode at 5.0 gives 20 A &checkmark. And note that all three device currents depend on \(\alpha\) — unlike the full converter, where they did not. As \(\alpha\) rises the freewheeling diode takes over more of the duty, so it must be rated for the largest firing angle used.
The supply carries current only during the 135° window:
The two factors and the power factor:
Against 0.636 for a full converter at the same firing angle. Note that the distortion factor has also improved — from 0.900 to 0.960 — because the gap in the current waveform makes it closer to a sinusoid, exactly as the 120° blocks of Set 11 did.
Where the improvement comes from. Both factors gained, for related reasons:
The freewheeling interval removes the tail of the current block rather than shifting the whole thing, so the fundamental's centroid moves by only half the firing angle. That is the entire mechanism — and the reason it works is the same reason the converter cannot invert.
A full converter supplies a load of \(R = 1\ \Omega\) in series with \(L\) and a back EMF of 100 V, from 230 V, 50 Hz at \(\alpha = 45^\circ\). Derive the minimum-current condition, determine whether \(L = 10\) mH gives continuous conduction, and find the critical inductance.
Set up the periodic steady state. In continuous conduction the current at the start of one half cycle must equal the current at the start of the next, since successive half cycles are identical apart from sign:
The general solution over one half cycle is the forced sinusoid, the forced DC term and a transient:
Impose periodicity. Writing \(A = (V_m/Z)\sin(\alpha-\phi)\) and \(k = e^{-\pi/\tan\phi}\), and using \(\sin(\alpha+\pi-\phi) = -\sin(\alpha-\phi)\):
Conduction is continuous if and only if this is non-negative. If it comes out negative, the current would have to reverse to satisfy periodicity — which thyristors forbid — so the current instead reaches zero early and the assumption fails.
Evaluate at \(L = 10\) mH:
Substitute:
Negative, so 10 mH is not enough — the converter is discontinuous, narrowly. Note how close it is: a small change in \(L\), \(E\) or \(\alpha\) flips the mode, and with it the formula that applies.
Find the critical inductance by solving \(I_{min}(L) = 0\). Every term depends on \(L\) through \(Z\), \(\phi\) and \(k\), so this is transcendental and must be solved numerically:
So 10 mH misses by 4%. In practice one would specify 15 mH or more, because \(L_{crit}\) depends on the operating point — and the operating point is what a drive changes for a living.
How the boundary moves:
| Change | Effect on \(L_{crit}\) | Why |
|---|---|---|
| Larger \(\alpha\) | rises | less volt-second area to sustain current |
| Larger \(E\) | rises steeply | the EMF opposes conduction all cycle |
| Larger \(R\) | rises | faster decay between pulses |
| Lighter load (smaller \(I_{dc}\)) | — | equivalent to larger \(E\) — Problem 6 |
The second row is the one that matters for drives. A motor's back EMF rises with speed, so a lightly loaded machine running fast is in the worst position — large \(E\), small \(I_{dc}\), and therefore firmly discontinuous.
The same converter now has \(L = 5\) mH, well below the critical value. With \(R = 1\ \Omega\), \(E = 100\) V and \(\alpha = 45^\circ\), find the extinction angle, the conduction period, the output voltage and the average current, and verify the result.
The current starts from zero. Because the previous pulse has already died, there is no initial current to carry over, and the transient constant is fixed by \(i(\alpha) = 0\):
Two transient terms now, one for each forced component. The \(E/R\) bracket is often dropped by mistake — it is what makes the back EMF suppress the current from the very first instant.
The parameters at 5 mH:
Solve \(i(\beta) = 0\) numerically for the extinction angle:
Consistent with Problem 2, which predicted this from the sign of \(I_{min}\) without solving for \(\beta\) at all. The idle interval is only 14°, so this is marginally discontinuous — and marginal cases are exactly where using the wrong formula does the most damage, because the answer still looks plausible.
