Part 6 · Chapter 26

Induction Motor Drives: V/f and Vector Control

The squirrel-cage motor won on cost and ruggedness and lost on control — its speed was fixed by the supply frequency, and every pre-electronic remedy either wasted energy or reintroduced slip rings. This chapter builds the torque-slip curve, derives why constant volts-per-hertz is the right control law, works out where field weakening must stop, and then shows how a change of coordinates turns an induction machine into something that behaves like a DC one.

Power Electronics Prof. Mithun Mondal Reading time ≈ 60 min
Where this sits
Part 6 · Electric Drives
Chapter 26 of 30 — the second of Part 6
You should already know
Three-phase inverters and SPWM from Chapter 18, space vector modulation from Chapter 19, and the two-loop cascade idea from Chapter 25.
By the end you can
Explain why constant V/f keeps torque available, size the low-speed boost, work out where field weakening begins, and describe what vector control adds that V/f cannot provide.
Time
≈ 60 min reading · ≈ 50 min problems
i What you'll learn
  • Why the cage induction motor displaced the DC machine everywhere, and the one problem that kept it from variable speed for eighty years.
  • How to read the torque–slip curve — and the single most useful fact about it: breakdown torque does not depend on rotor resistance.
  • Constant V/f: why holding the volts-per-hertz ratio fixed holds the flux fixed, and why that keeps full torque available at every speed.
  • Why V/f fails at low frequency, and how much voltage boost to add — with the penalty for adding too much.
  • What happens above base speed, and why breakdown torque there falls as \( 1/f^2 \) rather than \( 1/f \).
  • The three things V/f control fundamentally cannot do, and why they matter for a crane and not for a fan.
  • Field-oriented control: how the \( dq \) transformation turns an induction motor into something that behaves like a separately-excited DC machine.
  • The slip relation that makes indirect FOC work, and why it makes the drive sensitive to rotor temperature.
Section 26-1

Why the Cage Motor Won

Chapter 25 ended with the DC machine's fatal flaw: the commutator. The squirrel-cage induction motor has no commutator, no brushes, no slip rings and no windings on the rotor at all — just aluminium or copper bars cast into a laminated iron core and shorted by end rings.

The consequences are worth listing, because together they explain why roughly 85% of all industrial motor power is induction.

  • Nothing wears out. The only maintenance item is the bearings.
  • It is cheap. A cast rotor is one of the least expensive precision components in engineering.
  • It is sealed. No brush dust, no sparking — so it runs in flour mills, paint shops and mines where a DC machine is simply not permitted.
  • It is robust. Overload capability of 2–3 times rated torque, and a rotor that tolerates temperatures which would destroy a commutator.
  • It has a higher power density than a DC machine of the same frame size, because the rotor carries no copper losses of its own beyond the bar losses and needs no space for a commutator.

Against all that stood one problem.

Section recap. The cage rotor is cheap, sealed and maintenance-free, which is why induction motors dominate. Their one weakness — speed locked to supply frequency — was structural, not fixable by any pre-electronic method without wasting energy or reintroducing slip rings. The variable-frequency inverter removed it.
Section 26-2

Torque, Slip, and the Curve

The rotor turns at \( \omega_r \), the stator field at \( \omega_s \). The difference, expressed as a fraction, is the slip:

Slip
\[ s = \frac{\omega_s - \omega_r}{\omega_s}, \qquad \omega_r = (1-s)\,\omega_s \]

Slip is not a defect. It is the mechanism. The rotor bars only have voltage induced in them because they are moving relative to the field; at \( s = 0 \) there is no relative motion, no bar current and no torque. A cage machine must slip to produce torque, which is why the family is called asynchronous.

The frequency of the current in the rotor bars is \( f_r = s f \) — typically 1–2 Hz at rated load on a 50 Hz supply.

PER-PHASE EQUIVALENT CIRCUIT V₁ at f R₁ jX₁ jXm jX₂′ R₂′/s the only element that varies with load Reactances scale with frequency: X = 2πfL. Only R₂′/s changes with mechanical load.
The per-phase equivalent circuit. Everything mechanical is hidden inside one resistance, \( R_2'/s \) — and the power delivered to it, less the rotor copper loss, is the shaft power.
  1. Replace everything left of the rotor branch by its Thévenin equivalent
    Thévenin source and impedance
    \[ V_{th} = V_1\frac{X_m}{\sqrt{R_1^2 + (X_1+X_m)^2}}, \qquad Z_{th} = R_{th} + jX_{th} = \frac{jX_m(R_1+jX_1)}{R_1 + j(X_1+X_m)} \]
    This is legitimate because \( R_2'/s \) is the only element that changes, so everything to its left is a fixed source.
  2. Find the rotor current
    Working
    \[ I_2' = \frac{V_{th}}{\sqrt{\left(R_{th} + \dfrac{R_2'}{s}\right)^2 + (X_{th}+X_2')^2}} \]
  3. Torque is air-gap power divided by synchronous speed
    Torque equation
    \[ T = \frac{P_{ag}}{\omega_s} = \frac{3}{\omega_s}\,I_2'^2\,\frac{R_2'}{s} = \frac{3}{\omega_s}\cdot\frac{V_{th}^2\,(R_2'/s)}{\left(R_{th}+\dfrac{R_2'}{s}\right)^2 + (X_{th}+X_2')^2} \]
    Note it is \( \omega_s \), not \( \omega_r \), because the air-gap power crosses at synchronous speed.
  4. Differentiate to find the peak
    Slip at breakdown
    \[ s_{max} = \frac{R_2'}{\sqrt{R_{th}^2 + (X_{th}+X_2')^2}} \]
    Breakdown torque
    \[ T_{max} = \frac{3\,V_{th}^2}{2\,\omega_s\left[R_{th} + \sqrt{R_{th}^2 + (X_{th}+X_2')^2}\,\right]} \]
The most useful fact about the torque–slip curve
Rotor resistance appears in \( s_{max} \) but not in \( T_{max} \).

