Eng-Interview Questions
ISRO · DRDO · BARC · NTPC · BEL
Important 150 top Technical Interview Questions for Electrical and Electronics Engineering—covering Circuits, Machines, Power, Electronics, Control Systems, and much more. These questions will help you prepare for interviews, as well as understand the patterns and difficulty level of interview panels.
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Basic Electrical Circuits & Theory
Q01
Explanation
KCL: The algebraic sum of currents entering any node equals zero — based on conservation of charge.
KVL: The algebraic sum of all voltages around any closed loop equals zero — based on conservation of energy.
KVL: The algebraic sum of all voltages around any closed loop equals zero — based on conservation of energy.
KCL: ΣI_in = ΣI_out | KVL: ΣV = 0 (closed loop)
They hold in AC because at any instant, charge is still conserved and energy is still conserved. At very high frequencies, distributed capacitance between wires can cause apparent violation — this is a lumped-circuit assumption boundary.
Both laws are frequency-independent for lumped circuits; only the lumped model assumption fails at very high frequencies (e.g., GHz range).
Q02
Explanation
With AC: Current flows because capacitor reactance
With DC: After initial transient, capacitor blocks steady-state DC completely. Current drops to zero and the bulb does NOT glow (after brief flash during charging).
Xc = 1/(2πfC) allows current to pass. The bulb glows.With DC: After initial transient, capacitor blocks steady-state DC completely. Current drops to zero and the bulb does NOT glow (after brief flash during charging).
A capacitor is an open circuit for steady-state DC and a short circuit for very high-frequency AC. This is a classic tricky question in PSU interviews.
Q03
Explanation
Peak Value (Vm): Maximum amplitude of the sinusoidal waveform.
RMS Value: The equivalent DC value that delivers the same average power to a resistive load.
We use RMS because it directly represents heating effect — a practical measure for power calculations:
RMS Value: The equivalent DC value that delivers the same average power to a resistive load.
V_rms = V_peak / √2 ≈ 0.707 × V_peak (for sinusoid)
For 230 V AC supply, peak voltage = 230 × √2 ≈ 325 V.We use RMS because it directly represents heating effect — a practical measure for power calculations:
P = V²_rms / R.
All power ratings on electrical equipment use RMS values. India’s standard supply is 230 V RMS at 50 Hz.
Q04
Explanation
No, power factor (PF) cannot exceed 1. PF = cos φ where φ is the phase angle between voltage and current. Since cos φ ranges from −1 to +1, and PF is always taken as a magnitude,
Unity PF (PF = 1): Voltage and current are perfectly in phase. All power drawn is real/active power — no reactive power. This occurs for pure resistive loads.
0 ≤ PF ≤ 1.Unity PF (PF = 1): Voltage and current are perfectly in phase. All power drawn is real/active power — no reactive power. This occurs for pure resistive loads.
PF = cos φ = Active Power (W) / Apparent Power (VA)
Leading PF: capacitive loads. Lagging PF: inductive loads. Unity PF is the ideal operating condition for maximum efficiency.
Q05
Explanation
Any linear network with voltage/current sources and resistors can be replaced by a single Thevenin voltage (Vth) in series with a Thevenin resistance (Rth) at any two terminals.
1. Remove the load. Find open-circuit voltage → V_th.
2. Kill all independent sources (short voltage sources, open current sources).
3. Find resistance looking into terminals → R_th.
4. Draw equivalent: V_th in series with R_th.
V_th = Open-circuit voltage at terminals
R_th = Resistance seen from terminals (all sources killed)
Steps:R_th = Resistance seen from terminals (all sources killed)
1. Remove the load. Find open-circuit voltage → V_th.
2. Kill all independent sources (short voltage sources, open current sources).
3. Find resistance looking into terminals → R_th.
4. Draw equivalent: V_th in series with R_th.
Maximum power transfer occurs when load resistance = R_th. Efficiency at max power = 50%.
Q06
Explanation
Both are rated for the same voltage (230 V). Using
P = V²/R → R = V²/P.
R_100W = 230² / 100 = 529 Ω | R_60W = 230² / 60 = 882 Ω
The 100 W bulb has lower resistance. Lower resistance allows more current to flow at the same voltage, hence more power dissipation and brighter light. The 60 W bulb has higher resistance — restricts current — dissipates less power.
When connected in SERIES (opposite scenario), the 60W bulb glows brighter because the same current flows and P = I²R — the higher resistance dissipates more power.
Q07
Explanation
Resonance occurs when inductive reactance equals capacitive reactance:
• Series RLC: Impedance is minimum (= R), current is maximum, PF = 1.
• Parallel RLC: Impedance is maximum, current is minimum, circuit acts as open for AC source.
• Voltage across L and C can be much larger than supply voltage (voltage magnification).
XL = XC.
f₀ = 1 / (2π√LC) Hz
At resonance:• Series RLC: Impedance is minimum (= R), current is maximum, PF = 1.
• Parallel RLC: Impedance is maximum, current is minimum, circuit acts as open for AC source.
• Voltage across L and C can be much larger than supply voltage (voltage magnification).
Q-factor (Quality factor) = ω₀L/R = ratio of energy stored to energy dissipated. Higher Q → sharper resonance peak → more selective circuit.