The output voltage has two contributions. During conduction the load sees the supply; during the idle interval it sees its own back EMF, because no current flows and therefore no voltage appears across \(R\) or \(L\):
The second term is the one that gets forgotten. Omitting it would give 162.0 V — wrong by 5% — and would also break the current check below.
The average current, two ways. First from the voltage:
And independently, by integrating the current pulse itself:
The agreement confirms \(\beta\), \(V_{dc}\) and the idle-interval term together. In DCM this check is not a formality — it is the only thing distinguishing a correct solution from a plausible one.
Compare with the continuous-conduction formula:
| Quantity | CCM formula | Actual (DCM) |
|---|---|---|
| \(V_{dc}\) | 146.4 V | 169.8 V |
| \(I_{dc}\) | 46.4 A | 69.8 A |
| Error | — | +50% in current |
Half again as much current as the cosine law predicts, from a converter that is only 14° short of continuous. The error in current is far larger than the error in voltage, because — as in Set 9, Problem 6 — the back EMF turns the converter into a difference amplifier.
At \(\alpha = 60^\circ\) with a constant 25 A inductive load on the same 230 V supply, compare the full converter, the semiconverter and the half-wave controlled converter with a freewheeling diode, on output, power factor, device count and quadrant capability.
The three outputs:
The semiconverter delivers half again as much as the full converter at the same firing angle — because it does not throw away the negative volt-seconds. The half-wave circuit delivers exactly half the semiconverter's output, since it uses only one half cycle.
Power factors, assembled from the two component factors:
Everything side by side:
| Property | Full converter | Semiconverter | Half-wave + FWD |
|---|---|---|---|
| \(V_{dc}\) at 60° | 103.5 V | 155.3 V | 77.7 V |
| Control law | \(\cos\alpha\) | \(1+\cos\alpha\) | \(1+\cos\alpha\) |
| DPF | \(\cos\alpha\) | \(\cos(\alpha/2)\) | \(\cos(\alpha/2)\) |
| Power factor | 0.450 | 0.827 | 0.585 |
| Ripple frequency | 100 Hz | 100 Hz | 50 Hz |
| Thyristors / diodes | 4 / 0 | 2 / 3 | 1 / 1 |
| Transformer DC | none | none | yes |
| Quadrants | I and IV | I only | I only |
| Can invert? | yes | no | no |
Which quadrants each reaches. Since thyristors conduct one way, current is always positive; only the voltage sign can change:
Neither of the freewheeling circuits can produce a negative average output at any firing angle, because the freewheeling path clamps the output at zero the moment it tries. That is the whole limitation, and it comes from the same component that gives them their power factor.
Choosing between them:
| Requirement | Choose |
|---|---|
| One-way power, best power factor | semiconverter |
| Regenerative braking needed | full converter |
| Speed reversal needed | dual converter — Set 16 |
| Very low power, cost critical | half-wave + FWD |
| Best of both | rectify at \(\alpha = 0\), chop on the DC side |
The last row is Part 3's answer and it wins on every count: a diode bridge at \(PF = 0.9\) feeding a chopper, which does the varying at 20 kHz where no supply displacement is involved at all.
A semiconverter charges a battery at a constant 20 A from 230 V, 50 Hz. The battery EMF is 120 V at the start of charge and 140 V at the end, with an internal resistance of \(0.5\ \Omega\). Find the firing angle and power factor at both points, the power split, and explain the trend.
Start of charge. The converter must supply the EMF plus the drop across the internal resistance:
The power factor there:
End of charge, with the battery risen to 140 V:
The power factor improves as the battery charges — from 0.741 to 0.810 — because a higher terminal voltage needs less firing delay. A charger is therefore at its worst electrically when the battery is at its most depleted, which is when it will be run hardest.
