Electric Drives

A comprehensive guide to motors, converters and control — based on the works of G.K. Dubey & R. Krishnan

Author: Dr. Mithun Mondal  ·  Department of Electrical & Electronics Engineering  ·  BITS Pilani — Hyderabad Campus

An electric drive is the engineered system that turns electrical energy into controlled mechanical motion. This revision note develops the subject end to end: the dynamics that govern every drive, DC and AC machine drives, the power converters that feed them, scalar and vector control, special machines, thermal sizing, industrial and traction applications, power quality, dynamic modelling, advanced control, and a set of fully solved numerical examples. The treatment follows the classic framework of Dubey and Krishnan and is organised for quick revision, GATE preparation and university examinations.

Module 01

Fundamentals of Electric Drives

What is an Electric Drive?

Key Concept

An electric drive is an electromechanical system that converts electrical energy into mechanical motion with controlled characteristics — speed, torque, position and direction.

Electric drives dominate motion control because they are highly efficient (85–98%), span an enormous power range from milliwatts to megawatts, allow four-quadrant operation, are clean and quiet, are easy to control electronically, and can regenerate energy back to the source.

Block diagram of an electric drive showing electric source feeding a power converter, then the motor and mechanical load, with a controller and sensors forming the feedback path.
Functional block diagram of an electric drive: the electric source supplies a power converter that feeds the motor and its load, while a controller acts on converter switching using feedback from current, speed and position sensors.

Historical Evolution of Electric Drives

Drive technology evolved in distinct eras: group (line-shaft) drives and early DC motors (1880s–1920); Ward–Leonard systems and mercury-arc rectifiers (1930s–1960); the thyristor era with current- and voltage-source inverters and analog control (1960s–80s); IGBT/MOSFET power stages with field-oriented control (FOC), direct torque control (DTC) and DSP control (1980s–2000); and today's wide-bandgap (SiC, GaN) devices, sensorless and model-predictive control, digital twins and AI.

Timeline of electric drive technology from 1880 to the present, marking group drives, Ward-Leonard, the thyristor era, IGBT and FOC, and modern wide-bandgap devices.
Evolution of electric drives across five technology eras, from line-shaft group drives to wide-bandgap, sensorless and AI-assisted converters.
Key Milestones
  • 1888 — Tesla's induction motor patent
  • 1957 — the thyristor (GE) revolutionises drives
  • 1971 — Blaschke's field-orientation theory published
  • 1985 — Takahashi–Noguchi direct torque control
  • 2010+ — commercial deployment of wide-bandgap devices
The Drive Market Today

The global variable-frequency-drive (VFD) market is roughly \$25 billion (2024). About 45% of the world's electricity is consumed by motor systems, which makes VFD penetration the single largest energy-saving lever in industry.

Components of an Electric Drive

Every drive is built from five essential subsystems plus the mechanical transmission:

  1. Power source — AC mains, a DC bus, battery, fuel cell or photovoltaic array.
  2. Power modulator (converter) — adjusts voltage, current, frequency and waveform; rectifiers, choppers, inverters, cycloconverters and AC voltage controllers.
  3. Electrical motor — DC, induction (IM), synchronous (SM), PMSM, BLDC, switched-reluctance (SRM) or stepper.
  4. Sensing unit — voltage, current, speed (encoder/resolver), position and temperature.
  5. Control unit — analog or digital controller (DSP, FPGA, microcontroller) implementing speed, torque and position loops.
Functional anatomy of an electric drive: power source, power modulator, motor and load in the power path; reference command, control unit and sensing unit in the signal path.
Functional anatomy of a drive, separating the power path (source → modulator → motor → load) from the signal path (reference, control unit and sensing feedback).

Classification of Electric Drives

Drives are classified along four independent axes, and by physical configuration:

  • By source: DC drives, AC drives, hybrid.
  • By motor: induction, synchronous, DC/BLDC.
  • By control: scalar (V/f), vector/FOC, DTC/MPC.
  • By application: servo, traction, industrial.

Selection of an Electric Drive — Engineering Trade-offs

Drive selection balances eight criteria: steady-state requirements (rated power, torque, speed, duty cycle S1–S8); transient demands (starting/braking torque, acceleration); speed range and regulation; number of quadrants required (1Q, 2Q or 4Q); environment (ambient temperature, IP rating, hazardous area); power-quality and harmonic limits (IEEE 519, IEC 61000); capital plus life-cycle cost with energy-saving payback; and reliability and maintainability (MTBF, brushed versus brushless).

Typical best-fit motor and converter combinations by application.
ApplicationBest motorBest converter
Servo / roboticsPMSM / BLDCVSI + FOC
EV tractionIPMSM / IMSiC VSI + FOC/MTPA
Pumps, fansSCIMDiode rectifier + VSI (V/f)
Cranes, liftsSCIM or DC4-Q inverter / dual converter
Rolling millDC or large IM12-pulse + 4Q
Wind 2–6 MWDFIG / PMSGBack-to-back converter
CNC spindlePMSMVSI + FOC + field weakening
HVAC blowerECM / PMSMVSI + sensorless

Fundamental Torque Equation

The dynamics of every drive follow Newton's law for rotation:

Equation of motion \[ T_m - T_L = J\frac{d\omega_m}{dt} \]

Here \(T_m\) is the motor developed torque (N·m), \(T_L\) is the load torque referred to the shaft (N·m), \(J\) is the polar moment of inertia (kg·m\(^2\)) and \(\omega_m\) is the angular velocity (rad/s). Three operating states follow directly: \(T_m \gt T_L\) gives acceleration, \(T_m \lt T_L\) gives deceleration, and \(T_m = T_L\) is steady state.

When the inertia varies (a robotic arm, reeling drum or winch) an extra term appears:

\[ T_m - T_L = J\frac{d\omega_m}{dt} + \frac{\omega_m}{2}\frac{dJ}{dt} \]

The associated power balance is \(P_m = T_m\omega_m\), \(P_L = T_L\omega_m\), and the accelerating power

\[ P_{acc} = J\omega_m\frac{d\omega_m}{dt} = \frac{d}{dt}\!\left(\tfrac{1}{2}J\omega_m^2\right) \]

Referring Load Parameters to the Motor Shaft

A real drive train contains gears and translating masses. Defining the gear ratio \(a_i = \omega_i/\omega_m\), all inertias and torques are referred to the motor shaft so the single equation of motion still applies.

Equivalent inertia \[ J_{eq} = J_0 + \sum_i J_i a_i^2 + M\!\left(\frac{v}{\omega_m}\right)^{\!2} \]
Equivalent load torque \[ T_{L,eq} = T_{L0} + \sum_i \frac{T_{Li}\,a_i}{\eta_i} + \frac{F\,v}{\eta\,\omega_m} \]

These follow from energy conservation, \( \tfrac{1}{2}J_{eq}\omega_m^2 = \tfrac{1}{2}J_0\omega_m^2 + \sum_i \tfrac{1}{2}J_i\omega_i^2 + \tfrac{1}{2}M v^2\), with efficiencies \(\eta_i\) accounting for transmission losses.

Drive train with a motor coupled through a gearbox to a rotational load and to a translating mass, used to refer inertias and torques to the motor shaft.
A motor driving a rotational load through a gearbox of ratio \(a_1\) and a translating mass \(M\); each element is referred to the motor shaft to form \(J_{eq}\) and \(T_{L,eq}\).

Load Torque Characteristics

The total load torque combines several components:

\[ T_L = T_{Lf} + T_{Lw} + T_{Ls} + T_{Lg} \]

where \(T_{Lf}\) is friction \((C + B\omega_m)\), \(T_{Lw}\) is windage \((C_w\omega_m^2)\), \(T_{Ls}\) is the useful shaft work and \(T_{Lg}\) is a gravity term (hoists). Four canonical speed–torque shapes recur: constant torque (hoist), torque linear in speed (viscous friction), torque proportional to \(\omega^2\) (fans and pumps) and constant-power loads where \(T_L \propto 1/\omega\). Loads are also classified as active (hoist, crane — torque retains its sign and can drive the motor) or passive (drill, mill, press — torque always opposes motion).

Four load torque versus speed curves: constant torque, torque linear in speed, fan torque proportional to speed squared, and constant power torque inversely proportional to speed.
Characteristic load torque–speed curves: constant torque, linear (friction), fan-type \(T_L \propto \omega^2\), and constant-power \(T_L \propto 1/\omega\).

Steady-State Stability

Applying a small perturbation about an operating point and linearising the equation of motion gives

\[ \left(\frac{dT_m}{d\omega_m} - \frac{dT_L}{d\omega_m}\right)\Delta\omega_m = J\frac{d\Delta\omega_m}{dt} \]

whose solution \(\Delta\omega_m = (\Delta\omega_m)_0\,e^{t/\tau}\) has time constant

\[ \tau = \frac{J}{\dfrac{dT_L}{d\omega_m}-\dfrac{dT_m}{d\omega_m}} \]
Stability criterion
An operating point is stable when the load torque rises faster with speed than the motor torque

\( \dfrac{dT_L}{d\omega_m} \gt \dfrac{dT_m}{d\omega_m} \). A shunt motor driving a fan load (\(T_L \propto \omega^2\)) satisfies this and settles at a stable intersection.

Drooping shunt-motor torque-speed line intersecting a quadratic fan load curve at a stable equilibrium point, with restoring-flow arrows.
A drooping shunt-motor characteristic intersecting a quadratic fan load. The intersection is a stable equilibrium because perturbations produce a restoring change in net torque.

Four-Quadrant Operation

With \(P = T\omega_m\), the sign of power distinguishes motoring \((P\gt0)\) from regeneration \((P\lt0)\). Plotting torque against speed yields four quadrants: Q-I forward motoring, Q-II forward braking, Q-III reverse motoring and Q-IV reverse braking.

Torque versus speed plane divided into four quadrants labelled forward motoring, forward braking, reverse motoring and reverse braking with power sign in each.
The four-quadrant torque–speed plane. Motoring quadrants deliver positive power; braking quadrants return power, enabling regeneration.
Hoist example mapped to the four quadrants.
QuadrantActionLoadPower flow
ILift upLoadedMotoring
IILift downLoadedBraking (regen)
IIILift downEmptyMotoring
IVLift upEmptyBraking

Braking Methods — Comparison

Three electrical braking methods are used in drives. Regenerative braking occurs when \(E \gt V_s\) (or \(\omega \gt \omega_s\)): energy flows back to the source with \(P_{reg} = E I_a\), making it the most efficient method. Dynamic (rheostatic) braking disconnects the supply and connects a braking resistor, dissipating kinetic energy as heat with \(P_{diss} = E^2/(R_a + R_{br})\). Plugging reverses the supply voltage, producing a very large current \(I_a = (V+E)/(R_a + R_{br})\) for fast but inefficient stopping.

