UGC NET · Electronic Science · Code 88 · Unit-Wise Notes

Unit 9 — Power Devices, SMPS/UPS & Control Systems: Complete Exam Notes

SCR, DIAC, TRIAC & power transistors · thyristor over-voltage/over-current protection · dv/dt & di/dt · single-pulse & pulse-train gating · AC/DC motor construction & speed control · SMPS · UPS · open- & closed-loop control · block-diagram reduction · transfer functions & signal-flow graphs · Routh–Hurwitz & Nyquist stability · on-off, P, PI, PD & PID controllers.

SYLLABUS: NTA UGC NET (88) LEVEL: Asst. Professor / JRF FORMAT: Theory + Formulas + Revision

§ 9.1SCR: Characteristics & Two-Transistor Model

The Silicon Controlled Rectifier (thyristor) is a four-layer P-N-P-N, three-terminal (Anode, Cathode, Gate) latching switch — the workhorse of high-power control (kV, kA).

V–I characteristic (three regions)

  • Forward blocking (V_AK > 0, gate open): only small leakage until the forward break-over voltage V_BO; J₂ blocks.
  • Forward conduction (latched): after triggering, V_AK drops to ~1–1.5 V, large current flows, device acts as a closed switch; negative-resistance transition between the two.
  • Reverse blocking (V_AK < 0): like a reverse diode until reverse breakdown V_BR (J₁, J₃ block).

Two-transistor (regenerative) model — the key explainer

Split the PNPN into a PNP (Q₁) + NPN (Q₂) with cross-coupled collector–base:

Latch (turn-on) condition $$ I_A = \frac{\alpha_2 I_G + I_{CO}}{1 - (\alpha_1 + \alpha_2)} \quad\Longrightarrow\quad \text{turns ON (regenerative) when } \alpha_1 + \alpha_2 \to 1 $$

Gate current raises α₂ (α rises with current) → loop gain reaches 1 → each transistor drives the other into saturation → latch. Once latched, the gate loses control.

Key currents & turn-off

  • Latching current I_L: minimum anode current to stay on just after triggering (gate still applied); holding current I_H: minimum to remain on (I_L ≈ 2–3 × I_H).
  • Turn-off = commutation (drop I_A below I_H): natural/line commutation (AC reverses each half cycle — phase-controlled rectifiers) or forced commutation (DC circuits: a charged capacitor / LC momentarily reverse-biases or zeros I_A — choppers, inverters). Turn-off time t_q (reverse + gate-recovery) defines slow vs fast (inverter-grade) SCRs.
  • Turn-on methods: gate triggering (normal), plus forward over-voltage, dv/dt, light (LASCR), and temperature (all undesired — see §9.5).
  • Ratings: V_DRM/V_RRM, I_T(avg)/I_T(rms), I²t surge, di/dt & dv/dt limits.
  • GTO (gate turn-off thyristor): a negative gate pulse turns it off — used in traction inverters before IGBTs.
UGC NET focus α₁ + α₂ = 1 latch condition; gate loses control after firing; I_L vs I_H (latching > holding); SCR off only by commutation; on-state drop ~1.5 V; natural vs forced commutation contexts.

§ 9.2DIAC & TRIAC

DIAC (DIode AC switch)

  • Two-terminal, bidirectional three-layer (or 5-layer) device — no gate; conducts in either direction once |V| exceeds the break-over voltage V_BO (~30 V), then exhibits a negative-resistance snap (V drops ~5 V).
  • Symmetrical V–I (breaks over both polarities). Chief use: triggering device for the TRIAC gate — provides a sharp current pulse at a controlled phase angle in dimmer/speed circuits.

TRIAC (TRIode AC switch)

  • Three-terminal (MT1, MT2, Gate), bidirectional thyristor ≡ two SCRs in inverse-parallel sharing one gate → controls both half-cycles of AC directly.
  • Four-quadrant triggering (MT2 ±, gate ±); quadrant I⁺ and III⁻ are most sensitive; quadrant II/III with opposite-polarity gate are weaker — so dv/dt and asymmetry need care.
  • Limitations vs back-to-back SCRs: lower power/voltage, poorer dv/dt immunity and commutation (single device sees the full reversal) → snubber needed; used to ~kW, mains 50/60 Hz.
  • Phase control the standard application: DIAC + RC sets the firing angle α each half cycle → lamp dimmers, fan/universal-motor speed, heater control.
    Phase-controlled output (resistive load, full wave) $$ V_{o(rms)} = V_{rms}\sqrt{\frac{1}{\pi}\left[(\pi - \alpha) + \frac{\sin 2\alpha}{2}\right]} \qquad (\alpha = \text{firing angle}) $$
UGC NET focus DIAC = bidirectional, gateless, triggers the TRIAC; TRIAC = two anti-parallel SCRs, both half-cycles; most-sensitive quadrants I/III; DIAC–RC phase control for dimmers; TRIAC weaknesses vs SCR pair.