Increasing \( R_2' \) moves the peak to higher slip without changing its height. The whole curve slides sideways, keeping the same maximum.

This is the entire basis of rotor-resistance starting on wound-rotor machines: put the peak at \( s = 1 \) and you get breakdown torque at standstill. It is also why deep-bar and double-cage rotors exist — they use the skin effect in the bars to make \( R_2' \) large at starting (where \( f_r = f \)) and small at running (where \( f_r \approx 1 \) Hz), giving a high starting torque and a low running slip from a single fixed rotor.

Section recap. Slip is the mechanism, not a fault — no relative motion means no rotor current and no torque. Torque is air-gap power over synchronous speed. Below \( s_{max} \) torque is proportional to slip and the operating point is stable; beyond it the machine stalls. Rotor resistance sets where the peak is, not how high it is.
Section 26-3

Constant V/f Control

An inverter can supply any frequency. The naive step is to change the frequency and leave the voltage alone — and it destroys the machine within seconds. Understanding why gives the whole of scalar control.

  1. Start from Faraday's law applied to the stator winding
    Induced EMF
    \[ E = 4.44\,f\,N\,k_w\,\Phi \]
    with \( N \) turns, winding factor \( k_w \) and peak air-gap flux \( \Phi \).
  2. Rearrange for the flux
    Result
    \[ \Phi = \frac{E}{4.44\,N\,k_w\,f} \;\propto\; \frac{E}{f} \]
    The flux is set by the volts-per-hertz ratio, and by nothing else.
  3. See what halving the frequency alone would do Leave \( V \) at 400 V and drop \( f \) from 50 Hz to 25 Hz, and the flux doubles. The iron saturates, the magnetising current rises by a factor of ten or more, and the machine draws enormous current while producing almost nothing. This is not a subtle effect — it trips the drive or burns the stator.
  4. State the control law
    Constant V/f
    \[ \frac{V_1}{f} = \text{constant} \;\Longrightarrow\; \Phi \approx \Phi_{rated} \ \text{at every frequency} \]
    A 400 V, 50 Hz machine is driven at 8 V/Hz: 200 V at 25 Hz, 80 V at 10 Hz, 320 V at 40 Hz.
Why constant V/f is the right law
Constant flux means constant torque per ampere — so full rated torque is available at every speed down to a few hertz.

Torque in a machine is always flux times current times a constant. Hold the flux and you hold the torque capability, whatever the speed. The whole torque–slip curve simply translates along the speed axis, keeping its shape and its height.

Compare this with stator-voltage control (Chapter 21), where reducing the speed reduces the flux and the breakdown torque falls as the square of the voltage. Constant V/f gives a genuine constant-torque drive; voltage control does not.

Interactive · V/f control, boost, and field weakening

A 15 kW, 400 V, 50 Hz, four-pole machine — rated torque about 100 N·m, shown as the dashed load line. Move the frequency and watch the curve translate. Then take the frequency low and see what happens without boost.

50 Hz
10 V
Torque against speed for an inverter-fed induction machine Torque on the vertical axis against rotor speed on the horizontal. Faint curves show the family obtained at a series of stator frequencies under constant volts per hertz; the highlighted curve is the frequency selected. Each curve rises from its starting torque at zero speed to a breakdown peak and then falls steeply to zero at synchronous speed. A dashed horizontal line marks the rated load torque of one hundred newton metres. At low frequency without voltage boost the whole curve collapses below the load line; adding boost restores it. Above fifty hertz the supply voltage cannot rise further, so the peak falls as the inverse square of frequency. torque (N·m) rotor speed (rpm) rated load
Stator voltage231 V
Synchronous speed1500 rpm
Breakdown torque249 N·m
Starting torque115 N·m

Section recap. Flux is set by \( E/f \), so holding \( V/f \) constant holds the flux and keeps full torque available at every speed — the curve translates without changing shape. At low frequency the \( I_1R_1 \) drop breaks the approximation, so a voltage boost is added; too much boost saturates the machine at light load, which is why automatic \( I_1R_1 \) compensation is preferred.
Section 26-4

Beyond Base Speed

The V/f line cannot rise forever. It stops at the point where the inverter is producing all the voltage it has — the DC link is fixed, and the modulator has reached its limit. That frequency is the base speed, and for a machine matched to its supply it is the machine's own rated frequency.

Above it the voltage stays put while the frequency keeps rising, so \( V/f \) falls and the flux falls with it. This is exactly the field weakening of Chapter 25 — obtained here without a separate field winding, simply by running out of volts.