Comparison of electrical braking methods.
MethodEnergy recoveryStopping timeHeat dissipationUse case
RegenerativeYesMediumLowTraction, EV, lifts
DynamicNoMediumIn \(R_{br}\)General industrial
PluggingNoFastHighEmergency stop
Module 02

DC Motor Drives

DC Motor — Fundamental Equations

The DC machine is governed by an EMF and a torque relation that share the same machine constant \(K\phi\):

EMF and torque \[ E = K\phi\,\omega_m, \qquad T_m = K\phi\,I_a, \qquad K\phi = \frac{PZ}{2\pi A}\phi \]

Applying Kirchhoff's voltage law to the armature gives the circuit and speed equations:

\[ V_a = E + I_a R_a \] \[ \omega_m = \frac{V_a - I_a R_a}{K\phi} = \frac{V_a}{K\phi} - \frac{R_a}{(K\phi)^2}T_m \]

There are three control variables — armature voltage \(V_a\), field flux \(\phi\) and series resistance \(R_a\) — and each defines a distinct speed-control region. The mechanical time constant is \( \tau_m = JR_a/(K\phi)^2 \).

DC Machine — Construction and Cross-Section

The key parts are the yoke/frame (mechanical support and flux return path), the field poles carrying shunt or series windings that establish \(\phi\), the laminated armature whose slots hold the lap or wave winding, the commutator and brushes (a mechanical inverter that rectifies the internal AC EMF to DC at the terminals), and interpoles and compensating windings that cancel armature reaction and reduce sparking.

Generated EMF \[ E = \frac{P\,Z\,\phi\,n}{60\,A} = \underbrace{\frac{P\,Z}{2\pi A}}_{K}\,\phi\,\omega_m \]

where \(P\) is the number of poles, \(Z\) the total conductors and \(A\) the number of parallel paths (\(A=2\) for wave winding, \(A=P\) for lap winding).

Cross-section of a two-pole DC machine showing yoke, north and south field poles, field windings, slotted armature, commutator and brushes.
Cross-section of a two-pole DC machine: the yoke returns the pole flux, the slotted armature carries the winding, and the commutator with brushes rectifies the internal EMF to DC.

Types of DC Motors — Characteristics

The four excitation arrangements give markedly different speed–torque characteristics, which determine where each is used.

Speed versus torque curves for separately excited, shunt, series and compound DC motors.
Speed–torque curves of DC machines. The series motor shows the steepest droop and very high starting torque; separately excited and shunt motors hold speed nearly constant.
TypeSpeed regulationStarting torqueApplication
Separately excitedExcellentMediumServo, precision drives
ShuntGoodMediumFans, pumps, lathes
SeriesPoor (no-load overspeed)Very highTraction, cranes
CompoundGoodHighRolling mills, compressors

Speed Control — Three Regions

A separately excited DC motor offers two control regions. Below base speed, the flux is held at its rated value and the armature voltage is varied, giving a constant-torque region:

\[ \omega_m = \frac{V_a - I_a R_a}{K\phi_{rated}} \]

Above base speed, the voltage is capped and the field is weakened, so \( \omega_m \propto 1/\phi \). Power remains constant while \(T_{max} \propto \phi \propto 1/\omega_m\) — the constant-power region.

Torque and power versus speed showing the constant-torque region below base speed and the constant-power field-weakening region above base speed for a DC motor.
Constant-torque (armature-voltage) region below base speed and the constant-power (field-weakening) region above it, with the series-compensation region at the highest speeds.

Starting of a DC Motor

▲ Starting problem

At \(t = 0^+\), the speed is zero so \(E = 0\) and the armature current is limited only by \(R_a\): \( I_{a,start} = V/R_a \approx 10\text{–}20\,I_{a,rated} \). This damages the armature and trips protection.

Three solutions are used: a stepped rheostatic starter (traditional), a reduced-voltage start through a converter (modern), or the Ward–Leonard system (legacy, smooth). For an \(n\)-step starter the current swings between a maximum \(I_1\) and minimum \(I_2\):

Starter design \[ \gamma = \frac{I_1}{I_2} = \left(\frac{V/R_a}{V/R_{1}}\right)^{1/n}, \qquad R_k = R_a\,\gamma^{\,n-k+1}, \qquad n = \frac{\log(V/I_2 R_a)}{\log(I_1/I_2)} \]

Power Semiconductor Devices — the Drive Toolbox

The converter that feeds the motor is built from power semiconductors. The choice of device fixes the achievable voltage, current and switching frequency.

DeviceVoltageCurrent\(f_{sw}\)ControlTypical drive use
Diode8 kV5 kA50 Hz–MHzUncontrolledFront-end rectifier, free-wheel
SCR12 kV6 kA< 1 kHzTurn-on onlyPhase rectifier, LCI, cycloconverter
GTO6 kV6 kA1–3 kHzTurn-on/offLegacy MV drives, traction
IGCT10 kV5 kA~1 kHzGate-commutatedMV multilevel inverters
MOSFET (Si)1 kV200 A100 kHz–MHzGate voltageServo, low-power VFD, BLDC
IGBT6.5 kV3 kA5–30 kHzGate voltageWorkhorse of modern VFDs
SiC MOSFET10 kV300 Aup to 200 kHzGate voltageEV traction, solar, fast chargers
GaN HEMT650 V100 AMHzGate voltageServo, on-board chargers, LV drives
Loss & thermal rule of thumb \[ P_{sw} = \tfrac{1}{2}V_{off}I_{on}(t_{on}+t_{off})\,f_{sw}, \qquad P_{cond} = R_{ds(on)}I_{rms}^2 \;(\text{MOSFET}) \] \[ T_j = T_a + (P_{cond}+P_{sw})\,R_{th(j\text{-}a)} \]

Performance Indices for Phase-Controlled Converters

Phase-controlled converters are characterised by DC-side and AC-side indices. On the DC side,

\[ V_{dc} = \frac{1}{T}\!\int_0^{T}\!v_o\,dt, \quad V_{rms} = \sqrt{\frac{1}{T}\!\int_0^T v_o^2\,dt}, \quad FF = \frac{V_{rms}}{V_{dc}}, \quad RF = \sqrt{FF^2-1} \]

On the AC side, the efficiency \(\eta = P_{dc}/P_{ac}\), transformer utilisation factor \(\text{TUF} = P_{dc}/(V_sI_s)_{rated}\), displacement power factor \(DPF = \cos\phi_1\), harmonic factor \(HF = \sqrt{I_s^2-I_{s1}^2}/I_{s1}\) and overall power factor \(PF = (I_{s1}/I_s)\cos\phi_1\).

These matter directly for DC drives: a low ripple factor gives smooth armature current and low torque ripple; a high TUF means better transformer utilisation; a high power factor reduces line current and \(I^2R\) loss; and a low harmonic factor secures compliance with IEEE 519 and IEC 61000-3-2.

▲ Continuous versus discontinuous conduction

At light load or large firing angle, \(i_a\) may fall to zero before the next firing — discontinuous conduction mode (DCM). In DCM the output voltage rises and regulation degrades. A smoothing inductor \(L_a\) keeps the drive in continuous conduction mode (CCM).

Single-Phase Phase-Controlled Converters

Single-phase converter topologies and their average output voltage (continuous conduction).
TopologyAverage \(V_a\) (CCM)Quadrants
Half-wave (1 SCR)\(V_a = \dfrac{V_m}{2\pi}(1+\cos\alpha)\)1 (Q-I)
Semi (2 SCR + 2 D)\(V_a = \dfrac{V_m}{\pi}(1+\cos\alpha)\)1 (Q-I)
Full / bridge (4 SCR)\(V_a = \dfrac{2V_m}{\pi}\cos\alpha\)2 (Q-I, IV)
Dual (two full)\(V_a = \pm\dfrac{2V_m}{\pi}\cos\alpha\), with \(\alpha_1+\alpha_2 = 180^\circ\)4

For the full bridge with inductive load, the key design relations are \(V_a = \tfrac{2V_m}{\pi}\cos\alpha\), \(I_a = (V_a - E)/R_a\), \(V_{a,rms} = V_m/\sqrt{2}\), \(FF = \pi/(2\sqrt{2}\cos\alpha)\), fundamental source current \(I_{s1} = 4I_a/(\pi\sqrt 2)\) and \(PF \approx 0.9\cos\alpha\). With \(\alpha \lt 90^\circ\) the converter rectifies; with \(\alpha \gt 90^\circ\) it inverts and returns energy (regeneration).

Normalised average output voltage versus firing angle for single-phase full, semi and half-wave controlled converters, marking rectification and inversion regions.
Average output voltage versus firing angle for single-phase controlled converters. Only the full converter crosses into the inversion region for regenerative operation.

Single-Phase Full Converter with R-L-E (DC Motor) Load

Solving \(L_a\dot i + R_a i = v_o(t) - E\) gives the steady-state armature current in continuous conduction:

\[ i_a(\omega t) = \frac{V_m}{Z}\sin(\omega t - \phi) - \frac{E}{R_a} + A\,e^{-(\omega t-\alpha)/\omega\tau_a} \]

with \(Z = \sqrt{R_a^2 + (\omega L_a)^2}\), \(\phi = \tan^{-1}(\omega L_a/R_a)\) and \(\tau_a = L_a/R_a\). The average current is \(I_a^{avg} = (V_a - E)/R_a\). The critical inductance for the CCM boundary is approximately \(L_{a,crit} \approx V_m\sin\alpha/(\omega I_{a,min})\); below this the drive enters DCM and \(V_a\) rises.

Single-Phase Converter-Fed DC Drives — Quadrant Map

For a single full converter, \(V_a = \tfrac{2V_m}{\pi}\cos\alpha\): with \(0 \le \alpha \lt 90^\circ\) the drive rectifies in Q-I, and with \(90^\circ \lt \alpha \le 180^\circ\) it inverts in Q-IV (regeneration). A semi-converter, \(V_a = \tfrac{V_m}{\pi}(1+\cos\alpha)\), is single-quadrant (no inversion). A dual converter (two anti-parallel full bridges) achieves four-quadrant operation: in non-circulating mode \(\alpha_1 + \alpha_2 = 180^\circ\) with one bridge active; in circulating mode both are active and a reactor limits the circulating current \(i_{circ} = \tfrac{1}{\omega L_r}\!\int (v_{o1}-v_{o2})\,dt\).

Armature voltage versus armature current plane showing forward motoring, forward regeneration, reverse motoring and reverse regeneration for a single-phase converter-fed DC drive.
Quadrant map for single-phase converter-fed DC drives: a single full converter covers Q-I and Q-IV, while a dual converter reaches all four quadrants.

Three-Phase Phase-Controlled Converters

Three-phase converters, average output and input power factor in continuous conduction.
ConverterAverage \(V_a\)Pulse / QuadrantsInput PF (CCM)
Half-wave (3 SCR)\(\dfrac{3\sqrt 3 V_m}{2\pi}\cos\alpha\)3 / Q-I, IV\(\tfrac{3}{2\pi}\cos\alpha\)
Semi (3 SCR + 3 D)\(\dfrac{3V_{mL}}{2\pi}(1+\cos\alpha)\)3 or 6 / Q-I\(\le 0.955\)
Full / 6-pulse\(\dfrac{3\sqrt 2 V_{LL}}{\pi}\cos\alpha\)6 / Q-I, IV\(\approx 0.955\cos\alpha\)
Dual / 12-pulse\(\alpha_1+\alpha_2=180^\circ\)6 / 4-Q (12-pulse)\(\approx 0.99\cos\alpha\)

For the three-phase full bridge with inductive load, \(V_a = \tfrac{3\sqrt 2 V_{LL}}{\pi}\cos\alpha\), \(I_{s,rms} = \sqrt{2/3}\,I_a\), \(I_{s1} = \tfrac{\sqrt 6}{\pi}I_a\), \(HF = 0.311\), \(DPF = \cos\alpha\), \(PF = \tfrac{3}{\pi}\cos\alpha\) and the ripple frequency is \(6f\). Source inductance modifies the output to \(V_a = \tfrac{3\sqrt 2 V_{LL}}{\pi}\cos\alpha - \tfrac{3\omega L_s I_a}{\pi}\).