§ 9.3Power Transistors: BJT, MOSFET, IGBT

Power switching devices — the comparison the exam wants
PropertyPower BJTPower MOSFETIGBT
Controlcurrent (base)voltage (gate, ~0 power)voltage (gate)
Switching speedmoderate (storage delay)fastest (MHz)fast (tens of kHz)
Conduction droplow V_CE(sat)R_DS(on)·I — rises with V-ratinglow V_CE(sat) (BJT-like)
Voltage / current reachmoderatelow-V, high-fhigh-V, high-I (up to kV/kA)
Temperature coeff.negative (hot-spot/2nd breakdown risk)positive (easy paralleling)positive (newer)
Sweet spotlegacySMPS, low-V high-fmotor drives, inverters, traction
  • Safe Operating Area (SOA): the V–I–time envelope; BJTs suffer second breakdown (current crowding/thermal runaway) → restricted SOA; MOSFETs are largely free of it (positive TC spreads current) — a recurring MCQ.
  • MOSFET = majority-carrier, no storage time, body diode included; gate is capacitive (drive current only to charge C_iss — Miller plateau during switching).
  • IGBT = MOS gate + BJT output (voltage-driven input, conductivity-modulated low-drop output) → combines MOSFET ease of drive with BJT low conduction loss at high voltage; tail current limits f_sw. The dominant device in EV/industrial inverters.
  • SiC MOSFET / GaN HEMT (Unit-1 §1.17) now extend f_sw, voltage and efficiency beyond Si.
UGC NET focus MOSFET voltage-driven/fastest/positive-TC/no-second-breakdown; BJT second breakdown; IGBT = MOS input + BJT output (high-power inverters); paralleling ease of MOSFETs; SOA meaning.

§ 9.4Thyristor Protection: Over-Voltage & Over-Current

Over-voltage protection

  • Sources: switching/commutation transients, lightning, supply spikes; exceeding V_DRM can falsely fire or destroy the device.
  • Remedies: RC snubber across the SCR (limits dv/dt and absorbs transient energy — also §9.5), metal-oxide varistor (MOV) / selenium suppressor / TVS clamping the line, crowbar (an SCR that fires to short the supply into a fuse on over-voltage), and voltage-grading networks for series strings.

Over-current protection

  • Sources: load short, commutation failure, overload. SCRs have low thermal mass → act fast.
  • Remedies: fast-acting (semiconductor) HRC fuses with I²t coordination — the fuse I²t must be less than the SCR's withstand I²t so the fuse clears first; magnetic circuit breakers for slower overloads; current-limiting reactor (series L) caps di/dt and peak fault current; electronic over-current relays gating the trigger off.
  • Series/parallel operation: voltage-equalizing resistors + RC for series strings; current-sharing reactors + matched devices for parallel.
  • Thermal: heat sinks, junction-to-case thermal resistance budget \( T_J = T_A + P\theta_{JA} \); forced-air/liquid cooling for high power.
UGC NET focus RC snubber + MOV + crowbar for over-voltage; semiconductor fuse I²t-coordination (fuse clears before SCR) for over-current; series-L limits di/dt; voltage-grading for series strings; crowbar = SCR shorting into a fuse.

§ 9.5SCR Triggering: dv/dt & di/dt

dv/dt (false turn-on) and its snubber

  • A rapidly rising anode voltage drives capacitive (displacement) current through junction J₂: \( i = C_{J2}\,dv/dt \). If large enough it acts like gate current → unwanted firing without a gate signal — a reliability hazard.
  • Cure: RC snubber across the SCR limits the rate the device sees:
    Snubber action $$ \left.\frac{dv}{dt}\right|_{device} \approx \frac{V}{R_s C_s}\ \text{(initial)};\qquad R_s \text{ limits capacitor discharge current at turn-on} $$
    C_s slows the voltage rise; R_s damps the L-C ringing and limits the C-discharge surge into the SCR when it does fire (R_s also bounds turn-on di/dt from the snubber).