  1. Above base speed, hold the voltage and raise the frequency
    Flux
    \[ V_1 = V_{max} = \text{constant} \;\Longrightarrow\; \Phi \propto \frac{V_{max}}{f} \propto \frac{1}{f} \]
  2. Find how breakdown torque scales In \( T_{max} \) the numerator carries \( V_{th}^2 \), which is fixed, and the denominator carries \( \omega_s \) and the reactances — which all grow with \( f \):
    Scaling
    \[ T_{max} \approx \frac{3V_{th}^2}{2\omega_s(X_{th}+X_2')} \;\propto\; \frac{V^2}{f\cdot f} \;=\; \frac{V^2}{f^2} \;\propto\; \frac{1}{f^2} \]
    once the resistances become negligible against the reactances, which they do quickly above base speed.
  3. Compare with what constant power would need Constant power requires \( T \propto 1/f \). The breakdown torque falls as \( 1/f^2 \), which is faster. So the two curves must cross.
  4. Find where the constant-power region ends
    Result
    \[ \frac{T_{max,rated}}{(f/f_b)^2} = \frac{T_{rated}}{(f/f_b)} \;\Longrightarrow\; \frac{f}{f_b} = \frac{T_{max,rated}}{T_{rated}} \]
    The constant-power range equals the machine's breakdown-torque ratio. A machine with \( T_{max}/T_{rated} = 2.5 \) can hold constant power to 2.5 times base speed — and beyond that, torque must fall as \( 1/f^2 \) because the breakdown curve, not the current rating, is the limit.
The two-region picture, for an induction drive
Below base speed: constant torque, \( V/f \) fixed. Above base speed: constant power, until \( 1/f^2 \) catches up.

In practice a margin is kept — a drive is usually operated to about 80–90% of the theoretical crossover, so that the machine still has some pull-out margin for transients. Asking a field-weakened machine to develop torque close to its breakdown value leaves nothing in reserve, and a load step will simply stall it.

Section recap. Base speed is where the inverter runs out of voltage. Above it the flux falls as \( 1/f \) and breakdown torque as \( 1/f^2 \), so the constant-power region extends only to about the machine's breakdown-torque ratio — typically 2–2.5 times base speed — after which torque is limited by pull-out rather than by current.
Section 26-5

What V/f Cannot Do

V/f control is a steady-state law. Every equation behind it — the equivalent circuit, the torque–slip curve, \( \Phi = E/4.44Nk_wf \) — assumes sinusoidal steady state at a fixed frequency. That is a perfectly good assumption for a fan. It is useless for a crane.

Three limitations follow, and they are all the same limitation seen from different angles.

The three things scalar control cannot do
LimitationWhy it happensWhat it costs you
No direct torque control The drive commands frequency; torque follows from whatever slip the load happens to produce. Torque is an outcome, not an input. Cannot hold a defined torque — so no tension control, no torque limiting worth the name, and no controlled load sharing between drives.
Slow dynamic response A frequency step must propagate through the rotor flux, whose time constant is \( L_r/R_r \) — 100–500 ms in a typical machine. Torque settles in hundreds of milliseconds. Servo applications need single-digit milliseconds.
Nothing at zero speed At \( f = 0 \) there is no rotating field and no induced rotor current, however much voltage is applied. No holding torque at standstill. A hoist would drop its load; a positioning axis cannot hold position.
Section recap. V/f is a steady-state law, so it cannot command torque, cannot respond quickly, and produces nothing at zero speed. The underlying reason is that one set of terminals must do two jobs — magnetising and torque production — with no natural mechanism keeping them apart.
Section 26-6

Vector Control

Field-oriented control does one thing: it changes the coordinate system. Everything else follows.