Three-Phase Full Converter-Fed DC Drive — Operating Modes

The speed–torque relation in continuous conduction is a family of parallel lines, one per firing angle:

\[ \omega_m = \frac{3\sqrt 2 V_{LL}\cos\alpha}{\pi K\phi} - \frac{R_a}{(K\phi)^2}T \]

At light load the converter enters DCM where \(V_a = \tfrac{3V_{mL}}{\pi}[\cos\alpha - \cos(\alpha+\beta)]\) with \(\beta \lt 60^\circ\), and the output becomes load-dependent. Four-quadrant reversing drives (rolling mills) use a dual converter with \(\alpha_1 + \alpha_2 = 180^\circ\) so that \(V_{a1} = -V_{a2}\), a reactor limiting the circulating current.

Per-unit output voltage versus firing angle for three-phase full and semi controlled converters, showing motoring and regenerative regions.
Normalised output of three-phase full and semi converters versus firing angle, with \(V_{a0} = 3\sqrt2 V_{LL}/\pi\) as the uncontrolled DC output.

Discontinuous conduction, source inductance and filtering all degrade performance. A critical inductance keeps the three-phase full converter in CCM:

\[ L_{a,crit} \ge \frac{V_{mL}\sin\alpha}{6\omega I_{a,min}} \]

Phase control gives a poor power factor at low speed (\(PF = 0.955\cos\alpha\)). It is improved by asymmetrical or sequence control of multi-stage SCR banks, by a PWM active front-end (giving unity power factor and sinusoidal line current) or by 12-pulse operation for harmonic mitigation.

Chopper-Fed DC Drives — Five Classes

DC–DC choppers feed DC motors from a DC bus and are grouped into five classes by the polarity of voltage and current they allow. The duty ratio is \(\delta = t_{on}/T\).

ClassPolarityQuadrantsOutput
A\(V_a\gt0,\,I_a\gt0\)Q-I (motoring)\(V_a = \delta V_s\)
B\(V_a\gt0,\,I_a\lt0\)Q-II (regen)\(V_a = (1-\delta)V_s\)
C\(V_a\gt0,\,\pm I_a\)Q-I + II\(V_a = \delta V_s\)
D\(\pm V_a,\,I_a\gt0\)Q-I + IV\(V_a = (2\delta-1)V_s\)
E\(\pm V_a,\,\pm I_a\)4-Q (H-bridge)\(V_a = (2\delta-1)V_s\)

For the Class A buck chopper the ripple is \(\Delta I_a \approx V_s\delta(1-\delta)/(f_c L_a)\), maximal at \(\delta = 0.5\), with critical inductance \(L_{a,crit} = V_s\delta(1-\delta)/(f_c I_{a,min})\). The Class B boost chopper regenerates by boosting the motor EMF onto the bus, with \(\delta_{regen} = 1 - (E - I_aR_a)/V_s\) and \(P_{reg} = E|I_a|\). Class E (the H-bridge) gives full four-quadrant operation, and unipolar PWM offers four times lower ripple than bipolar PWM. Control is usually fixed-frequency PWM (variable \(\delta\)) or hysteretic, where \(i_a\) is bounded between limits and the frequency varies.

Circuit schematic of a four-quadrant H-bridge chopper feeding a DC motor, with two upper and two lower switches and freewheeling diodes.
Four-quadrant (Class E) H-bridge chopper feeding a DC motor; bipolar or unipolar PWM of the four switches sets both the polarity and magnitude of the armature voltage.

Closed-Loop Control — Cascade Structure

Modern DC drives use a cascade of two loops: a fast inner current loop and a slower outer speed loop. The armature current and mechanical responses are first-order:

\[ \frac{I_a(s)}{V_a(s)-E(s)} = \frac{1/R_a}{1+s\tau_a},\quad \tau_a = \frac{L_a}{R_a}; \qquad \frac{\omega_m(s)}{T(s)-T_L(s)} = \frac{1}{Js+B} \]

The cascade arrangement is preferred because saturation of the speed-loop PI sets a natural current limit, the inner loop gives fast current (and hence torque) control, and the outer loop gives good speed regulation. A bandwidth ratio of about 10:1 between the loops keeps them decoupled.

Cascade control block diagram with an outer speed PI loop, inner current PI loop, converter, motor, tachogenerator and current sensor feedback.
Cascade speed–current control of a converter-fed DC drive. The outer speed PI commands the inner current PI; tachogenerator and current-sensor signals close the two loops.

Ward–Leonard System versus Modern Solid-State Drive

The classical Ward–Leonard system varies DC-motor speed through the field of a motor-generator set — an induction motor drives a DC generator whose field rheostat sets the armature voltage of the DC motor. It is smooth and inherently four-quadrant, but uses three rotating machines, is bulky and only 60–70% efficient. A modern solid-state drive replaces the generator set with a four-quadrant dual converter under closed current and speed loops — compact, 92–97% efficient and with millisecond response.

Side-by-side comparison of the classical Ward-Leonard motor-generator set and a modern dual-converter solid-state DC drive.
Classical Ward–Leonard motor–generator scheme (left) versus a modern dual-converter solid-state drive (right) with digital current and speed loops.
AspectWard–LeonardSolid-state
Efficiency60–70%92–97%
Size & weightVery largeCompact
MaintenanceHigh (3 rotating machines)Low (static)
ResponseSlow (field time constant)Fast (ms)
Status todayObsoleteIndustry standard
Module 03

Induction Motor Drives

Induction Motor — Fundamentals

The induction motor runs below the rotating field. Its key speeds and slip are

\[ n_s = \frac{120f}{P}\ \text{rpm}, \quad \omega_s = \frac{4\pi f}{P}\ \text{rad/s}, \quad s = \frac{n_s-n}{n_s} = \frac{\omega_s-\omega_m}{\omega_s} \]

The rotor quantities scale with slip: rotor frequency \(f_r = sf\), rotor EMF \(E_{2s} = sE_2\), rotor reactance \(X_{2s} = sX_2\), so \(Z_{2s} = R_2 + jsX_2\). The per-phase equivalent circuit places \(R_1\) and \(X_1\) in the stator, a magnetising branch \(X_m\), and the referred rotor branch \(X_2'\) in series with \(R_2'/s\).

Per-phase equivalent circuit of an induction motor with stator resistance and reactance, magnetising reactance, referred rotor reactance and the slip-dependent resistance R2 prime over s.
Per-phase equivalent circuit of an induction motor. The slip-dependent resistance \(R_2'/s\) absorbs the air-gap power, of which the fraction \((1-s)\) becomes mechanical output.
Power flow \[ P_{ag} = 3I_2'^2\frac{R_2'}{s}, \quad P_{cu2} = sP_{ag}, \quad P_{mech} = (1-s)P_{ag}, \quad T = \frac{P_{ag}}{\omega_s} \]

Parameter Estimation — No-Load and Blocked-Rotor Tests

The equivalent-circuit parameters are found from two tests. In the no-load test (rated voltage and frequency, rotor free, \(s \to 0\)):

\[ R_{NL} = \frac{P_{NL}}{3I_{NL}^2}, \quad Z_{NL} = \frac{V_{NL}}{\sqrt 3 I_{NL}}, \quad X_{NL} = \sqrt{Z_{NL}^2 - R_{NL}^2}, \quad X_m \approx X_{NL} - X_1 \]

In the blocked-rotor test (rotor locked, \(s = 1\), reduced voltage to circulate rated current):

\[ R_{eq} = \frac{P_{BR}}{3I_{BR}^2}, \quad X_{eq} = \sqrt{Z_{BR}^2 - R_{eq}^2} \]

For a NEMA design-B machine, \(X_1 \approx X_2' \approx X_{eq}/2\) and \(R_2' \approx R_{eq} - R_1\). In practice \(R_1\) is measured separately by a DC test (with an AC/DC ratio of about 1.05–1.2), the blocked-rotor test is run at reduced frequency (about 25%) for high-efficiency designs to avoid skin-effect bias, and the no-load friction-and-windage loss is separated by extrapolating to zero voltage.

Power Flow and Efficiency

Power passes from the input through stator copper loss, the air gap, rotor copper loss and friction-and-windage loss to the shaft. The core relations are \(P_{ag} = 3I_2'^2 R_2'/s\), \(P_{cu2} = sP_{ag}\), \(P_{mech} = (1-s)P_{ag}\), \(P_{out} = P_{mech} - P_{f+w}\) and \(T_e = P_{ag}/\omega_s\).

Power flow diagram of an induction motor from input power through stator copper loss, air-gap power, core loss, rotor copper loss and friction and windage to output power.
Power-flow diagram of an induction motor. Each stage sheds a loss component; the air-gap power splits into mechanical power and rotor copper loss in the ratio \((1-s):s\).

Torque–Slip Characteristic

Torque rises with slip to a maximum (the breakdown torque) and then falls. The slip at maximum torque and the Kloss approximation are

\[ s_{mT} = \pm\frac{R_2'}{\sqrt{R_1^2+(X_1+X_2')^2}}, \qquad \frac{T}{T_{max}} = \frac{2}{\,s/s_{mT} + s_{mT}/s\,} \]

The same characteristic describes motoring (\(0 \lt s \lt 1\)), plugging/braking (\(s \gt 1\)) and generating (\(s \lt 0\)).

Torque versus slip characteristic of an induction motor marking the motoring, braking and generating regions, with the breakdown torque and starting torque points.
Torque–slip characteristic showing the motoring, braking and generating regions, the breakdown point \((s_{mT}, T_{max})\) and the starting torque at \(s = 1\).

Starting Methods for Induction Motors

Method\(V_{start}\)\(T_{start}/T_{fl}\)Remarks
Direct on-line (DOL)\(1.0\)1.5–2.5High \(I_{start} \approx 6I_{fl}\); small motors
Star–delta\(V/\sqrt3\)↓ to \(1/3\)Torque and current drop to one-third
Auto-transformer\(kV\)\(k^2\) of DOLAdjustable tap; smooth transition
Rotor resistance (slip-ring)\(V\)up to \(T_{max}\)\(s_{mT}\) shifted toward \(s = 1\)
Soft starter (SCR)VariableVariableLow cost; voltage ramp
VFD (VVVF inverter)\(V \propto f\)up to \(T_{max}\)Best: low current, high torque

For star–delta starting, \(I_Y = I_{DOL}/3\) and \(T_{Y/\Delta} = \tfrac{1}{3}T_{DOL}\). For an auto-transformer at tap \(k\), the line current is \(k^2 I_{DOL}\) and the starting torque is \(k^2 T_{DOL}\).

Braking of Induction Motors

Regenerative braking requires \(\omega_m \gt \omega_s\) (so \(s \lt 0\)) — from an active load (a descending hoist or downhill EV) or by reducing the supply frequency below the rotor speed in a VVVF drive; torque reverses and power flows to the source. Plugging swaps two stator phases to reverse \(n_s\); the slip becomes \(s = 2 - s_{old}\), torque opposes rotation and the motor decelerates rapidly, but it must be disconnected near zero speed to prevent reversal. DC dynamic braking disconnects the AC supply and injects DC into two stator phases, creating a stationary field in which the rotor acts as a loaded synchronous generator; the equivalent AC current for a star connection is \(I_{ac,eq} = \sqrt{2/3}\,I_{dc}\), and the braking torque is adjustable through \(I_{dc}\) and the rotor resistance.