di/dt (turn-on current rate)

  • At turn-on, conduction starts in a small area near the gate and spreads (plasma spreading velocity ~50–100 µm/µs). If anode current rises faster than the conducting region grows → local hot spot → device failure.
  • Cure: series inductor (di/dt reactor / saturable reactor) in the anode line limits \( di/dt = V/L \); interdigitated/amplifying gates speed up area spreading. Manufacturer's di/dt rating must not be exceeded.
Memory hook C for dv/dt, L for di/dt. Snubber capacitor tames voltage rate (false firing); series inductor tames current rate (hot-spot). The snubber R does double duty: damping and limiting the snubber-capacitor discharge.
UGC NET focus dv/dt → capacitive false turn-on → RC snubber; di/dt → localized heating → series L; i = C·dv/dt mechanism; why R_s is needed (discharge/damping); the C-vs-L memory hook is a classic MCQ.

§ 9.6Gate Triggering: Single Pulse & Train of Pulses

  • Gate requirements: the gate pulse must exceed I_GT/V_GT, stay within the safe gate-power locus, and persist until anode current exceeds the latching current I_L — otherwise the SCR fails to stay on. Steep-front pulses reduce turn-on di/dt stress and spread; pulse amplitude ≥ a few × I_GT for reliability.
  • Triggering circuits: RC phase-shift (simple, lossy), UJT relaxation oscillator (the classic — intrinsic standoff ratio η ≈ 0.5–0.8; \( f = 1/[RC\ln(1/(1-\eta))] \); fires near V_P = ηV_BB + V_D), PUT, ramp-comparator, and isolated pulse-transformer / optocoupler gate drives.

Single pulse vs train of pulses (the named comparison)

Single-pulse vs pulse-train gating
Single (continuous) pulseTrain of pulses (carrier/high-frequency)
Formone wide gate pulse per cycleburst of narrow pulses (1–10 kHz) over the desired conduction window
Gate dissipationhigher (long pulse)lower (short pulses, low average)
Pulse-transformer sizelarge (avoids core saturation on long pulse)small (short pulses don't saturate the core)
Inductive / discontinuous loadmay fail to latch if I_A rises slowly past I_L within the pulsere-fires repeatedly → reliable latching as current builds
Useresistive loads, simple drivesinductive loads, TRIACs, isolated drives — the preferred method
  • Why a train wins for inductive loads: with a lagging current the anode current may not reach I_L during a single short pulse — repeated pulses keep re-attempting the latch until conduction is established; also eases pulse-transformer design and gate heating.
UGC NET focus Gate pulse must last until I_A > I_L; UJT relaxation oscillator + intrinsic standoff ratio η; pulse-train advantages (low gate dissipation, small pulse transformer, reliable latch on inductive loads); pulse-transformer isolation.

§ 9.7DC Motors: Construction & Speed Control

Construction & basics

  • Stator field (poles/permanent magnet) + rotor armature + commutator + brushes (mechanical inverter keeping torque unidirectional). Back-EMF \( E_b = k\phi N \); torque \( T = k\phi I_a \); terminal \( V = E_b + I_aR_a \).
  • Types: shunt (≈ constant speed), series (high starting torque, speed ∝ 1/load — traction, starters), compound; separately excited (precise control).
Speed equation — the control map $$ N = \frac{V - I_aR_a}{k\phi} \;\Rightarrow\; \text{three knobs: } V,\ R_a\ (\text{added}),\ \phi $$
  • Armature-voltage control (V): speed ∝ V below base speed, constant torque — the modern method via a controlled rectifier (phase-controlled SCR bridge) for AC supply or a DC chopper (PWM, duty D → V_o = D·V_in) for DC supply. Smooth, efficient.
  • Field (flux) control (φ): weaken field → speed above base, constant power region; limited range, simple/cheap.
  • Armature-resistance control (R_a added): reduces speed but wastes power in the resistor (poor efficiency) — legacy.
  • Four-quadrant operation, regenerative braking (return energy to supply) with reversible converters.
  • BLDC (electronic commutation, no brushes — reliability, efficiency) increasingly replaces brushed DC.
UGC NET focus N = (V − I_aR_a)/kφ and the three control knobs; armature control = below base (constant torque), field weakening = above base (constant power); chopper V_o = D·V_in; series motor high starting torque; why R_a control is inefficient.