  1. Collapse three phases into two (the Clarke transform)
    abc to stationary αβ
    \[ i_\alpha = i_a, \qquad i_\beta = \frac{1}{\sqrt3}\left(i_b - i_c\right) \]
    Legitimate because \( i_a + i_b + i_c = 0 \) in a three-wire machine — the third phase carries no independent information. Two numbers describe the stator current completely.
  2. Rotate into a frame that turns with the rotor flux (the Park transform)
    Stationary αβ to rotating dq
    \[ \begin{bmatrix} i_d \\ i_q \end{bmatrix} = \begin{bmatrix} \cos\theta & \sin\theta \\ -\sin\theta & \cos\theta \end{bmatrix}\begin{bmatrix} i_\alpha \\ i_\beta \end{bmatrix} \]
    with \( \theta \) the instantaneous angle of the rotor flux. In this frame the sinusoidal quantities become DC. A current that was three 50 Hz sinusoids is now two constants.
  3. Choose the frame so the flux lies entirely along d This is the orientation, and it is what gives the method its name. With \( \lambda_{qr} = 0 \) by construction:
    Rotor flux
    \[ \lambda_r = L_m\,i_d \qquad \text{(first-order lag, time constant } \tau_r = L_r/R_r) \]
  4. Write the torque in the new frame
    Torque under field orientation
    \[ T = \frac{3}{2}\cdot\frac{P}{2}\cdot\frac{L_m}{L_r}\,\lambda_r\,i_q \]
    Compare with \( T = k\Phi I_a \). They are the same equation. \( i_d \) plays the role of field current, \( i_q \) the role of armature current, and they are independent.
  5. Find the angle — the part that makes it work The rotor flux angle cannot be measured directly. In indirect FOC it is computed, by integrating the rotor speed plus the slip frequency that field orientation demands:
    The slip relation
    \[ \omega_{sl} = \frac{R_r}{L_r}\cdot\frac{i_q}{i_d}, \qquad \theta = \int\left(\omega_r + \omega_{sl}\right)dt \]
    This is the heart of the scheme. Get \( \omega_{sl} \) right and the orientation holds; get it wrong and the \( d \) and \( q \) axes no longer correspond to flux and torque, and the decoupling degrades.
INDIRECT FIELD-ORIENTED CONTROL speed loop flux ref i*q i*d current controllers inverse Park/Clarke SVM inverter M Clarke/Park i_d, i_q ω_sl = (R_r/L_r)(i_q/i_d) θ = ∫(ω_r + ω_sl) dt θ feeds both transforms
Indirect FOC. The two current references are independent — \( i_d \) sets the flux, \( i_q \) sets the torque — and the whole scheme depends on computing \( \theta \) correctly from the slip relation.
Choosing a control method
MethodSensorsSpeed rangeTorque responseTypical use
Open-loop V/f none required about 20:1, no zero speed 100–500 ms Fans, pumps, multi-motor groups
V/f with slip compensation current about 40:1 50–200 ms Conveyors, mixers, general process
Sensorless vector current about 100:1, poor below 1–2 Hz 5–20 ms Extruders, general machinery, most modern general-purpose drives
Closed-loop FOC current + encoder full range including zero speed 1–5 ms Hoists, winders, servo axes, traction
Direct torque control current (+ encoder for zero speed) about 100:1 1–2 ms Rolling mills, high-dynamic industrial drives
Section recap. Field-oriented control transforms the stator current into a frame rotating with the rotor flux, where \( i_d \) sets the flux and \( i_q \) sets the torque independently — reproducing the DC machine's orthogonality computationally. Indirect FOC computes the flux angle from the slip relation \( \omega_{sl} = (R_r/L_r)(i_q/i_d) \), which puts rotor resistance inside the control loop and makes the drive sensitive to rotor temperature.
Section 26-7

Worked Examples

1 Setting up a V/f drive

Problem. A 15 kW, 400 V, 50 Hz, four-pole motor has a full-load speed of 1440 rev/min, a full-load current of 29 A and \( R_1 = 0.35\ \Omega \). Find the rated slip and torque, the V/f ratio, the voltage at 15 Hz, and a suitable boost setting.

Rated slip and torque
\[ n_s = \frac{120(50)}{4} = 1500\ \text{rev/min}, \qquad s = \frac{1500-1440}{1500} = 0.04 \]
\[ \omega_r = \frac{2\pi(1440)}{60} = 150.8\ \text{rad/s}, \qquad T = \frac{15000}{150.8} = 99.5\ \text{N·m} \]
V/f ratio (line values)
\[ \frac{V}{f} = \frac{400}{50} = 8\ \text{V/Hz} \;\Longrightarrow\; V(15\ \text{Hz}) = 120\ \text{V line} \]
Boost, from the rated resistive drop
\[ V_0 \approx I_{rated}R_1 = 29(0.35) = 10.2\ \text{V per phase} \;\approx\; 17.6\ \text{V line} \]

As a percentage, \( 17.6/400 = 4.4\% \) — which is why drive manuals default the boost parameter to somewhere between 2% and 5%. That default is not arbitrary; it is the rated \( I_1R_1 \) drop of a typical machine expressed as a fraction of rated voltage.

Sanity-check the size dependence. A 1.5 kW machine might have \( R_1 = 4\ \Omega \) and a rated current of 3.5 A, giving \( I_1R_1 = 14 \) V per phase — 6% of rated. A 150 kW machine would be nearer 1%. Small machines need more boost, and that is a real physical trend rather than a quirk of a particular manufacturer: the per-unit stator resistance falls as machines get larger.

And a caution. Setting 4.4% boost on this machine gives correct flux at full load. On no load the current is perhaps 40% of rated, the actual \( I_1R_1 \) drop is 4 V rather than 10.2 V, and the machine is over-fluxed by the difference. If the load runs light at low speed for long periods, use automatic boost instead.

2 How far can field weakening go?

Problem. The same machine has a breakdown torque of 2.5 times rated. It must drive a load at 3000 rev/min. Find the flux, the breakdown torque and the torque available at that speed, with a 15% pull-out margin, and say whether the drive can deliver rated power there.

Operating point
\[ f = 100\ \text{Hz} = 2f_b, \qquad V_1 = V_{max} \;\Longrightarrow\; \frac{\Phi}{\Phi_{rated}} = \frac{1}{2} \]
Breakdown torque falls as the square
\[ T_{max} = \frac{2.5\,T_{rated}}{2^2} = 0.625\,T_{rated} = 62\ \text{N·m} \]
Torque needed for rated power at twice base speed
\[ T = \frac{T_{rated}}{2} = 49.8\ \text{N·m} \]

It fits, but only just. The required 49.8 N·m is 80% of the 62 N·m breakdown value, leaving a pull-out margin of only 1.25:1 where the machine at base speed has 2.5:1. A load step, a supply dip, or any transient that momentarily demands more torque will stall it.