Where the power goes, at the start of charge:
| Destination | Expression | Power |
|---|---|---|
| Stored in the battery | \(EI\) | 2400 W |
| Internal resistance | \(I^2R_i\) | 200 W |
| Delivered by converter | \(V_{dc}I\) | 2600 W |
| Apparent power drawn | \(V_sI_s\) | 3510 VA |
Charging efficiency at the battery terminals is \(2400/2600 = 92.3\%\), and the 200 W lost internally is unavoidable at this current — it is the battery's own resistance, not the converter's.
Why the semiconverter suits this job. Three reasons, all structural:
(ii) A battery charger never needs to return power to the supply, so quadrant IV is worthless; and (iii) the freewheeling path means an accidental loss of firing pulses leaves the current decaying safely to zero rather than the battery discharging back through the converter. Note the first figure: at this large firing angle the full converter would be at 0.230, so the semiconverter is worth more than a factor of three here.
A full converter drives a DC motor with \(R_a = 0.5\ \Omega\), \(L_a = 50\) mH and \(K\phi = 1.2\ \text{V}\cdot\text{s/rad}\) from 230 V, 50 Hz at \(\alpha = 60^\circ\). Find the back EMF at which conduction becomes discontinuous, the corresponding critical armature current and speed, and describe what the drive does below it.
Set up the boundary condition from Problem 2, but solve it for \(E\) rather than \(L\) — because in a drive the inductance is fixed and the EMF is what varies:
Note how close \(\phi\) is to 90° and how close \(k\) is to 1 — a highly inductive load barely decays between pulses, which is what makes continuous conduction possible at all.
Evaluate the sinusoidal term:
Set \(I_{min} = 0\) and solve for \(E\):
Translate into a current and a speed. At the boundary the converter is still just continuous, so the cosine law still applies:
So at this firing angle the drive stays continuous only while it is delivering more than 11.5 A — about 14 N·m of torque. Below that it goes discontinuous, and 11.5 A is a perfectly ordinary light load for a machine of this size.
What happens below the boundary. The output rises, so the speed rises with it, and the speed–torque characteristic changes shape:
| Region | Output law | Speed vs load | Loop gain |
|---|---|---|---|
| Continuous (\(I_a > 11.5\) A) | \(V_{dc} = \frac{2V_m}{\pi}\cos\alpha\) | stiff, nearly flat | constant |
| Discontinuous (\(I_a < 11.5\) A) | depends on \(E\) and \(\alpha\) | rises steeply as load falls | much higher |
The speed regulation becomes poor exactly where a user would expect it to be best — at light load. And the small-signal gain from firing angle to speed rises sharply, so a controller tuned in the continuous region can become oscillatory or unstable when the load falls away.
The remedies, in the order a designer would consider them:
A series reactor is the standard answer and is why converter-fed DC drives almost always have one. Beyond that: use a semiconverter, whose freewheeling path keeps current flowing longer; add a bleeder to guarantee a minimum load; or gain-schedule the controller against measured current so it retunes itself when the mode changes. Modern digital drives do the last, having first detected the mode by checking whether the current reaches zero.