§ 9.8AC Motors: Construction & Speed Control

Synchronous speed & slip $$ N_s = \frac{120f}{P}\ \text{rpm}; \qquad \text{slip } s = \frac{N_s - N}{N_s}; \qquad N = N_s(1 - s) $$

Induction motor (the industrial workhorse)

  • Three-phase stator → rotating field; squirrel-cage rotor (rugged, cheap) or wound rotor (slip-ring); rotor runs at slip (2–5% full load) — induction, asynchronous. Single-phase versions need a starting auxiliary (capacitor-start, split-phase, shaded-pole).
  • Speed-control methods:
    • V/f control (VFD — the dominant method): vary frequency f (changes N_s) while keeping V/f constant to hold flux → wide smooth range, constant torque; realized by a rectifier → DC link → IGBT PWM inverter (power-electronics tie-in).
    • Pole-changing (discrete speeds), stator-voltage control (fans), rotor-resistance control (wound rotor — like DC R_a, lossy), slip-recovery (Scherbius) schemes.

Synchronous motor

  • Runs exactly at N_s (zero slip); needs DC field + starting means; power-factor correction by over-excitation (synchronous condenser); constant-speed drives.

Universal (series AC/DC) motor: high speed, light tools/appliances — TRIAC phase-controlled (§9.2). Stepper/servo for precise positioning (Unit-6 §6.17).

UGC NET focus N_s = 120f/P and slip s = (N_s−N)/N_s numericals; V/f (VFD) constant-flux frequency control = the modern AC method; squirrel-cage ruggedness; synchronous motor zero slip + PF correction; rectifier-DClink-PWM inverter chain.

§ 9.9Switched-Mode Power Supply (SMPS)

An SMPS regulates by switching the pass device fully ON/OFF at high frequency (tens of kHz–MHz) and filtering, instead of dissipating the difference in a linear pass transistor. The switch is in saturation or cutoff → low loss → 70–95% efficiency, small high-frequency magnetics, light weight.

Non-isolated DC–DC converters (duty cycle D = t_on/T, CCM)
TopologyOutputRelation
Buck (step-down)V_o < V_in\( V_o = D\,V_{in} \)
Boost (step-up)V_o > V_in\( V_o = \dfrac{V_{in}}{1 - D} \)
Buck–Boost (inverting)either, inverted\( V_o = -\dfrac{D}{1 - D}V_{in} \)
Ćukinverting, low ripplesame ratio as buck–boost, capacitor energy transfer
  • Isolated (transformer) topologies: flyback (cheap, < ~150 W — stores energy in the transformer gap, chargers/adapters), forward (single-switch, mid-power), push–pull / half-bridge / full-bridge (high power, better core utilization). Transformer gives isolation + multiple/turns-ratio outputs.
  • Regulation loop: output sampled → error amp vs reference → PWM comparator vs sawtooth → adjusts duty cycle (voltage-mode) or peak current (current-mode); optocoupler crosses the isolation barrier.
  • Building blocks: switch (MOSFET/IGBT), fast diode (Schottky/synchronous rectifier), inductor (energy storage), output capacitor (ripple), high-f transformer. Higher f_sw → smaller L, C, transformer but more switching loss/EMI; soft-switching (ZVS/ZCS resonant) reduces both.
SMPS vs linear regulator — the certain comparison
LinearSMPS
Efficiencylow (≈ V_o/V_in, 30–50%)high (70–95%)
Heat / size / weightlarge heatsink, heavy (50 Hz transformer)small, light
Noise / ripplevery low, cleanswitching noise / EMI (needs filtering)
Step-up?no (only step-down)yes (boost/buck-boost)
Complexity / costsimple, cheapcomplex control
UGC NET focus Buck V_o = DV_in, boost V_in/(1−D), buck-boost −D/(1−D) numericals; SMPS efficiency & size advantages; flyback = isolated low-power; PWM duty-cycle regulation; switch in cutoff/saturation = low loss; EMI as the downside.

§ 9.10Uninterruptible Power Supply (UPS)

A UPS supplies the load through a stored-energy path (battery + inverter) so power is maintained during mains failure, sag, or surge. Core chain: rectifier/charger → batteryinverter → load, with a transfer/static switch and bypass.