Find the honest limit. With a rule of 15% margin — that is, never asking for more than 85% of breakdown:

Working
\[ \frac{T_{rated}}{(f/f_b)} = 0.85\,\frac{2.5\,T_{rated}}{(f/f_b)^2} \;\Longrightarrow\; \frac{f}{f_b} = 0.85(2.5) = 2.1 \]

So rated power is safely available to about 105 Hz, and above that the torque must be derated as \( 1/f^2 \).

The general result is worth remembering: the constant-power speed range of an induction drive is approximately the machine's breakdown-torque ratio, reduced by whatever margin you keep. A machine with a 2:1 breakdown ratio gives you less field weakening than one with 3:1, and this is a machine specification you should check before promising a wide-range drive.

3 Detuning in an indirect FOC drive

Problem. A vector drive is commissioned cold with \( R_r = 0.30\ \Omega \) and \( L_r = 0.085 \) H. At rated torque it commands \( i_d = 12 \) A and \( i_q = 26 \) A. After an hour the rotor reaches 115 °C. Find the correct slip frequency hot and cold, and comment on what the drive does wrong.

Cold, at 20 °C
\[ \omega_{sl} = \frac{R_r}{L_r}\cdot\frac{i_q}{i_d} = \frac{0.30}{0.085}\cdot\frac{26}{12} = 3.53(2.167) = 7.65\ \text{rad/s} = 1.22\ \text{Hz} \]
Hot: aluminium at 0.4% per kelvin over a 95 K rise
\[ R_r = 0.30\left[1 + 0.004(95)\right] = 0.30(1.38) = 0.414\ \Omega \]
\[ \omega_{sl,true} = \frac{0.414}{0.085}(2.167) = 10.55\ \text{rad/s} = 1.68\ \text{Hz} \]

The drive is still applying 1.22 Hz, because \( R_r \) in its equation has not changed. It is short by 0.46 Hz — about 38% too little slip.

What that does, in order:

  1. The commanded flux angle advances more slowly than the true flux, so the estimated \( d \) axis falls behind the real one.
  2. The current the drive believes is purely torque-producing now has a component along the true flux axis, and vice versa. The decoupling is lost.
  3. Because \( i_d \) is no longer purely magnetising, the actual flux differs from the commanded flux, and the torque produced by a given \( i_q \) is no longer the torque commanded — typically 10–20% low in a case like this.
  4. The speed loop compensates by demanding more \( i_q \), which raises the losses further and heats the rotor more. The error is mildly self-reinforcing.

The remedies, in increasing order of cost: a thermal model driven by the measured current (a few lines of firmware); online adaptation using the mismatch between voltage-model and current-model flux estimates; or direct FOC, which measures the flux angle instead of computing it and does not use \( R_r \) at all.

And note the diagnostic value. If a vector drive holds torque perfectly for the first twenty minutes and degrades thereafter, the cause is thermal and the parameter is \( R_r \). No amount of retuning the speed loop will fix it.

Section 26-8

Summary and Formula Sheet

Chapter 26 in five sentences:

  1. Slip is the mechanism of the cage machine, and torque below \( s_{max} \) is very nearly proportional to it.
  2. Rotor resistance sets where the breakdown peak sits, not how high it is.
  3. Flux is set by \( E/f \), so constant V/f keeps full torque available at every speed — with a boost added at low frequency to cover the \( I_1R_1 \) drop.
  4. Above base speed the flux falls as \( 1/f \) and breakdown torque as \( 1/f^2 \), so the constant-power range is about the machine's breakdown-torque ratio.
  5. Vector control resolves the stator current into flux-producing and torque-producing components in a frame rotating with the rotor flux, giving DC-machine behaviour — at the cost of needing to know the flux angle accurately.
Formula sheet · Chapter 26
Synchronous speed\(P\) = number of poles
\( n_s = \dfrac{120f}{P}, \quad \omega_s = \dfrac{4\pi f}{P} \)
Sliprotor frequency is \(sf\)
\( s = \dfrac{\omega_s-\omega_r}{\omega_s} \)
Torquefrom the Thévenin circuit
\( T = \dfrac{3V_{th}^2(R_2'/s)}{\omega_s\left[(R_{th}+R_2'/s)^2+(X_{th}+X_2')^2\right]} \)
Slip at breakdownmoves with \(R_2'\)
\( s_{max} = \dfrac{R_2'}{\sqrt{R_{th}^2+(X_{th}+X_2')^2}} \)
Breakdown torqueindependent of \(R_2'\)
\( T_{max} = \dfrac{3V_{th}^2}{2\omega_s\left[R_{th}+\sqrt{R_{th}^2+(X_{th}+X_2')^2}\right]} \)
Air-gap power splitthe reason slip costs energy
\( P_{mech} = (1-s)P_{ag}, \quad P_{cu,rotor} = sP_{ag} \)
Flux from the EMFthe basis of V/f
\( \Phi = \dfrac{E}{4.44\,N k_w f} \)
V/f law with boost\(V_0 \approx I_{rated}R_1\)
\( V_1 = V_0 + \dfrac{V_{rated}-V_0}{f_{rated}}\,f \)
Field weakeningabove base speed
\( \Phi \propto \dfrac{1}{f}, \quad T_{max} \propto \dfrac{1}{f^2} \)
Constant-power rangebefore derating
\( \dfrac{f}{f_b}\Big|_{max} \approx \dfrac{T_{max,rated}}{T_{rated}} \)
Rotor flux under orientationlag \(\tau_r = L_r/R_r\)
\( \lambda_r = L_m i_d \)
Torque under field orientationcompare \(T=k\Phi I_a\)
\( T = \dfrac{3}{2}\dfrac{P}{2}\dfrac{L_m}{L_r}\lambda_r i_q \)
Slip relationindirect FOC; \(R_r\) drifts with temperature
\( \omega_{sl} = \dfrac{R_r}{L_r}\dfrac{i_q}{i_d} \)