Speed Control Methods — Summary

Induction-motor speed control divides into three families. Stator-side methods change the stator voltage (\(T \propto V^2\)), the frequency (which moves \(n_s\)), the V/f ratio (which preserves flux) or the pole count (discrete speeds). Rotor-side methods, available only on slip-ring machines, add rotor resistance (inefficient) or recover the slip power (static Kramer, Scherbius/DFIG, rotor-EMF injection). High-performance methods give DC-like control: field-oriented control (FOC), direct torque control (DTC) and model-predictive control (MPC).

Stator Voltage Control — AC Voltage Controller

Varying the stator voltage at fixed frequency through an anti-parallel SCR pair (a TRIAC for small motors) changes the torque without holding the rotor flux constant. Because torque scales with the square of voltage at any given slip,

\[ T \propto V_1^2 \cdot \frac{R_2'/s}{(R_1+R_2'/s)^2+(X_1+X_2')^2} \quad\Rightarrow\quad T \propto V_1^2 \ \text{at fixed }s \]

the slip at maximum torque is unchanged while \(T_{max}\) falls as \(V_1^2\). For an R-load with firing angle \(\alpha\), \(V_{1,rms} = V_{ph}\sqrt{1 - \alpha/\pi + \sin 2\alpha/2\pi}\).

Torque versus speed curves at three stator voltages intersecting a quadratic fan load, showing the operating point sliding as voltage decreases.
Stator-voltage control: as \(V_1\) falls the torque curve shrinks as \(V_1^2\) but \(s_{mT}\) stays fixed, so the operating point on a fan load slides to lower speed. Best suited to \(T \propto \omega^2\) loads.

Constant V/f Control — the Workhorse

Key Concept

To hold the air-gap flux constant as frequency changes, keep \(V_1/f = \text{constant}\). Since \(\phi \propto V_1/f\), this avoids saturation below base speed and allows field weakening above it.

Below base frequency the drive operates in the constant-torque region; above base frequency it enters the constant-power (field-weakening) region. At low frequency the stator resistance drop becomes significant and the flux collapses, so a voltage boost is added: \(V_1 = V_{boost} + kf\).

Family of torque-speed curves for constant V/f induction motor control showing the constant-torque region and the field-weakening region where maximum torque falls as one over frequency squared.
Constant V/f control: in the constant-torque region the breakdown torque is preserved; above base frequency the voltage is capped and \(T_{max} \propto 1/f^2\) in the field-weakening region.

VSI versus CSI — Two Inverter Philosophies

A voltage-source inverter (VSI) presents a stiff DC voltage through a large capacitor and outputs a six-step or PWM voltage; its fundamental in six-step mode is \(V_1 = 2V_d/\pi\), PWM uses modulation index \(m_a = V_{ctrl}/V_{tri}\), and four-quadrant operation needs anti-parallel diodes plus an active front-end. A current-source inverter (CSI) presents a stiff DC current through a large inductor and outputs a quasi-square current; the motor sets the voltage, four-quadrant operation is inherent, and it suits very large machines.

Voltage-source inverter with a DC-link capacitor and current-source inverter with a DC-link inductor, both feeding a six-switch bridge and an induction motor.
VSI (capacitor DC link, stiff voltage) versus CSI (inductor DC link, stiff current) feeding an induction motor through a six-switch bridge.
AspectVSICSI
DC-link elementCapacitorInductor
Output waveformVoltage (6-step / PWM)Current (quasi-square)
Power rating1 kW – MWHundreds of kW – MW
Typical useGeneral, servoVery large induction motors

Six-Step VSI — Voltage and Harmonic Analysis

With \(180^\circ\) conduction, each switch conducts for half a cycle and three conduct at once, producing six unique switch combinations and a six-step phase voltage:

\[ v_{an} = \frac{V_d}{\pi}\!\!\sum_{n=1,5,7,\ldots}\!\!\frac{4}{n}\sin n\omega t \]

The fundamental is \(V_{an,1} = 2V_d/\pi\) with harmonics \(V_{an,n} = V_{an,1}/n\) for \(n = 6k\pm1\); the line-voltage fundamental is \(V_{ab,1} = 2\sqrt3 V_d/\pi\). The RMS values are \(V_{an,rms} = \sqrt{2/3}\,V_d \approx 0.471V_d\) and \(V_{ab,rms} \approx 0.816V_d\), with a voltage THD of about 31%.

Six-step phase voltage waveform of a voltage-source inverter over one electrical cycle, with levels at plus and minus two-thirds and one-third of the DC voltage.
Six-step phase voltage \(v_{an}\) of a VSI, stepping between \(\pm V_d/3\) and \(\pm 2V_d/3\) over one fundamental cycle.

PWM Techniques for VSI

Sinusoidal PWM compares a sinusoidal reference with a high-frequency triangular carrier. The modulation index \(m_a = \hat V_{ref}/\hat V_{tri}\) (with \(0 \le m_a \le 1\) in the linear range) sets the output: \(\hat V_{1,line} = m_a \tfrac{\sqrt3}{2}V_d\). Overmodulation (\(m_a \gt 1\)) adds low-order harmonics.

Sinusoidal PWM showing a sinusoidal reference signal compared against a high-frequency triangular carrier wave, with modulation-index reference lines.
Sinusoidal PWM: the sinusoidal reference \(v_r = m_a\sin\omega t\) is compared with the triangular carrier \(v_c\) to generate the switching pattern.

Advanced schemes improve on basic SPWM: space-vector PWM (SVPWM) raises bus utilisation by 15% (\(V_{1,max} = V_d/\sqrt3\)); third-harmonic injection gives a similar gain; discontinuous PWM lowers switching loss; and random PWM spreads the EMI spectrum.

Inverter Dead-Time and Compensation

▲ Why dead-time?

The two switches in one leg must never conduct together (shoot-through). A blanking interval \(t_d\) is inserted between turn-off and turn-on, which introduces an average voltage error.

\[ \Delta V = \frac{t_d + t_{on} - t_{off}}{T_s}\,V_{dc}\,\mathrm{sgn}(i_{leg}) \]

Dead-time produces low-order distortion (5th, 7th harmonics), torque ripple and audible noise, worst at low fundamental amplitude. Compensation uses sign-of-current correction (add or subtract \(\Delta V\)), adaptive observers, or wide-bandgap devices with much smaller \(t_d\) (50 ns versus 2 µs). PWM also produces a common-mode voltage \(V_{cm} = (v_a+v_b+v_c)/3\) that drives bearing currents and EMI, mitigated by common-mode chokes, shielding and CM-aware modulation.

Multilevel Inverters for Medium-Voltage Drives

Why multilevel?

At medium voltage (2.3–13.8 kV) a single switch cannot block the bus, so devices are stacked or the voltage is partitioned across several capacitors to build a stair-step output — lowering \(dv/dt\), reducing THD and shrinking filters.

\[ V_{step} = \frac{V_{dc}}{n-1}, \qquad \text{capacitors} = (n-1), \qquad \text{switches per leg} = 2(n-1) \]

The common topologies are the neutral-point-clamped (NPC) inverter with clamping diodes, the flying-capacitor (FC) inverter with floating capacitors, the cascaded H-bridge (CHB) with isolated DC sources (modular), and the modular multilevel converter (MMC) used for HVDC and very-high-voltage drives.

Staircase output voltage waveform of a multilevel inverter approximating a sine wave with multiple discrete voltage levels.
Stepped output of a multilevel inverter: more levels approximate the sinusoid more closely, reducing harmonic distortion and \(dv/dt\) stress on the motor insulation.

Cycloconverter and Slip-Power Recovery

A cycloconverter performs direct AC–AC frequency conversion (output frequency typically \(\le f_{in}/3\)), used for very large low-speed drives such as ball mills and ship propulsion. On slip-ring machines, the slip power can be recovered rather than wasted.

The static Kramer drive rectifies the rotor slip power and inverts it back to the mains through a line-commutated inverter; the converter is rated at only about 30% of the motor rating, but it allows sub-synchronous operation only. The slip-power balance gives \(P_{ag} = T\omega_s\), \(P_{slip} = sP_{ag}\), and \(\omega_m = \omega_s\left(1 - V_{dc,inv}/V_{dc,rect}\right)\).

The Scherbius drive uses a bidirectional rotor converter (cycloconverter or back-to-back), enabling both sub- and super-synchronous operation. This is the basis of the doubly-fed induction generator (DFIG) used in wind turbines.

Static Kramer slip-power recovery with rotor rectifier and line-commutated inverter, beside a Scherbius scheme with a bidirectional rotor converter feeding the mains.
Static Kramer (sub-synchronous only) and Scherbius (sub- and super-synchronous) slip-power recovery. The Scherbius bidirectional rotor converter underlies the DFIG wind turbine.

Vector Control (Field-Oriented Control)

The big idea

Transform the stator currents into two orthogonal components aligned with the rotor-flux frame: \(i_{ds}\) (flux-producing, like a DC field current) and \(i_{qs}\) (torque-producing, like a DC armature current). The result is decoupled, DC-like control of an AC machine.

Rotor-flux frame \[ \psi_r = \frac{L_m\,i_{ds}}{1+s\tau_r}, \quad \tau_r = \frac{L_r}{R_r}, \qquad T_e = \frac{3P}{4}\cdot\frac{L_m}{L_r}\psi_r\,i_{qs}, \qquad \omega_{sl} = \frac{L_m\,i_{qs}}{\tau_r\,\psi_r} \]

There are two variants: direct FOC, where the flux is measured (Hall/search coil) or estimated from a voltage model, and indirect FOC, where the slip frequency is added to the rotor speed — simpler and more popular. FOC needs an accurate rotor resistance (it drifts with temperature), so online adaptation or a model-reference adaptive system (MRAS) is used, along with an encoder or a sensorless observer.

Direct Torque Control (DTC)

DTC controls torque and stator flux directly, without coordinate transformations or current loops. The torque is

\[ T_e = \frac{3P}{4}\cdot\frac{L_m}{\sigma L_s L_r}|\psi_s||\psi_r|\sin\delta, \qquad \psi_s = \int(v_s - R_s i_s)\,dt \]

where \(\delta\) is the angle between the stator and rotor flux and \(\sigma = 1 - L_m^2/(L_sL_r)\). Hysteresis controllers on \(|\psi_s|\) and \(T_e\), combined with the flux sector, select an optimal voltage vector from a switching table.