UPS topologies — the discriminating table
TypeNormal-mode pathTransfer timeTraits / use
Offline / standbymains directly to load; inverter idle, battery chargingfinite (~2–10 ms)cheapest; home PCs; no conditioning
Line-interactivemains via an autotransformer/AVR (buck–boost taps); inverter bidirectionalshortvoltage regulation without battery use; SOHO/servers
Online / double-conversionalways rectifier→battery→inverter (AC→DC→AC) — load never sees raw mainszero (no break)best conditioning & isolation; data centres, medical, critical loads; lower efficiency, costlier
  • Online UPS rationale: continuous conversion regenerates a clean sine independent of input quality → zero transfer time, full conditioning; static bypass handles overload/fault.
  • Battery: VRLA/Li-ion; backup time = (battery Wh × efficiency)/load W; sized for ride-through to generator start or graceful shutdown.
  • Inverter output quality: pure sine (sensitive/PFC loads) vs modified/stepped sine (cheap, basic loads).
  • Specs: VA/W rating (power factor!), runtime, efficiency, THD, transfer time; contrast with a standby generator (long outages, slow start) — often paired.
UGC NET focus Online (double-conversion, zero transfer, best quality) vs offline (standby, finite transfer, cheap) vs line-interactive (AVR); rectifier→battery→inverter chain; backup-time computation; pure vs modified sine; static-switch role.

§ 9.11Open-Loop & Closed-Loop Control Systems

Open-loop vs closed-loop
Open-loopClosed-loop (feedback)
Feedbacknone — output not measuredoutput sensed & compared to reference
Accuracydepends on calibration; driftsself-correcting (error-driven)
Disturbance rejectionpoorgood
Stabilityinherently stable (if components are)can become unstable (the price of feedback)
Cost / complexitylowhigher (sensors, controller)
Examplewashing-machine timer, toaster, traffic-light timerthermostat, cruise control, servo, voltage regulator
Closed-loop (negative-feedback) transfer function $$ \frac{C(s)}{R(s)} = \frac{G(s)}{1 + G(s)H(s)} \qquad (\text{unity feedback: } H = 1) $$
  • Loop gain GH; characteristic equation 1 + GH = 0 (its roots = closed-loop poles → stability, §9.14–9.15).
  • Sensitivity: feedback reduces sensitivity to plant variation by 1/(1+GH); also reshapes bandwidth, disturbance and noise response (the §4.9/§3.x feedback story applied to systems).
  • Time-domain specs (second-order, Unit-3 §3.10): rise time, peak overshoot \( M_p = e^{-\pi\zeta/\sqrt{1-\zeta^2}} \), settling \( t_s = 4/\zeta\omega_n \), damping ζ, natural frequency ω_n.
  • Steady-state error & system type (number of s in the denominator = number of integrators):
    Static error constants $$ K_p = \lim_{s\to0}GH,\ \ K_v = \lim_{s\to0}sGH,\ \ K_a = \lim_{s\to0}s^2GH; \quad e_{ss}(\text{step}) = \frac{1}{1+K_p},\ e_{ss}(\text{ramp}) = \frac{1}{K_v} $$
    Type-0 → finite step error; Type-1 → zero step error, finite ramp error; Type-2 → tracks ramps with zero error. Adding an integrator (PI, §9.16) raises the type → kills steady-state error.
UGC NET focus C/R = G/(1+GH); 1 + GH = 0 = characteristic equation; system-type ↔ steady-state-error table (Type-1 zero step error); e_ss = 1/(1+K_p) and 1/K_v; open vs closed property matching; feedback trades stability for accuracy.

§ 9.12Block-Diagram Reduction

Reduction rules
ConfigurationEquivalent
Cascade (series)G₁·G₂
Parallel (summing)G₁ ± G₂
Negative feedback loopG/(1 + GH)
Positive feedback loopG/(1 − GH)
Move summing point past a blockinsert 1/G on the moved input
Move take-off point past a blockinsert G on the moved branch
Move take-off before a blockinsert 1/G
  • Strategy: combine innermost cascades/parallels first, collapse inner feedback loops, then relocate summing/take-off points to untangle interlocking loops, repeat until a single block C/R remains.
  • The relocation rules keep the signal mathematically unchanged — the inserted 1/G or G compensates the moved block.
  • For multi-input systems (reference + disturbance), use superposition: find C/R with disturbance = 0 and C/D with reference = 0, then add.
UGC NET focus Series/parallel/feedback collapses; the 1/G–G compensation when moving summing vs take-off points; superposition for reference + disturbance; reduce a given diagram to C/R (a guaranteed full-solve question).