Key terms

Slip
The fractional difference between synchronous and rotor speed. No slip means no rotor current and no torque.
Breakdown torque
The peak of the torque–slip curve. Its height depends on voltage and leakage reactance, not on rotor resistance.
Constant V/f
Holding the volts-per-hertz ratio fixed so the air-gap flux stays at its rated value at every frequency.
Voltage boost
A fixed or current-dependent voltage offset added at low frequency to compensate the stator resistance drop.
Base speed
The speed at which the inverter reaches its maximum output voltage. Constant torque below, constant power above.
Slip compensation
Adding an estimated slip to the frequency command so shaft speed holds as load changes. A scalar-control refinement.
Field-oriented control
Resolving stator current into components along and across the rotor flux, so flux and torque can be commanded independently.
Detuning
Loss of correct field orientation, usually because the rotor resistance used in the slip relation no longer matches the hot machine.
Direct torque control
Selecting inverter states directly from hysteresis comparisons of estimated flux and torque, without transformation or a modulator.
Check yourself

Test Yourself

Chapter 26 · six questions answers hidden until you ask
Why does reducing the frequency of a fixed-voltage supply destroy an induction motor, when reducing the voltage at fixed frequency merely weakens it?

Because flux is proportional to \( V/f \), so the two changes move it in opposite directions.

The governing relation
\[ \Phi = \frac{E}{4.44Nk_wf} \]
  • Reducing \( V \) at fixed \( f \) reduces the flux. The machine is under-fluxed: torque capability falls as \( V^2 \), and it may stall, but nothing is damaged. This is the mechanism of Chapter 21's stator-voltage control.
  • Reducing \( f \) at fixed \( V \) increases the flux, in inverse proportion. Halve the frequency and the flux doubles.

And the iron will not allow it. A machine is designed with its rated flux density close to the knee of the B–H curve — typically 1.5–1.7 T for silicon steel, where saturation begins around 1.8–2.0 T. Asking for twice the flux does not give twice the flux; it gives a modest increase in flux and an enormous increase in magnetising current, because the core has left the linear region entirely.

What actually happens in the first seconds:

  1. Magnetising current rises by a factor of five to twenty.
  2. Stator copper loss rises as the square of that current.
  3. Core loss rises steeply as well, because the flux density is higher.
  4. The drive either trips on overcurrent — the usual outcome — or, on a supply with no protection, the stator insulation fails thermally.

The one-line rule: voltage down is safe and weak; frequency down alone is unsafe. That asymmetry is the entire reason V/f control exists.

A wound-rotor machine has external rotor resistance added. What happens to the starting torque, the breakdown torque, and the full-load efficiency?

Starting torque rises, breakdown torque is unchanged, efficiency falls.

Starting torque — up. The peak of the curve sits at \( s_{max} = R_2'/\sqrt{R_{th}^2+(X_{th}+X_2')^2} \). Increasing \( R_2' \) increases \( s_{max} \), sliding the whole curve towards higher slip. Choose \( R_2' \) so that \( s_{max} = 1 \) and the machine develops its full breakdown torque at standstill — the largest starting torque it is capable of.

Breakdown torque — unchanged. \( R_2' \) does not appear in \( T_{max} \) at all. This is the single most useful fact about the curve: rotor resistance relocates the peak without changing its height.

Efficiency — down, and by a predictable amount. The air-gap power divides as

Power split
\[ P_{mech} = (1-s)P_{ag}, \qquad P_{cu,rotor} = s\,P_{ag} \]

so the rotor circuit dissipates a fraction \( s \) of the air-gap power regardless of where that resistance physically sits. Running at 30% slip means throwing away 30% of the air-gap power as heat — some in the rotor bars, most in the external resistors.

Which is why this is a starting method and not a speed-control method. It is entirely reasonable to accept large losses for the few seconds of a start, and entirely unreasonable to accept them continuously. Wound-rotor speed control by resistance was used for decades on crane and mill drives precisely because nothing better existed; an inverter now does the same job at 97% efficiency.

And the modern echo of the idea: deep-bar and double-cage rotors achieve the same effect without slip rings, using the skin effect. At standstill the rotor frequency equals the supply frequency, current crowds into the top of the bar and the effective resistance is high; at running slip the rotor frequency is 1–2 Hz, the current fills the bar, and the resistance is low. One rotor, both characteristics.