Space-vector hexagon for direct torque control showing six active voltage vectors, two zero vectors, the stator flux vector and the six sectors.
DTC voltage-vector diagram: six active vectors plus two zero vectors. The stator flux position selects the sector, and hysteresis errors choose the vector to apply.
FeatureFOCDTC
Coordinate transformRequired (\(abc \leftrightarrow dq\))Stator frame only
Current controllersYes (PI)No (hysteresis)
Switching frequencyFixed (PWM)Variable
Torque transientFast (~ms)Faster (< ms)
Torque rippleLowHigher
Parameter sensitivityHigh (\(R_r\))Low (\(R_s\) only)
Module 04

Synchronous, PMSM & BLDC Drives

Synchronous Motor — Fundamentals

The per-phase relation is \(\mathbf{V} = \mathbf{E}_f + \mathbf{I}_a(R_a + jX_s)\). The developed power for a cylindrical rotor is

\[ P = \frac{3VE_f}{X_s}\sin\delta \]

and for a salient-pole machine the two-reaction theory adds a reluctance term:

\[ P = \frac{3VE_f}{X_d}\sin\delta + \frac{3V^2}{2}\!\left(\frac{1}{X_q}-\frac{1}{X_d}\right)\sin 2\delta \]

By varying the field current the power factor is controlled: an under-excited machine draws a lagging (inductive) current, unity excitation gives the lowest armature current, and an over-excited machine draws a leading (capacitive) current. Plotting \(I_a\) against \(I_f\) at constant power gives the characteristic V-curves.

V-curves of a synchronous motor: armature current versus field current at light, medium and full load, with the unity power factor locus joining the minima.
Synchronous-motor V-curves at constant power. Each curve has a minimum armature current at unity power factor; lower field gives lagging operation and higher field gives leading operation.

Power-Angle Characteristic and Stability

The torque follows the power, \(T = P/\omega_s\). The salient-pole reluctance term peaks earlier in \(\delta\), giving a higher maximum power than the cylindrical machine. Pull-out occurs where \(dP/d\delta = 0\).

Power versus load angle for cylindrical and salient-pole synchronous machines, marking a stable operating point and the pull-out point.
Power–angle characteristic. The salient-pole curve (with its \(\sin 2\delta\) reluctance term) reaches a higher peak than the cylindrical \(\sin\delta\) curve.
▲ Stability and hunting

Stable operation lies in \(0 \lt \delta \lt \delta_{po}\). A load step or supply dip makes the rotor oscillate (hunting). A damper (amortisseur) winding suppresses these oscillations; in a self-controlled drive the inverter itself provides the damping.

Synchronous Motor Drives — Types

Four drive arrangements are used. A cycloconverter performs direct AC–AC conversion (\(f_o \le f_{in}/3\)) for ball mills and ship propulsion. A VSI/PWM-fed drive converts constant-frequency input to variable-frequency PWM for PMSMs and general drives. A self-controlled (LCI) drive feeds commutating pulses from rotor position, behaving as a "commutatorless DC motor" for large rugged machines. A true synchronous drive uses an independent frequency source and needs a damper, suited to multi-motor textile mills.

In self-controlled mode the over-excited (leading power factor) motor supplies the reactive power needed for inverter commutation, with no hunting or loss of synchronism — making it popular for large salient-pole machines in the megawatt range. Synchronous motors are started by a damper winding (asynchronous start and pull-in), a pony motor, a variable-frequency inverter ramp, or reduced frequency for an LCI.

Load-Commutated Inverter (LCI) Drive

Topology

A line-side phase-controlled rectifier feeds a DC-link reactor; the load side is a six-pulse current-fed thyristor inverter commutated by the back-EMF of the over-excited synchronous motor.

DC link and torque \[ V_{d1} = \frac{3\sqrt2 V_{LL}}{\pi}\cos\alpha_1, \quad V_{d2} = -\frac{3\sqrt2 E_{f,LL}}{\pi}\cos\alpha_2, \quad I_d = \frac{V_{d1}-|V_{d2}|}{R_{link}} \] \[ I_{a,1} = \frac{\sqrt6}{\pi}I_d, \qquad T_e = \frac{3P}{2}\psi_f I_{a,1}\cos\gamma \]

The lead angle \(\gamma\) between the motor current and back-EMF is set to about \(30^\circ\) for safe commutation. The inverter SCRs commutate from the motor EMF only above about 5% speed; below this a pulsed-mode start is used until natural commutation takes over. Rugged thyristors make the LCI the standard for very large pumps, compressors and ID fans up to about 100 MW.

VSI/CSI-Fed Synchronous Motor Drives

A VSI-fed synchronous motor uses sinusoidal PWM, with \(V_{1,LL} = m_a\tfrac{\sqrt3}{2}V_{dc}\) for SPWM or \(V_{1,LL} = m_a V_{dc}/\sqrt2\) for SVPWM (a 15% gain). Scalar V/f suits open-loop operation while FOC is used for high-performance PMSM drives. A CSI-fed machine (auto-sequentially commutated) produces quasi-square current, commutated by capacitors before pickup and then by the motor EMF, with inherent four-quadrant operation. Because there is no slip, the inverter output frequency directly sets the speed: \(n_s = 120f_1/P\).

AspectLCIVSI-PMSM
Power range1–100 MW1 W–5 MW
SwitchesSCRsIGBT / SiC
CommutationMotor EMFForced / PWM
StartingPulsed-modeInherent
Reactive powerMotor over-excitationInverter
Output waveformQuasi-square currentPWM voltage
Torque rippleModerateLow
Cost (\$/kW)LowHigher

PMSM — Permanent Magnet Synchronous Motor

In the rotor \(d\)-\(q\) frame the PMSM voltage and torque equations are

\[ v_d = R_s i_d + L_d\dot i_d - \omega_e L_q i_q, \qquad v_q = R_s i_q + L_q\dot i_q + \omega_e(L_d i_d + \psi_f) \] \[ T_e = \frac{3P}{4}\big[\psi_f i_q + (L_d-L_q)i_d i_q\big] \]

The torque has a magnet (alignment) component and a reluctance component. Two constructions exist: surface PM (SPM), where \(L_d = L_q\), non-salient, with no reluctance torque; and interior PM (IPM), where \(L_d \lt L_q\) and reluctance torque is available.

Cross-section of an eight-pole interior permanent magnet rotor with buried magnets and the d and q axes marked.
Interior permanent-magnet (IPM) rotor cross-section with buried magnets. The saliency \((L_d \lt L_q)\) provides an additional reluctance torque component.

PMSM Control Strategies

StrategyConditionUse case
\(i_d = 0\)SPM, below base speedSimplest; equals MTPA for SPM
MTPA (max torque per amp)IPM, optimum \(i_d \lt 0\)Maximises efficiency
Flux weakeningAbove base speed, \(V_s\) saturatedExtends speed range
MTPV (max torque per volt)Very high speedAvoids current-limit violation
Unity power factorMinimise inverter VARare, for grid-tied systems
MTPA and voltage-limit ellipse (IPM) \[ i_d = \frac{\psi_f}{2(L_q-L_d)} - \sqrt{\frac{\psi_f^2}{4(L_q-L_d)^2}+i_q^2} \] \[ (L_d i_d + \psi_f)^2 + (L_q i_q)^2 \le \left(\frac{V_s}{\omega_e}\right)^{\!2} \]

The voltage-limit ellipse shrinks with speed, driving the operating trajectory toward \(i_d = -\psi_f/L_d\) in deep field weakening.

BLDC Motor — the Rugged Sibling

The BLDC machine differs from the PMSM in its waveforms and control: the back-EMF is trapezoidal (with a \(120^\circ\) flat top), the phase current is rectangular (\(120^\circ\) blocks), commutation is electronic at \(60^\circ\) intervals, and position is sensed by three Hall sensors (or estimated sensorlessly). With two phases conducting at any instant,

\[ T_e = \frac{e_a i_a + e_b i_b + e_c i_c}{\omega_m} = 2K_t I_p \]
Trapezoidal back-EMF and aligned 120-degree rectangular phase current for a BLDC motor over one electrical cycle.
BLDC phase \(a\): trapezoidal back-EMF aligned with \(120^\circ\) rectangular current. Torque is produced during the flat-top conduction windows.
FeatureBLDCPMSM
Back-EMF shapeTrapezoidalSinusoidal
Current shapeRectangular (6-step)Sinusoidal (PWM)
Torque rippleModerate (commutation spikes)Low
Control complexitySimple (6-step)Higher (FOC)
CostLowerHigher
ApplicationHVAC, EV, drones, disk drivesServo, high-end EV, robotics
Module 05

Special Machine Drives

Stepper Motor Drives

Digital motion

Each input pulse advances the rotor by one discrete step, giving open-loop positioning without an encoder.

The step angle is \( \beta = 360^\circ/(N_r\cdot m)\), where \(N_r\) is the number of rotor teeth and \(m\) the number of phases. Three types exist: variable-reluctance (soft-iron rotor, high speed, no detent), permanent-magnet (PM rotor, detent torque, low speed) and hybrid (VR + PM, typically \(\beta = 1.8^\circ\), the most common). Driving modes trade resolution for torque: full-step with one phase on, full-step with two phases on (more torque), half-step (\(\beta/2\)) and microstepping (\(\beta/n\), up to \(n = 256\)). The performance limits are the pull-in rate (maximum starting rate without losing steps), the pull-out rate (maximum running rate) and the holding torque (static torque at rated current).

Stepper Drive Electronics

An \(L\)-\(R\) winding driven by a step voltage rises with time constant \(\tau_e = L/R\):

\[ V = Ri + L\frac{di}{dt} \;\Rightarrow\; i(t) = \frac{V}{R}\left(1 - e^{-t/\tau_e}\right) \]

The step time \(T_s = 1/f_{step}\) must satisfy \(T_s \gtrsim 4\tau_e\), which limits the maximum step rate. Drive techniques extend speed: an L/R drive adds series resistance to raise the voltage (with high losses); a bi-level or chopper drive uses a high voltage for fast current rise with a chopper limiting the current; and a constant-current chopper uses PWM hysteresis tracking. Microstepping feeds two sinusoidal currents \(90^\circ\) apart, \(i_a = I_p\cos(N_r\theta)\) and \(i_b = I_p\sin(N_r\theta)\), giving \(\beta_{micro} = \beta/n\).

Switched Reluctance Motor (SRM)

Pure reluctance

Salient poles on both stator and rotor, with no magnets and no rotor winding. The unidirectional stator current produces torque from the rotor's tendency to align with the excited pole.

Torque comes from the co-energy: \(T_e = \left.\partial W'(i,\theta)/\partial\theta\right|_{i}\), which in the linear region is \(T_e = \tfrac{1}{2}i^2\,dL(\theta)/d\theta\). Each phase is fed by an asymmetric half-bridge with two switches and two diodes.

Asymmetric half-bridge converter for one phase of a switched reluctance motor, with two switches, two diodes and the phase inductance.
Asymmetric half-bridge converter for one SRM phase. Turning both switches on energises the phase; turning them off freewheels the current through the diodes back to the supply.
AdvantagesDrawbacksWhere used
Rugged, no magnets, low costHigh torque rippleEVs (next-gen)
Fault tolerant, high-speedAcoustic noiseAppliances (washers, HVAC)
Simple converter per phaseNeeds position sensingAerospace actuators

The per-phase voltage equation includes a motional back-EMF term:

\[ v = Ri + L(\theta)\frac{di}{dt} + i\,\omega_m\frac{dL}{d\theta}, \qquad e = i\,\omega_m\frac{dL}{d\theta} \]

Two control modes are used. At low speed, chopping limits the current by chopping the bus, controlling duty and turn-on angle. At high speed, single-pulse operation switches on at \(\theta_{on}\) and off at \(\theta_{off}\). The average torque and base speed are

\[ T_{avg} = \frac{m N_r}{2\pi}\oint i^2\,\frac{dL}{d\theta}\,d\theta, \qquad \omega_b \approx \frac{V_{dc}-RI^*}{N_r L_{aligned}I^*} \]

Above \(\omega_b\) the machine enters its constant-power region. Acoustic noise is reduced by profiled current waveforms (torque-sharing functions), randomised PWM and skewed laminations.