§ 9.13Transfer Function & Signal-Flow Graphs

  • Transfer function T(s) = C(s)/R(s) at zero initial conditions = ℒ{output}/ℒ{input}; poles = roots of the characteristic polynomial (denominator), zeros = numerator roots (Unit-3 §3.11). Defined only for LTI systems; impulse response = ℒ⁻¹{T(s)}.
  • Signal-flow graph (SFG): nodes = variables, directed branches = gains; an algebraic, no-relocation alternative to block diagrams. Vocabulary: forward path, loop, non-touching loops, path gain, loop gain.
Mason's gain formula — the SFG payoff $$ T = \frac{\sum_k P_k\Delta_k}{\Delta}, \quad \Delta = 1 - \sum L_i + \sum L_iL_j - \sum L_iL_jL_k + \cdots $$
  • Δ (graph determinant) = 1 − (sum of all loop gains) + (sum of products of two non-touching loops) − (products of three non-touching loops) + …
  • P_k = gain of the k-th forward path; Δ_k = Δ evaluated with all loops touching P_k removed.
  • One formula gives C/R directly — no successive reduction; the reason SFGs are exam favourites for complex multi-loop systems.
UGC NET focus Apply Mason's formula to a given SFG (compute Δ, identify non-touching loops, forward paths and their Δ_k); convert a block diagram ↔ SFG; T from a single-loop graph = P/(1−L).

§ 9.14Routh–Hurwitz Stability Criterion

Stability definition A linear system is (BIBO/absolutely) stable ⟺ all roots of the characteristic equation 1 + GH = 0 lie in the left half of the s-plane. Routh–Hurwitz tests this without solving for the roots.

Procedure

  1. Necessary condition: all coefficients of the characteristic polynomial \( a_ns^n + \cdots + a_0 \) present and of the same sign (a missing or sign-changed coefficient ⇒ unstable immediately).
  2. Build the Routh array (sⁿ, sⁿ⁻¹ rows from coefficients; lower rows from 2×2 determinants).
  3. Stability ⟺ no sign change in the first column; the number of first-column sign changes = number of RHP roots.
  • Special cases:
    • Zero in the first column (rest of row nonzero): replace with ε → 0⁺ and continue.
    • Entire row of zeros: symmetric roots (on jω axis / RHP–LHP pairs) — form the auxiliary equation from the row above, differentiate, and use its coefficients; the auxiliary roots reveal jω-axis (marginal) crossings.
  • Marginal stability: a row of zeros with auxiliary roots purely on the jω axis → sustained oscillation at \( \omega = \sqrt{\text{auxiliary root}} \).
  • Design use: find the range of a gain K for stability (the classic numerical) — express the first-column entries in K and require all > 0; the boundary value gives the critical gain and oscillation frequency.
UGC NET focus Construct the array and read first-column sign changes = RHP roots; find the K-range for stability and the critical K / oscillation frequency from the auxiliary equation; necessary-coefficient condition; ε-method and row-of-zeros handling.

§ 9.15Nyquist Plot & Stability

A frequency-domain stability test using the open-loop G(jω)H(jω) to judge the closed-loop — and, unlike Routh, it handles transport delay and reads off relative stability (margins).

Nyquist criterion (encirclement) $$ N = Z - P \quad\Longrightarrow\quad \textbf{stable } (Z = 0) \text{ iff } N = -P $$
  • N = number of clockwise encirclements of the −1 + j0 point by the Nyquist plot of GH (the polar plot for ω: −∞→∞, mapping the closed contour); P = open-loop poles in the RHP; Z = closed-loop poles in the RHP (must be 0 for stability). Encirclements counted counter-clockwise = −N.
  • Open-loop-stable case (P = 0): closed loop stable ⟺ the plot does not encircle −1 — the everyday version.
  • Relative stability — margins (Unit-3 §3.12):
    Gain & phase margins $$ GM = \frac{1}{|GH|}\bigg|_{\angle GH = -180^\circ}\ (\text{dB} = -20\log|GH|); \qquad PM = 180^\circ + \angle GH\big|_{|GH| = 1} $$
    positive GM and PM ⇒ stable; the closer the plot passes to −1, the smaller the margins, the more oscillatory.
  • Relation to Bode (same information, different view): gain-crossover (|GH| = 1) ↔ PM; phase-crossover (∠ = −180°) ↔ GM. Polar-plot crossing of the negative real axis at distance d from origin → GM = 1/d.
UGC NET focus N = Z − P and "no encirclement of −1 when P = 0"; gain/phase-margin definitions and reading them off the plot/Bode; −1 point significance; margins as relative stability; counting RHP open-loop poles P.