A V/f drive starts a conveyor fine when it is empty but trips on overcurrent when loaded. The boost is at the factory default. What is happening, and what would over-correcting do?

The machine is under-fluxed at the starting frequency, so it cannot produce the torque the loaded conveyor needs, and the drive supplies more and more current trying.

The mechanism. Flux depends on \( E/f \), not \( V_1/f \), and \( E = V_1 - I_1(R_1+jX_1) \). At 3 Hz on a 400 V, 50 Hz machine, constant V/f gives 24 V line — and the \( I_1R_1 \) drop at starting current may be 20 V of it. Almost nothing is left to magnetise the machine.

Why it starts empty and not loaded: the empty conveyor needs little torque, so it draws little current, so the \( I_1R_1 \) drop is small and the flux is adequate. Loading it raises the current, which raises the drop, which reduces the flux — exactly when more torque is needed. The fault is self-aggravating.

The correct fix, in order:

  1. Increase the boost towards the rated \( I_1R_1 \) drop — typically 3–6% of rated voltage for a small machine.
  2. Better, enable automatic boost / IR compensation if the drive has it, so the offset tracks the actual current.
  3. Extend the acceleration ramp. Much of the starting current goes into accelerating the inertia, not into the steady-state load.
  4. Check the current limit setting — many drives ship with 110% and a conveyor start legitimately needs 150%.

Now the over-correction, which is the part people miss. Set the boost high enough for a loaded start and the machine is over-fluxed whenever it runs light at low speed:

  • The iron saturates, and magnetising current rises far more than proportionally.
  • Losses rise while output does not, so efficiency at low speed collapses.
  • The motor gets hot at low speed — where its own shaft-mounted fan is barely working — and hums audibly.

The recognisable symptoms of the two faults are opposites: too little boost trips on overcurrent under load; too much boost runs hot and noisy on no load. If you see both, the answer is not a compromise value but automatic boost.

Why does breakdown torque fall as \( 1/f^2 \) above base speed rather than \( 1/f \)?

Because both the flux and the leakage reactance work against you, and each contributes a factor of \( f \).

Start from the high-speed approximation. Above base speed the reactances dominate the resistances, so

Working
\[ T_{max} \approx \frac{3V_{th}^2}{2\,\omega_s\,(X_{th}+X_2')} \]

Now count the frequency dependence of each term with \( V \) held at its ceiling:

  • \( V_{th}^2 \) — constant. The inverter cannot give more.
  • \( \omega_s \) — proportional to \( f \).
  • \( X_{th}+X_2' = 2\pi f(L_{th}+L_2') \) — also proportional to \( f \).

Two factors of \( f \) in the denominator, none in the numerator: \( T_{max}\propto 1/f^2 \).

The physical reading. Flux falls as \( 1/f \), which alone would give \( T \propto 1/f \). But the leakage reactance also rises with \( f \), which limits the current that a given voltage can drive into the rotor circuit — a second, independent \( 1/f \). The machine loses torque capability twice over.

The consequence for drive sizing. Constant power needs \( T \propto 1/f \). Since the ceiling falls faster, the two must cross:

Crossover
\[ \frac{f}{f_b} = \frac{T_{max,rated}}{T_{rated}} \]

Beyond it, the drive is limited by pull-out rather than by heating, and torque must be derated as \( 1/f^2 \). A machine with a 2:1 breakdown ratio gives a much narrower constant-power range than one with 3:1, which is a specification worth checking before promising a wide-range drive.

Contrast with the DC machine of Chapter 25, where the constant-power region is bounded by commutation and by the risk of residual-flux runaway, not by a pull-out torque. The two machines run out of field weakening for entirely different reasons.

In field-oriented control, what exactly is being “oriented”, and why can a PI controller suddenly do a job it could not do before?

The reference frame is being oriented — rotated so that one of its axes lies exactly along the rotor flux vector.

What that buys, in two steps:

  1. The flux becomes one-dimensional. By construction \( \lambda_{qr}=0 \) and \( \lambda_{dr}=\lambda_r=L_mi_d \). The flux now depends on one current component and one only.
  2. Torque becomes a product of two independent things.
    Result
    \[ T = \frac{3}{2}\frac{P}{2}\frac{L_m}{L_r}\lambda_r i_q \]
    which is \( T = k\Phi I_a \) with \( i_d \) as the field current and \( i_q \) as the armature current.

Now the PI question, which is the more interesting half. A PI controller drives steady-state error to zero only for a constant reference — its integrator has infinite gain at DC and finite gain everywhere else. Ask it to track a 50 Hz sinusoid and it will always lag in phase and fall short in amplitude, because at 50 Hz its gain is no longer infinite.

In the rotating frame there is no sinusoid. A balanced three-phase current at 50 Hz, viewed from a frame rotating at 50 Hz, is two constants. The PI controller sees a DC reference, applies infinite DC gain, and achieves exactly zero steady-state error. The same controller that could not track the current in stationary coordinates tracks it perfectly here.

Two practical points that follow:

  • This is why FOC uses ordinary PI controllers rather than anything exotic. The transformation does the hard work; the controllers can be textbook.
  • The alternative — staying in stationary coordinates and using resonant controllers tuned to the fundamental — exists and is used in grid converters, but it needs a new resonant term for every frequency of interest, whereas the rotating frame handles the fundamental once and for all.