Module 06

Motor Sizing, Duty & Thermal Design

Heating and Cooling of Motors

A motor is modelled as a first-order thermal body: the loss power either raises the temperature or is conducted away, \(P_{loss}\,dt = G_h c\,d\theta + A\lambda\,\theta\,dt\). Heating and cooling then follow exponentials:

\[ \theta(t) = \theta_{ss}\left(1 - e^{-t/\tau_h}\right) + \theta_0 e^{-t/\tau_h}, \quad \theta_{ss} = \frac{P_{loss}}{A\lambda}, \quad \tau_h = \frac{G_h c}{A\lambda} \] \[ \text{cooling:}\quad \theta(t) = \theta_1\,e^{-t/\tau_c} \]

The cooling time constant often exceeds the heating one because there is no forced cooling at standstill (\(\tau_c \gt \tau_h\)).

Exponential heating curve rising toward the steady-state temperature followed by a slower cooling curve after the supply is switched off.
First-order thermal response: temperature rises toward \(\theta_{ss}\) with time constant \(\tau_h\), then decays after supply-off with the slower self-cooling constant \(\tau_c\).

Classes of Duty (IEC 60034-1)

Eight standard duty types describe how a motor is loaded over time: S1 continuous (steady-state reached); S2 short-time (stops to cool to ambient); S3 intermittent periodic (cyclic duration factor below 100%); S4 intermittent with heavy starts; S5 intermittent with starting and braking; S6 continuous with intermittent load (never stops); S7 continuous with starting and braking; and S8 continuous with speed changes.

Cyclic duration factor \[ \text{CDF} = \frac{t_N}{t_N + t_R}\times 100\% \]

where \(t_N\) is the load (working) time and \(t_R\) the rest time. Most catalogue ratings assume S1; non-S1 duties permit a higher peak at a reduced cycle, verified by the equivalent-current method.

Motor Rating Selection Methods

For loads that vary over a cycle, an equivalent steady value is computed so the catalogue rating can be chosen as \(I_{rated} \ge I_{eq}\):

\[ I_{eq} = \sqrt{\frac{\sum I_i^2 t_i}{\sum t_i}}, \quad T_{eq} = \sqrt{\frac{\sum T_i^2 t_i}{\sum t_i}}, \quad P_{eq} = \sqrt{\frac{\sum P_i^2 t_i}{\sum t_i}} \]

For short-time duty of length \(t_r\), the allowable overload factor is

\[ K = \frac{P_{st}}{P_{cont}} = \sqrt{\frac{1}{1 - e^{-t_r/\tau_h}}} \]

so a shorter loading time permits a larger overload. For self-cooled motors that stop during idle, the effective idle (cooling) time is reduced by a factor \(\beta \approx 0.5\): \(t_{idle,eff} = \beta\,t_{idle}\).

Module 07

Industrial & Traction Applications

Traction Drives — Physics

The tractive effort balances acceleration, gradient and resistance forces:

\[ F_t = F_a + F_g + F_r = (M+M_e)a + Mg\sin\alpha + rM, \qquad P_t = F_t v \]

where \(M_e\) accounts for rotational inertia and \(r\) lumps rolling and wind resistance. A typical trip has four phases — acceleration, free run, coast and brake — and energy use is quoted as specific energy \(W_{sp}\) in kWh per tonne-kilometre.

Speed versus time curve for a typical traction trip showing acceleration, free run at maximum speed, coasting and braking phases.
Speed–time profile of a traction trip: acceleration to \(v_m\), free run, coasting, then braking to rest.

Electric Vehicle (EV) Drive Architecture

An EV powertrain runs from the battery (48–800 V) through an optional DC/DC boost stage, an inverter (VSI with SVPWM), the traction motor (PMSM or IM), a single-speed gearbox and the wheels. A motor control unit implements FOC/MTPA/field-weakening, a battery management system handles cell balancing and state-of-charge, and regenerative braking returns energy from the wheels to the battery.

Electric vehicle drivetrain block diagram from battery through DC-DC converter, inverter, motor and gearbox to wheels, with motor control unit, battery management system and regenerative braking path.
EV drive architecture: the power path runs battery → DC/DC → inverter → motor → gearbox → wheels, with the motor control unit and BMS supervising and a regenerative-braking path returning energy.
EV motor requirements
  • Wide speed range (4:1 to 6:1)
  • High peak torque for launch
  • High efficiency across the operating map
  • Compact, light and thermally robust
  • Four-quadrant for regenerative braking
Production examples
  • Tesla Model S (rear) — IPM-SRM hybrid
  • Tesla Model 3 (rear) — IPMSM
  • Tesla Model Y (front) — induction
  • Nissan Leaf — PMSM
  • Hyundai Ioniq 5 — PMSM

Wind & Renewable Energy Drives

The doubly-fed induction generator (DFIG) connects its stator directly to the grid and its rotor through a bidirectional (back-to-back) converter, giving variable speed over about \(\pm30\%\) of synchronous speed with a converter rated at only 30% of the nominal power — the standard for 1–5 MW turbines. The direct-drive PMSG is a low-speed, high-torque, multi-pole machine with a full-rated converter and no gearbox (used by Siemens, Enercon and GE). The captured power is

\[ P_{wind} = \tfrac{1}{2}\rho A\,C_p(\lambda,\beta)\,v^3, \qquad \lambda = \frac{\omega R}{v} \]

with \(C_p\) optimal at a tip-speed ratio \(\lambda_{opt} \approx 7\); maximum-power-point tracking drives the pitch and rotor speed to stay there. Grid codes require fault ride-through (LVRT), reactive support (\(\pm0.95\) power factor), frequency response and harmonic compliance.

Industrial Applications — Motor Selection Matrix

ApplicationLoad natureDriveKey feature
Paper millTight tensionVFD-IM + FOCSynchronised speed
Steel rolling millShock, reversing4-Q DC or large CSIHigh overload, fast response
Cement kilnConstant speed, large \(J\)SRIM + slip recoverySoft start, efficient
Cranes & hoists4-Q, overhaulingIM-VFD or DCRegenerative braking
Pumps & fans\(T \propto \omega^2\)VFD-IM (V/f)Energy saving
CompressorConstant torqueVFD-IM or SMStarting current limit
Textile spinningMulti-motor syncTrue synchronousMatched speed
CNC machinePosition loopPMSM servoHigh bandwidth, precision
RoboticsHigh accelerationPMSM / BLDCTorque density
ElevatorsSmooth, positionPMSM gearlessRide quality
Electric vehicleWide range, 4-QPMSM / IM + FOCEfficiency map
Wind turbineVariable speedDFIG or PMSGConverter rating
RailwaysTraction, 4-QIM + VVVFRegen, reliability
Ship propulsionLow-speed, MWCycloconverter SMDirect drive
HVAC\(T \propto \omega^2\)VFD-IM or ECMLarge energy saving
Module 08

Power Quality, Harmonics & Efficiency

Power Quality Issues in Drives

▲ Harmonic sources in drives
  • Line side: a six-pulse rectifier produces harmonics at \(h = 6k \pm 1\) (5th, 7th, 11th, 13th, …)
  • Machine side: inverter voltage and current harmonics cause torque pulsations
  • PWM carrier harmonics
  • Common-mode voltage that drives bearing currents

The key metrics are the current total harmonic distortion and the true power factor:

\[ \text{THD}_I = \frac{\sqrt{\sum_{h\ge2}I_h^2}}{I_1}\times 100\%, \qquad \text{PF} = \underbrace{\frac{I_1}{I_{rms}}}_{\text{distortion}}\cdot\underbrace{\cos\phi_1}_{\text{DPF}} \]

Mitigation uses multi-pulse converters (12, 18 or 24-pulse), an active front-end (PWM rectifier), passive L or LCL filters, active power filters, and phase-shifting transformers. The IEEE 519-2014 limits depend on the short-circuit ratio \(I_{sc}/I_L\): for a low ratio (< 20) the total demand distortion must be \(\le 5\%\), while for a high ratio (> 1000) up to 20% is permitted.

Energy Efficiency in Drives

The system efficiency is the product of the converter, motor and transmission efficiencies, typically \(0.97 \times 0.93 \times 0.97 \approx 87\%\). The biggest savings come from variable-speed operation of fan and pump loads, where the affinity law makes power scale with the cube of speed:

\[ \frac{P_{new}}{P_{rated}} = \left(\frac{\omega_{new}}{\omega_{rated}}\right)^{\!3} \]

so a 20% speed reduction saves about 49% of the power. Motor efficiency classes are defined by IEC 60034-30-1 as IE1 < IE2 < IE3 < IE4 < IE5 (ultra-premium).

Power versus speed for a pump comparing linear throttle control with cubic VFD control, showing the energy saving at reduced speed.
VFD energy saving on a pump: throttling gives roughly linear power-versus-flow, whereas speed control follows the cubic affinity law, saving large amounts of energy at partial load.

Drive and Motor Protection Schemes

FaultProtection & detection
OvercurrentFast fuse plus IGBT desaturation detection (~10 µs)
Short circuitDC-link sensing with gate hardware shutdown
Overload (thermal)\(I^2t\) model in firmware; PTC/NTC in the winding
Over/under voltageDC-bus monitor; brake chopper at over-voltage
Phase loss / unbalanceNegative-sequence monitor
Earth faultResidual-current (\(I_0\)) sensor
Stall / locked rotor\(\omega \lt \omega_{min}\) with \(I \gt I_{rated}\)
Bearing currentsInsulated bearing or shaft-grounding ring

Protection is layered by speed of response: hardware (gate driver, fuse) acts in microseconds, firmware (DSP trip logic) in milliseconds, the application supervisor (drive/PLC) in tens of milliseconds, and plant relays and breakers in hundreds of milliseconds. Modern drives implement Safe Torque Off (STO) per IEC 61800-5-2, removing the inverter gate signals and certified to SIL3/PLe.