§ 9.16On-Off, P, PI, PD & PID Controllers

PID control law $$ u(t) = K_p e(t) + K_i\!\int e\,dt + K_d\frac{de}{dt} \;\Longleftrightarrow\; G_c(s) = K_p\left(1 + \frac{1}{T_is} + T_ds\right) = K_p + \frac{K_i}{s} + K_d s $$
Controller modes — effect of each term
ModeActionEffect on performance
On-Off (bang-bang)output full ON/OFF about a setpoint (with hysteresis/deadband)simplest; continuous oscillation about setpoint (thermostat); no precise hold
Pu ∝ errorfaster, lower rise time; leaves steady-state offset; large K_p → instability
Iu ∝ ∫erroreliminates steady-state error (adds a pole at origin → raises system type); slows response, can add overshoot/instability; integral windup
Du ∝ d(error)/dtanticipatory → improves damping/stability, reduces overshoot & settling; amplifies noise; never used alone
PIP + Izero steady-state error, good for slow processes; sacrifices some speed/stability
PDP + Dimproves transient/stability & speed; keeps an offset (no I)
PIDall threezero offset + good transient — the universal industrial controller
  • Term summary (memory hook): P = present error, I = accumulated past error, D = predicted future error.
  • Tuning — Ziegler–Nichols (the named method): increase K_p until sustained oscillation → record ultimate gain K_u and period T_u → set \( K_p = 0.6K_u,\ T_i = T_u/2,\ T_d = T_u/8 \) (classic PID); or the open-loop reaction-curve (process-reaction) method. Cohen–Coon, IMC as alternatives; modern auto-tuners.
  • Practical refinements: derivative on measurement (not error) to avoid setpoint kick; filtered D; integral anti-windup clamping; setpoint weighting.
  • Realization: op-amp analog PID (integrator + differentiator + summer, Unit-4 §4.12) or digital (difference-equation PID in a microcontroller, Unit-6 — sampled e[n], velocity form).
UGC NET focus Match term ↔ effect: I removes steady-state error (raises type), D improves stability/damping but amplifies noise, P leaves offset; PID law and G_c(s); Ziegler–Nichols K_u/T_u settings; on-off = hysteresis oscillation; P-I-D = present-past-future hook.

§ 9.17Unit-9 Formula Sheet

One-stop reference table — Unit 9
TopicResultNotes
SCR latchα₁ + α₂ → 1gate loses control after firing
SCR currentsI_L > I_H (latching > holding)off by commutation only
TRIAC phase controlV_o(rms) = V_rms√[(1/π)((π−α) + sin2α/2)]full-wave resistive load
dv/dt false turn-oni = C_{J2}·dv/dt → RC snubberC tames dv/dt
di/dt limitdi/dt = V/L → series inductorL tames di/dt
Over-currentfuse I²t < SCR I²tcrowbar for over-voltage
UJT triggerf = 1/[RC ln(1/(1−η))]; V_P = ηV_BB + V_Drelaxation oscillator
DC motor speedN = (V − I_aR_a)/kφV, φ, R_a knobs
ChopperV_o = D·V_inarmature-voltage control
Sync speed / slipN_s = 120f/P; s = (N_s−N)/N_sV/f (VFD) control
BuckV_o = D·V_instep-down
BoostV_o = V_in/(1−D)step-up
Buck–boostV_o = −D·V_in/(1−D)inverting
UPS backupt = (battery Wh × η)/load Wonline = zero transfer
Closed loopC/R = G/(1 + GH)char. eqn 1 + GH = 0
Steady-state errore_ss(step) = 1/(1+K_p); e_ss(ramp) = 1/K_vType-1 → zero step error
Error constantsK_p = limGH; K_v = lim sGH; K_a = lim s²GHs→0
Block reductionseries G₁G₂; feedback G/(1±GH)move point → ×G or ×1/G
MasonT = ΣP_kΔ_k/ΔΔ = 1 − ΣL + ΣL_iL_j − …
Routh–Hurwitzstable ⟺ no first-column sign change#changes = #RHP roots
NyquistN = Z − P; stable iff N = −PP=0: don't encircle −1
MarginsGM at ∠=−180°; PM = 180° + ∠GH at |GH|=1both > 0 ⇒ stable
PIDu = K_p e + K_i∫e + K_d de/dtI removes offset, D adds damping
Ziegler–NicholsK_p = 0.6K_u, T_i = T_u/2, T_d = T_u/8ultimate-gain method
2nd-order specsM_p = e^{−πζ/√(1−ζ²)}; t_s = 4/ζω_nω_d = ω_n√(1−ζ²)