The cost, stated honestly: everything depends on knowing \( \theta \). An angle error of \( \delta \) means \( i_q \) is not purely torque-producing, and the decoupling degrades roughly as \( \cos\delta \) for torque and \( \sin\delta \) for the unwanted flux disturbance. Ten degrees is tolerable; forty degrees is not control at all.

You have to specify a drive for a 30 kW hoist. Why will an open-loop V/f drive not do, and what would you specify instead?

Because a hoist needs full torque at zero speed, and V/f control produces none.

The three requirements a hoist imposes, and how V/f fails each:

  • Holding torque at standstill. At \( f=0 \) there is no rotating field, so no rotor EMF, so no rotor current, so no torque — regardless of applied voltage. The load would descend.
  • Controlled torque on the way up and down. V/f commands frequency and lets the load choose the slip, so torque is an outcome. A hoist must limit torque to protect the rope and the gearbox.
  • Four-quadrant operation. Lowering a load is generating: the motor is driven by the descending mass and returns power to the DC link. V/f drives can do this, but the transition through zero speed is exactly where V/f is weakest.

What to specify:

  1. Closed-loop field-oriented control with an encoder. This is not optional for a hoist — sensorless vector loses orientation below 1–2 Hz, which is precisely the region a hoist lives in during load pick-up and set-down.
  2. A regenerative front end or a braking resistor. Lowering a 30 kW load returns roughly 30 kW to the DC link, which will trip the drive on overvoltage in under a second otherwise. An active front end recovers it to the mains; a braking chopper and resistor dissipate it, which is cheaper and very common.
  3. A mechanical brake, interlocked with the drive. Electronic holding torque disappears the instant power is lost. Safety standards require a mechanical brake, and the drive must be configured to apply torque before the brake releases and to hold torque until it is re-applied — the “brake sequencing” parameters that every hoist drive provides.
  4. Torque proving. Before releasing the brake, the drive verifies it can produce the commanded torque. If it cannot — an open phase, a failed encoder — the brake stays on.

The general lesson for drive selection: ask what happens at zero speed and what happens when the load drives the motor. Those two questions separate the applications a V/f drive can serve from the ones it cannot, far more reliably than power rating or speed range.

Practice

Problems

Three habits for induction drive work:

  1. Check the flux first. Almost every low-speed complaint is a \( V/f \) or boost problem.
  2. Remember which quantities scale with \( f \) — reactances do, resistances do not. That single distinction explains both the boost requirement and the \( 1/f^2 \) field-weakening law.
  3. Ask about zero speed and about regeneration before choosing a control method.

Problems 1–5 are direct application; 6–9 need judgement; 10–12 are design questions worth discussing in a tutorial.

  1. A six-pole, 60 Hz machine runs at 1152 rev/min. Find the synchronous speed, the slip, the rotor frequency, and the shaft speed if the drive is set to 40 Hz at the same slip.
  2. A 400 V, 50 Hz machine is to run at 20 Hz. Find the required line voltage under constant V/f, and the flux that would result if the voltage were left at 400 V.
  3. A 7.5 kW, 415 V, 50 Hz, four-pole motor draws 15 A at full load and has \( R_1 = 1.2\ \Omega \). Find the rated torque, the boost voltage, and express the boost as a percentage of rated voltage.
  4. An induction machine has \( R_{th} = 0.30\ \Omega \), \( X_{th}+X_2' = 1.6\ \Omega \), \( R_2' = 0.25\ \Omega \), \( V_{th} = 225 \) V and four poles at 50 Hz. Find \( s_{max} \), \( T_{max} \), and the torque at 4% slip.
  5. For the machine of Problem 4, find the external rotor resistance that would place maximum torque at standstill, and state the efficiency penalty of running continuously at 25% slip.
  6. A drive holds constant power from base speed. If the machine's breakdown torque is 2.2 times rated, find the maximum speed ratio at which rated power is available with a 20% pull-out margin.
  7. An indirect FOC drive uses \( R_r = 0.22\ \Omega \), \( L_r = 0.062 \) H, \( i_d = 9 \) A, \( i_q = 21 \) A. Find the slip frequency, and the error introduced if the rotor rises 90 K above the commissioning temperature.
  8. A V/f drive runs a fan perfectly but a positive-displacement pump on the same drive stalls at low speed. Explain the difference in terms of the load's torque–speed characteristic and the machine's flux.
  9. A motor on a V/f drive hums loudly and runs hot at 5 Hz on no load, but is fine at 50 Hz. Diagnose the fault, and explain why it appears only at light load.
  10. Specify the complete drive for a 45 kW extruder: state the control method, justify it against the alternatives, choose the switching frequency with reference to Chapter 18, decide whether an encoder is required, and identify what happens on a power loss.
  11. Compare rotor-resistance speed control of a wound-rotor machine with inverter control of a cage machine for a 200 kW fan running 6000 hours a year at an average of 70% speed. Quantify the annual energy difference and comment on the payback.
  12. A single inverter is to drive four identical 5.5 kW pumps in parallel. Explain why vector control cannot be used, state what control method must be used instead, size the inverter, and identify two protection functions that are lost compared with one drive per motor.