Key Formulas
| Quantity | Relation | Notes |
|---|---|---|
| Semiconverter output | \(V_{dc} = \dfrac{V_m}{\pi}\left(1+\cos\alpha\right)\) | Never negative |
| Thyristor current | \(I_{avg} = I_{dc}\dfrac{\pi-\alpha}{2\pi}\) | Falls with \(\alpha\) |
| Freewheeling diode | \(I_{avg} = I_{dc}\dfrac{\alpha}{\pi}\) | Rises with \(\alpha\) |
| Semiconverter \(I_s\) | \(I_{dc}\sqrt{(\pi-\alpha)/\pi}\) | Problem 1 |
| Semiconverter DPF | \(\cos(\alpha/2)\) | Advantage grows with \(\alpha\) |
| Load angle | \(\phi = \tan^{-1}(\omega L/R),\ Z = \sqrt{R^2+\omega^2L^2}\) | — |
| Decay factor | \(k = e^{-\pi/\tan\phi}\) | Near 1 for large \(L\) |
| Minimum current | \(I_{min} = \dfrac{-A-E/R+\left(-A+E/R\right)k}{1-k}\) | \(A = \frac{V_m}{Z}\sin(\alpha-\phi)\) |
| Continuity condition | \(I_{min} \ge 0\) | Solve \(=0\) for \(L_{crit}\) or \(E_{crit}\) |
| DCM current | \(\frac{V_m}{Z}\left[\sin(\theta-\phi)-\sin(\alpha-\phi)e^{-\frac{\theta-\alpha}{\tan\phi}}\right]-\frac{E}{R}\left[1-e^{-\frac{\theta-\alpha}{\tan\phi}}\right]\) | Two transients |
| DCM output | \(\dfrac{V_m}{\pi}\left(\cos\alpha-\cos\beta\right)+\dfrac{E(\pi-\beta+\alpha)}{\pi}\) | Do not omit the second term |
| Universal check | \(I_{dc} = (V_{dc}-E)/R\) | True in both modes |
| Critical current | \(I_{a,crit} = \dfrac{V_{dc}-E_{crit}}{R_a}\) | Sets the smoothing reactor — Problem 6 |
Common Mistakes
Assuming semiconverter device currents are independent of \(\alpha\). They are for the full converter but not here — the freewheeling diode's share grows with the firing angle — Problem 1.
Forgetting the freewheeling diode when totalling the load current. Two thyristors at 7.5 A plus the FWD at 5 A must give 20 A — Problem 1.
Using \(\cos\alpha\) for the semiconverter's displacement factor. It is \(\cos(\alpha/2)\), and at 75° that is the difference between 0.741 and 0.230 — Problems 1 and 5.
Assuming continuous conduction because the inductance “looks big”. 10 mH gave \(I_{min} = -1.94\) A here — the criterion must be evaluated — Problem 2.
Omitting the \(E/R\) transient term in the DCM current. The back EMF suppresses the current from the first instant, not just on average — Problem 3.
Omitting the idle-interval contribution to \(V_{dc}\). During the gap the load terminal sits at \(E\), worth 7.8 V of the 169.8 V here — Problem 3.
Not checking \(I_{dc} = (V_{dc}-E)/R\). It is the only independent verification available in DCM, and it catches every algebraic slip — Problem 3.
Expecting a semiconverter to reach quadrant IV. The freewheeling path that gives it a good power factor is what prevents the output going negative — Problem 4.
Assuming a charger's power factor is constant. It improves as the battery voltage rises, because less firing delay is needed — Problem 5.
Treating discontinuous conduction as an unusual case in a drive. Below 11.5 A here — an ordinary light load — the drive is discontinuous, with a softer characteristic and a higher loop gain — Problem 6.
Six problems, and both loose ends from Set 12 are tied off. The semiconverter's freewheeling interval turned out to be a third conduction state with its own device duty, growing with \(\alpha\) exactly as the thyristors' share falls. And the continuity criterion turned out to be a two-line periodicity argument that answers the question directly: at \(\alpha = 60^\circ\) with 50 mH, a drive is discontinuous below 11.5 A, which is an ordinary light load and not an edge case at all.
Everything in Sets 12 and 13 has been single phase, which means the output ripple is at 100 Hz and the smoothing reactor has to be large. Applying the same firing-angle control to the six-pulse bridge of Set 11 changes both: the ripple is at 300 Hz, the reactor shrinks, and the critical current falls with it. It also opens the door to real power levels — tens or hundreds of kilowatts — where regeneration is not a convenience but the whole reason the converter exists.
Next: Set 14 — Three-Phase Controlled Converters and Inverter Mode, where the cosine law reappears on the six-pulse bridge, the output ripple is found as a function of firing angle, inversion is taken to its commutation limit, and a four-quadrant drive is worked through end to end.