§ 9.18Quick Revision Notes — Unit 9 in 25 Points

Rapid-fire recap (last-day revision)

  1. SCR = 4-layer PNPN latching switch; two-transistor model latches when α₁ + α₂ → 1; gate loses control after firing; on-drop ~1.5 V.
  2. I_L (latching, to stay on at firing) > I_H (holding, to remain on); turn-off only by commutation — natural (AC) or forced (DC, capacitor/LC).
  3. DIAC = two-terminal bidirectional gateless trigger (breaks over both ways) → fires the TRIAC gate.
  4. TRIAC = two anti-parallel SCRs, one gate, controls both AC half-cycles; quadrants I/III most sensitive; DIAC+RC phase control = dimmers/fan speed.
  5. Power MOSFET: voltage-driven, fastest, positive TC (easy paralleling), no second breakdown. BJT: second-breakdown SOA limit. IGBT: MOS input + BJT output → high-V/high-I inverters.
  6. dv/dt → capacitive current i = C·dv/dt → false turn-on → cure with RC snubber (C). di/dt → local hot spot → cure with series L. Memory: C for dv/dt, L for di/dt.
  7. Over-voltage: snubber + MOV + crowbar (SCR shorts into fuse). Over-current: fast semiconductor fuse with I²t < SCR I²t, series reactor limits di/dt.
  8. Gate pulse must persist until I_A > I_L; UJT relaxation oscillator (η standoff ratio) is the classic trigger.
  9. Pulse train beats single pulse: lower gate dissipation, smaller pulse transformer, reliable latching on inductive loads (re-fires until current builds).
  10. DC motor N = (V − I_aR_a)/kφ; armature-V control below base (constant torque, chopper V_o = DV_in), field weakening above base (constant power), R_a control wasteful.
  11. AC: N_s = 120f/P, slip s = (N_s−N)/N_s; V/f (VFD: rectifier→DC link→PWM inverter) is the modern induction-motor method; synchronous motor runs at N_s, corrects PF.
  12. SMPS: switch fully ON/OFF at high f → 70–95% efficient, small/light, but EMI; buck DV_in, boost V_in/(1−D), buck-boost −DV_in/(1−D); flyback = isolated low-power; PWM duty regulates.
  13. SMPS vs linear: efficient/small/step-up-capable/noisy vs simple/clean/heavy/step-down-only.
  14. UPS: online (double-conversion, zero transfer, best quality, costly) > line-interactive (AVR) > offline/standby (cheap, finite transfer); backup = battery Wh·η/load.
  15. Open-loop: no feedback, simple, drifts (toaster/timer). Closed-loop: self-correcting, can go unstable; C/R = G/(1+GH); 1 + GH = 0 = characteristic equation.
  16. System type = # integrators; e_ss(step) = 1/(1+K_p), e_ss(ramp) = 1/K_v; Type-1 → zero step error; adding I raises type → kills offset.
  17. Block reduction: series multiply, parallel add, feedback G/(1±GH); move summing point → insert 1/G, move take-off → insert G; superpose reference + disturbance.
  18. Mason: T = ΣP_kΔ_k/Δ, Δ = 1 − ΣL_i + Σ(non-touching pairs) − …; one-shot solution for multi-loop SFGs.
  19. Routh–Hurwitz: stable ⟺ all characteristic-eqn coefficients same sign AND no first-column sign change; #sign changes = #RHP roots; row of zeros → auxiliary equation (marginal/jω roots).
  20. Use Routh to find the K-range for stability and the critical gain/oscillation frequency.
  21. Nyquist: N = Z − P; stable iff Z = 0; with P = 0, plot must not encircle −1+j0.
  22. Gain margin at ∠GH = −180°, phase margin = 180° + ∠GH at |GH| = 1; both positive ⇒ stable; closer to −1 ⇒ more oscillatory.
  23. PID: u = K_p e + K_i∫e + K_d de/dt; P = present (offset remains), I = past (removes offset, adds lag/windup), D = future (damping, noise-amplifying).
  24. On-off = hysteresis oscillation (thermostat); PI = zero offset slow loops; PD = better transient with offset; PID = best of both (industrial standard).
  25. Ziegler–Nichols ultimate-gain tuning: K_p = 0.6K_u, T_i = T_u/2, T_d = T_u/8; realize PID with op-amps or a microcontroller.

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