Module 09

Dynamic Modelling

State-Space Model — DC Machine

With states \(\mathbf{x} = [i_a,\ \omega_m]^T\) and inputs \(\mathbf{u} = [V_a,\ T_L]^T\), the DC machine is a linear second-order system:

\[ \frac{d}{dt}\begin{bmatrix}i_a\\\omega_m\end{bmatrix} = \begin{bmatrix}-R_a/L_a & -K\phi/L_a\\ K\phi/J & -B/J\end{bmatrix} \begin{bmatrix}i_a\\\omega_m\end{bmatrix} + \begin{bmatrix}1/L_a & 0\\ 0 & -1/J\end{bmatrix} \begin{bmatrix}V_a\\ T_L\end{bmatrix} \]

The transfer functions follow as

\[ \frac{\omega_m(s)}{V_a(s)} = \frac{K\phi}{(sL_a+R_a)(sJ+B)+(K\phi)^2}, \qquad \frac{\omega_m(s)}{T_L(s)} = -\frac{sL_a+R_a}{(sL_a+R_a)(sJ+B)+(K\phi)^2} \]

Induction Motor — d-q Model (Synchronous Frame)

In the synchronously rotating frame the stator and rotor voltage equations are

\[ v_{ds} = R_s i_{ds} + \dot\psi_{ds} - \omega_e\psi_{qs}, \qquad v_{qs} = R_s i_{qs} + \dot\psi_{qs} + \omega_e\psi_{ds} \] \[ 0 = R_r i_{dr} + \dot\psi_{dr} - (\omega_e-\omega_r)\psi_{qr}, \qquad 0 = R_r i_{qr} + \dot\psi_{qr} + (\omega_e-\omega_r)\psi_{dr} \]

with flux linkages \(\psi_{ds} = L_s i_{ds} + L_m i_{dr}\) and \(\psi_{dr} = L_r i_{dr} + L_m i_{ds}\) (the \(q\)-axis is analogous). The electromagnetic torque and mechanical equation close the model:

\[ T_e = \frac{3P}{4}(\psi_{ds}i_{qs} - \psi_{qs}i_{ds}), \qquad J\,\dot\omega_m = T_e - T_L - B\omega_m \]

Park Transformation

The Park transformation maps three-phase quantities to the rotating \(dq0\) frame:

\[ \begin{bmatrix}f_d\\f_q\\f_0\end{bmatrix} = \frac{2}{3}\begin{bmatrix} \cos\theta & \cos(\theta-\tfrac{2\pi}{3}) & \cos(\theta+\tfrac{2\pi}{3}) \\ -\sin\theta & -\sin(\theta-\tfrac{2\pi}{3}) & -\sin(\theta+\tfrac{2\pi}{3}) \\ \tfrac12 & \tfrac12 & \tfrac12 \end{bmatrix}\begin{bmatrix}f_a\\f_b\\f_c\end{bmatrix} \]

with the inverse

\[ \begin{bmatrix}f_a\\f_b\\f_c\end{bmatrix} = \begin{bmatrix} \cos\theta & -\sin\theta & 1\\ \cos(\theta-\tfrac{2\pi}{3}) & -\sin(\theta-\tfrac{2\pi}{3}) & 1\\ \cos(\theta+\tfrac{2\pi}{3}) & -\sin(\theta+\tfrac{2\pi}{3}) & 1 \end{bmatrix}\begin{bmatrix}f_d\\f_q\\f_0\end{bmatrix} \]

The reference-frame choice depends on the application: \(\theta = 0\) gives the stationary \(\alpha\)-\(\beta\) (Clarke) frame; \(\theta = \omega_e t\) gives the synchronous frame (where balanced AC quantities become DC at steady state); and \(\theta = \theta_r\) gives the rotor frame used in PMSM FOC.

Module 10

Advanced Control Techniques

Feedback Devices — Position and Speed Sensors

SensorOutputResolution / accuracyTypical use
Tacho-generatorAnalog DC voltage\(\pm0.1\%\), low bandwidthLegacy DC drives
Incremental encoderA/B/Z TTL pulses256–10000 PPRServo, position tracking
Absolute encoder (SSI/EnDat)Digital word12–26 bit single-turnMulti-turn applications
Resolversin/cos analog~12 bit (RDC)Harsh environment, EV
Hall sensors (3×)Digital, \(60^\circ\)6 sectors / electrical revBLDC commutation
GMR / TMR sensorsAnalog / digital14–16 bitCompact, high-temperature
Optical linear scalePulses or absoluteµm levelCNC, machine tools

Selection is driven by the required resolution and bandwidth, the environment (temperature, dust, oil, vibration), cost and cabling, and whether absolute position is needed at power-up. Resolver-to-digital conversion excites the resolver at 5–10 kHz and demodulates the sin/cos envelopes through a tracking converter — robust to noise, shock and temperature, hence standard for EV traction motors.

Sensorless Control Techniques

Why sensorless?

Removing the encoder or resolver lowers cost, raises reliability, shrinks the package and improves tolerance to harsh environments.

At medium and high speed the rotor position is estimated from the back-EMF: EMF integration (voltage model), flux observers, model-reference adaptive systems (MRAS) and Kalman or Luenberger observers. At zero and low speed, where the back-EMF vanishes, saliency-based methods are used — high-frequency signal injection, the INFORM method and rotating HF carriers.

MRAS sensorless speed estimation block diagram with a voltage-based reference model and a current-based adaptive model, a comparator and a PI adaptation block producing estimated rotor speed.
MRAS structure: a voltage-model reference and a current-model adaptive estimator are compared, and the error drives the estimated speed through a PI block that closes the loop on the adaptive model.

Model Predictive Control (MPC)

Core idea

At each sampling instant, predict the future states under every candidate control action, pick the one that minimises a cost function, apply it, and repeat.

In finite-control-set MPC (FCS-MPC) the cost is evaluated for all seven inverter voltage vectors and the minimum chosen:

\[ g_j = \big\|i_s^*(k+1) - i_s^{p,j}(k+1)\big\|^2 + \lambda\,n_{switch} \] \[ i_s(k+1) = i_s(k) + \frac{T_s}{\sigma L_s}\big[v_s(k) - R_s i_s(k) + \ldots\big] \]

Continuous-control-set MPC (CCS-MPC) instead solves a constrained optimisation over a prediction horizon:

\[ \min_U \sum_{k=0}^{N_p}\|y(k)-y^*(k)\|_Q^2 + \|\Delta u(k)\|_R^2 \quad \text{s.t.}\ \underline{u}\le u(k)\le\bar u,\ \underline{x}\le x(k)\le\bar x \]

solved by quadratic programming at each step (with explicit solutions possible). MPC handles constraints natively, is inherently multivariable and gives a very fast torque response, at the cost of a high computational burden and (for FCS) a variable switching frequency.

Module 11

Worked Numerical Examples

The following fully solved problems span the core competencies of the course — DC and AC drive sizing, converter firing-angle selection, induction-motor torque, thermal rating and traction dynamics. Each is worked in the style expected in university examinations and GATE.

Example 1 — DC Motor Speed Control

Problem

A 220 V, 1500 rpm, 10 A separately-excited DC motor has armature resistance \( R_a = 0.5\ \Omega \) and drives a constant-torque load. Find the speed when the applied voltage is reduced to 150 V.

First establish the machine constant from rated data. The rated back-EMF and angular speed are

\[ E_{rated} = 220 - 10(0.5) = 215\ \text{V}, \qquad \omega_{rated} = \frac{2\pi\cdot 1500}{60} = 157.08\ \text{rad/s} \] \[ K\phi = \frac{215}{157.08} = 1.369\ \text{V}\cdot\text{s/rad} \]

Because the load is constant-torque, the armature current stays at 10 A. At \( V = 150 \) V,

\[ E_{new} = 150 - 10(0.5) = 145\ \text{V}, \qquad \omega_m = \frac{145}{1.369} = 105.9\ \text{rad/s} \]
Answer
\( n = 1011 \) rpm

Armature-voltage control gives a proportional reduction in speed below base speed at constant torque.

Example 2 — Three-Phase Full-Converter Drive

Problem

A 220 V, 1500 rpm, 50 A DC motor with \( R_a = 0.1\ \Omega \) is fed from a three-phase full converter supplied at 415 V, 50 Hz. Find the firing angle \( \alpha \) for (a) rated operation and (b) half speed.

The mean converter output voltage for a three-phase full converter is

\[ V_a = \frac{3\sqrt{2}\,V_{LL}}{\pi}\cos\alpha = 560.4\cos\alpha \]

(a) Rated 1500 rpm, 50 A

\[ E = 220 - 50(0.1) = 215\ \text{V}, \quad V_a = 220\ \text{V} \] \[ \cos\alpha = \frac{220}{560.4} = 0.3925 \;\Rightarrow\; \alpha = 66.9^\circ \]

(b) 750 rpm, 50 A

\[ E = 107.5\ \text{V}, \quad V_a = 107.5 + 5 = 112.5\ \text{V} \] \[ \cos\alpha = 0.2008 \;\Rightarrow\; \alpha = 78.4^\circ \]

Example 3 — Induction-Motor Torque

Problem

A three-phase, 400 V, 50 Hz, 4-pole induction motor has \( R_1 = 1\ \Omega \), \( R_2' = 0.5\ \Omega \) and \( X_1 + X_2' = 4\ \Omega \). Find the slip at maximum torque \( s_{mT} \), the maximum torque \( T_{max} \) and the starting torque \( T_{st} \).

The synchronous speed is \( n_s = 1500 \) rpm so \( \omega_s = 157.08 \) rad/s, and the per-phase voltage is \( V_1 = 400/\sqrt{3} = 230.9 \) V.

\[ s_{mT} = \frac{R_2'}{\sqrt{R_1^2 + (X_1+X_2')^2}} = \frac{0.5}{\sqrt{1+16}} = 0.121 \] \[ T_{max} = \frac{3\,(230.9)^2}{2(157.08)\,(1 + 4.123)} = 99.4\ \text{N}\cdot\text{m} \] \[ T_{st} = \frac{3\,(230.9)^2(0.5)}{157.08\,(2.25 + 16)} = 28.0\ \text{N}\cdot\text{m} \]

The starting-to-maximum ratio is \( T_{st}/T_{max} = 0.28 \), and the full-load torque at \( s = 0.05 \) is approximately 80 N·m.

Example 4 — V/f Control at Reduced Frequency

Problem

Using the motor of Example 3, operate it with constant V/f at 30 Hz. Find the new slip at maximum torque and the new maximum torque.

Scaling voltage and reactance with frequency:

\[ V_{1,new} = 230.9\times\frac{30}{50} = 138.5\ \text{V}, \qquad \omega_{s,new} = 94.25\ \text{rad/s} \] \[ X_{total} = 4\times\frac{30}{50} = 2.4\ \Omega \]

New slip at maximum torque

\[ s_{mT} = \frac{0.5}{\sqrt{1+5.76}} = 0.192 \]

The slip rises — beneficial for starting.

New maximum torque

\[ T_{max} = \frac{3\,(138.5)^2}{2(94.25)\,(1+\sqrt{6.76})} = \frac{57577}{678.7} = 84.9\ \text{N}\cdot\text{m} \]
Low-frequency derating

\( T_{max} \) drops about 15% because the stator-resistance drop becomes significant relative to the reduced applied voltage. The remedy is voltage boost, \( V_1 = V_{boost} + kf \), to compensate at low frequency.

Example 5 — Motor Rating for Intermittent Load

Problem

A constant-speed load follows the duty cycle: 100 N·m for 10 s, 50 N·m for 20 s, 25 N·m for 30 s, then idle for 40 s. Determine the equivalent continuous motor rating.

Using the equivalent-torque (RMS) method:

\[ T_{eq} = \sqrt{\frac{\sum T_i^2\,t_i}{\sum t_i}} = \sqrt{\frac{100^2(10)+50^2(20)+25^2(30)+0}{100}} = \sqrt{1687.5} = 41.1\ \text{N}\cdot\text{m} \]

A standard 50 N·m continuous motor (the next catalogue size) is selected. The peak demand of 100 N·m is twice rated torque, well within the 2–2.5× short-term capability of a typical machine.

With idle-cooling factor \( \beta = 0.5 \)

\[ T_{eq}' = \sqrt{\frac{168750}{60 + 0.5\cdot 40}} = \sqrt{2109} = 45.9\ \text{N}\cdot\text{m} \]

Reduced cooling while idling slightly increases the required rating.

Example 6 — Thermal Overload

Problem

A motor has heating time constant \( \tau_h = 60 \) min and rated steady-state temperature rise \( \theta_{ss} = 60\,^\circ\text{C} \). Find (a) the temperature rise 30 min after a cold start, (b) the time to reach 50 °C, and (c) the permissible 30-min overload from cold.

(a) Heating after 30 min

\[ \theta(30) = 60\,(1 - e^{-30/60}) = 23.6\,^\circ\text{C} \]

(b) Time to reach 50 °C

\[ 50 = 60\,(1 - e^{-t/60}) \;\Rightarrow\; e^{-t/60} = \tfrac{1}{6} \] \[ t = 60\ln 6 = 107.5\ \text{min} \]

(c) 30-min overload from cold

\[ \theta_{ss,OL} = \frac{60}{1 - e^{-0.5}} = \frac{60}{0.3935} = 152.5\,^\circ\text{C} \] \[ \frac{P_{OL}}{P_{rated}} = 2.54, \qquad K = \sqrt{2.54} = 1.60 \]

The motor can carry 1.6× rated current for 30 min when starting from cold.

Example 7 — Chopper-Fed DC Drive

Problem

A chopper-fed DC drive has \( V_s = 230 \) V, \( R_a = 0.2\ \Omega \), \( K\phi = 0.08 \) V·s/rpm, and is rated 1200 rpm at 20 A. Find the duty ratio \( \delta \) at (a) rated speed and (b) 600 rpm.

(a) Rated 1200 rpm, 20 A

\[ E = 0.08(1200) = 96\ \text{V}, \quad V_a = 96 + 4 = 100\ \text{V} \] \[ \delta = \frac{100}{230} = 0.435 \]

(b) 600 rpm, 20 A

\[ E = 48\ \text{V}, \quad V_a = 52\ \text{V} \;\Rightarrow\; \delta = 0.226 \]

The armature current ripple, for \( L_a = 10 \) mH, \( f_c = 1 \) kHz and \( \delta = 0.435 \), is

\[ \Delta I_a \approx \frac{V_s\,\delta(1-\delta)}{f_c L_a} = \frac{230(0.435)(0.565)}{10} = 5.65\ \text{A} \quad (\sim 28\%\ \text{ripple}) \]

Example 8 — Traction Speed–Time Dynamics

Problem

A 200-tonne train coasts on level track with rolling resistance \( r = 0.05 \) kN/tonne. Find the deceleration when the motors are switched off, and compare with coasting on a 1% down-gradient.

Level track

\[ F_r = 0.05\ \text{kN/t}\times 200\ \text{t} = 10\ \text{kN} \] \[ M_e = 1.08\times 200{,}000 = 216{,}000\ \text{kg} \] \[ a = -\frac{F_r}{M_e} = -\frac{10{,}000}{216{,}000} = -0.046\ \text{m/s}^2 \]

The 8% allowance accounts for the rotational inertia of wheels and motors.

1% down-gradient

\[ F_g \approx -200{,}000\times 9.81\times 0.01 = -19.6\ \text{kN} \] \[ a = \frac{F_g - F_r}{M_e} = \frac{-19.6 + 10}{216}\ \text{kN/t} = -0.044\ \text{m/s}^2 \]

Almost identical: gravity nearly offsets the rolling loss. On a steeper gradient the train would accelerate while coasting.

Module 12

Modern Trends and Emerging Technologies

Wide-Bandgap Devices: SiC and GaN

Silicon power devices are approaching their physical limits. Wide-bandgap (WBG) semiconductors — silicon carbide (SiC) and gallium nitride (GaN) — break through those limits with higher blocking voltage (up to 10 kV for SiC), switching frequencies in the hundreds of kilohertz, operation above 200 °C, roughly half the switching loss of silicon, and consequently much smaller passive components.

Comparison of key material properties for silicon, silicon carbide and gallium nitride power devices.
Parameter Si SiC GaN
Bandgap (eV)1.123.263.39
Breakdown field \(E_{br}\) (MV/cm)0.32.23.3
Saturation velocity (107 cm/s)1.02.02.5
Thermal conductivity (W/cm·K)1.54.91.3
Maximum switching frequency< 50 kHz100s of kHzMHz

WBG devices are already standard in EV traction inverters (Tesla, Lucid), wind and solar inverters, high-frequency DC–DC converters, and aerospace and rail systems.

Design challenges
  • Very fast \( dv/dt \) drives bearing currents and EMI
  • Gate-driver design becomes more demanding
  • PCB layout is critical — parasitic inductance must be minimised
  • Device cost is still higher than silicon

Emerging Topics in Electric Drives

Several research and product directions are reshaping the field:

Integrated drives

Motor and inverter share one housing, cutting cost, size, wiring and EMI.

Multilevel inverters

NPC, flying-capacitor, cascaded H-bridge and MMC topologies deliver low THD at medium voltage.

AI in control

Neural-network observers and reinforcement learning adapt to nonlinearity and faults.

Digital twin

A real-time virtual replica of the drive enables predictive maintenance.

Axial-flux motors

Pancake geometry gives high torque density in a short stack — ideal for EVs and drones.

Hairpin windings

Rectangular conductors raise the slot fill factor, improving efficiency and thermal behaviour.

Wireless charging

Resonant inductive power transfer enables cable-free charging for EVs and mobile robots.

Electric aviation

eVTOL and regional aircraft demand very high power density for zero-emission flight.

Smart Drives and Industry 4.0

Connected drives now embed intelligence and communication far beyond simple speed regulation:

Connected-drive features
  • Edge analytics on board the drive — FFT of stator currents and vibration spectra
  • Industrial protocols: EtherCAT, PROFINET, EtherNet/IP, OPC-UA
  • Cloud telemetry for fleet-wide KPIs and remote firmware updates
  • Cybersecurity: IEC 62443, signed firmware and role-based access

Motor Current Signature Analysis (MCSA) is a powerful predictive-maintenance tool: a broken rotor bar produces sidebands around the line frequency in the current spectrum at

\[ f_{br} = (1 \pm 2ks)\,f_1, \qquad k = 1, 2, \ldots \]
Faults diagnosable from drive data
  • Bearing wear: vibration and stator-current sidebands at \( f_1 \pm k f_{bearing} \)
  • Stator inter-turn shorts: negative-sequence current
  • Rotor unbalance / eccentricity: 1× and 2× rotational harmonics
  • Insulation degradation: leakage-current trending
Module 13

Course Synthesis and References

Mental Map of the Subject

The entire course radiates from a single object — the electric drive — through six branches: drive dynamics and stability, DC drives (rectifier- and chopper-fed), induction-motor drives (V/f, FOC and DTC), synchronous and permanent-magnet drives (LCI, cycloconverter, PMSM and BLDC), advanced control (sensorless estimation and model-predictive control), and applications (electric vehicles, rail, industry and wind).

Radial mind map centred on the electric drive, branching to dynamics, DC drives, induction-motor drives, synchronous and PMSM drives, control techniques, and applications, with sub-topics on each branch.
Concept map of the electric-drives course: a central drive node connects to six major themes, each expanding into its principal sub-topics, summarising the dependencies students should carry into examinations.

Key Formulas — Quick Reference Card

Drive Dynamics

\[ T_m - T_L = J\dot\omega_m, \qquad J_{eq} = \sum_i J_i a_i^2, \qquad \tau_m = \frac{J R_a}{(K\phi)^2} \]

DC Motor

\[ V = E + I_a R_a, \qquad E = K\phi\,\omega_m, \qquad T = K\phi\,I_a, \qquad \omega_m = \frac{V - I_a R_a}{K\phi} \]

Converters

\[ 1\phi\ \text{full}: V_a = \frac{2V_m}{\pi}\cos\alpha, \qquad 1\phi\ \text{semi}: V_a = \frac{V_m}{\pi}(1 + \cos\alpha) \] \[ 3\phi\ \text{full}: V_a = \frac{3\sqrt{2}\,V_{LL}}{\pi}\cos\alpha \] \[ \text{Class A}: V_a = \delta V_s, \qquad \text{Class E}: V_a = (2\delta - 1)V_s, \qquad \Delta I_a \approx \frac{V_s\,\delta(1-\delta)}{f_c L_a} \]

Induction Motor

\[ n_s = \frac{120 f}{P}, \qquad s = \frac{n_s - n}{n_s} \] \[ T = \frac{3\,V_1^2 (R_2'/s)}{\omega_s\big[(R_1 + R_2'/s)^2 + (X_1 + X_2')^2\big]} \] \[ s_{mT} = \frac{R_2'}{\sqrt{R_1^2 + (X_1+X_2')^2}}, \qquad P_{ag} = T\omega_s, \qquad P_{mech} = (1-s)P_{ag} \]

Synchronous Motor

\[ P = \frac{3 V E_f}{X_s}\sin\delta, \qquad n_s = \frac{120 f}{P} \]

Field-Oriented Control and PMSM

\[ T_e^{\text{IM}} = \frac{3P}{4}\frac{L_m}{L_r}\,\psi_r\, i_{qs}, \qquad \omega_{sl} = \frac{i_{qs}}{\tau_r\, i_{ds}} \] \[ T_e^{\text{PMSM}} = \frac{3P}{4}\big[\psi_f i_q + (L_d - L_q)\,i_d i_q\big] \]

Thermal and Rating

\[ \theta(t) = \theta_{ss}\big(1 - e^{-t/\tau_h}\big), \qquad \tau_h = \frac{G_h c}{A\lambda}, \qquad I_{eq} = \sqrt{\frac{\sum I_i^2 t_i}{\sum t_i}} \]

Traction and Wind

\[ F_t = (M + M_e)\,a + Mg\sin\alpha + rM \] \[ P = \tfrac{1}{2}\rho A\,C_p(\lambda,\beta)\,v^3, \qquad \lambda = \frac{\omega R}{v} \]

Park Transform (field angle)

\[ \theta_e = \int (\omega_r + \omega_{sl})\,dt \]

References and Further Reading

Foundational Textbooks

  1. G. K. Dubey, Fundamentals of Electrical Drives, 2nd ed., Narosa, 2001.
  2. G. K. Dubey, Power Semiconductor Controlled Drives, Prentice-Hall, 1989.
  3. R. Krishnan, Electric Motor Drives: Modeling, Analysis, and Control, Prentice-Hall, 2001.
  4. R. Krishnan, Permanent Magnet Synchronous and Brushless DC Motor Drives, CRC Press, 2009.
  5. R. Krishnan, Switched Reluctance Motor Drives, CRC Press, 2001.

Complementary Texts

  1. B. K. Bose, Modern Power Electronics and AC Drives, Prentice-Hall, 2002.
  2. W. Leonhard, Control of Electrical Drives, 3rd ed., Springer, 2001.
  3. N. Mohan, Electric Machines and Drives: A First Course, Wiley, 2012.
  4. P. C. Sen, Thyristor DC Drives, Wiley, 1981.
  5. J. M. D. Murphy and F. G. Turnbull, Power Electronic Control of AC Motors, Pergamon, 1988.

Standards

  • IEEE 519-2014 — harmonic limits for industrial drives
  • IEC 60034 series — rotating electrical machines
  • IEC 61800 series — adjustable-speed electrical power drive systems