Q08
Explanation
For two identical batteries (EMF = E, internal resistance = r) in parallel:
Resultant EMF = E (same as individual)
Resultant r = r/2 (parallel combination)
Why? Parallel connection doesn’t add voltage — it increases current capacity and reduces internal resistance. Each battery shares the load current equally, halving the effective internal resistance.
Resultant r = r/2 (parallel combination)
Parallel batteries are used to extend runtime/current capacity, NOT voltage. Series gives voltage addition but same internal resistance sum.
Q09
Explanation
Impedance (Z): Total opposition to AC current flow. It is the complex ratio of voltage to current phasor.
Z = R + jX [ohms, Ω] | |Z| = √(R² + X²)
Admittance (Y): Reciprocal of impedance. Ease with which AC flows.
Y = 1/Z = G + jB [siemens, S]
G = conductance, B = susceptance. Admittance is more convenient for parallel circuit analysis.
For pure resistance: Z = R, Y = 1/R. For pure inductance: Z = jωL, Y = 1/jωL = −j/ωL.
Q10
Explanation
Skin effect is the tendency of AC current to flow predominantly at the outer surface (skin) of a conductor rather than uniformly through its cross-section, increasing the effective resistance.
At 50 Hz, skin depth in copper ≈ 9.35 mm (not significant for standard wires). At MHz range, skin depth is micrometres — critical for RF cables and hollow conductors (waveguides).
Skin depth δ = √(2ρ / ωμ) metres
As frequency increases → skin depth decreases → current confined to thin surface layer → effective cross-section shrinks → resistance increases.At 50 Hz, skin depth in copper ≈ 9.35 mm (not significant for standard wires). At MHz range, skin depth is micrometres — critical for RF cables and hollow conductors (waveguides).
To combat skin effect in high-frequency applications: stranded/Litz wire, hollow conductors, or silver-plated conductors are used.
Q11
Explanation
In a linear network with multiple independent sources, the total response (voltage or current) equals the algebraic sum of responses due to each source acting alone (others killed).
Cannot be applied when:
• Circuit contains non-linear elements (diodes, transistors in non-linear region).
• For power calculations (P = I²R is non-linear — power is NOT superimposable).
• Circuits with dependent sources (keep dependent sources active while killing independents).
Cannot be applied when:
• Circuit contains non-linear elements (diodes, transistors in non-linear region).
• For power calculations (P = I²R is non-linear — power is NOT superimposable).
• Circuits with dependent sources (keep dependent sources active while killing independents).
Superposition is valid only for linear circuits. For power, calculate total current/voltage first using superposition, THEN compute power.
Q12
Explanation
Ideal Voltage Source: Must maintain constant terminal voltage regardless of load current. If internal resistance existed, voltage would drop (V = E − I·r). So r = 0 ensures V_terminal = E always.
Ideal Current Source: Must deliver constant current regardless of load resistance. For constant I, the source must have infinite impedance — otherwise current would divert internally. R_internal = ∞ forces all current into the external circuit.
Ideal Current Source: Must deliver constant current regardless of load resistance. For constant I, the source must have infinite impedance — otherwise current would divert internally. R_internal = ∞ forces all current into the external circuit.
Real sources have non-zero internal resistance. Norton source = current source || R_internal. Thevenin source = voltage source + R_internal in series.
Q13
Explanation
τ = RC (seconds) | For RL: τ = L/R
Time constant τ is the time required for a capacitor to charge to 63.2% of its final value (or discharge to 36.8%).After 5τ, capacitor is considered fully charged (99.3%). It represents the speed of response of the circuit to a step input.
V(t) = V₀(1 − e^(−t/τ)) for charging. Fast response = small τ = small RC. Used in timing circuits, filters, ADC reference settling.
Q14
Explanation
Reactive Power (Q): Power alternately stored and released by reactive elements (L and C). Measured in VAR (volt-ampere reactive).
Q = V·I·sin φ [VAR]
It does no net useful work — energy oscillates between source and reactive element. However, it is essential for creating magnetic fields in motors, transformers, and maintaining voltage levels in power systems. Without reactive power, inductive loads cannot operate.
Power companies penalise low power factor because reactive current increases line losses (I²R) without contributing to useful power. Capacitor banks are added to compensate reactive power.
Q15
Explanation
Ideal voltage source short-circuited: Infinite current flows (V/0 = ∞). This is physically impossible and destroys real sources. In circuit analysis, we avoid this invalid condition.
Ideal current source open-circuited: Infinite voltage develops across the open terminals (I × ∞ = ∞). Again physically impossible — in reality, arcing or insulation breakdown would occur.
These represent the boundary violations in ideal source models.
Ideal current source open-circuited: Infinite voltage develops across the open terminals (I × ∞ = ∞). Again physically impossible — in reality, arcing or insulation breakdown would occur.
These represent the boundary violations in ideal source models.
Rule: Never short-circuit a voltage source. Never open-circuit a current source. In power electronics, this is why shoot-through protection is critical in inverter legs.
Q16
Explanation
Duality means two circuits have the same mathematical form with variables interchanged. Dual pairs: Voltage↔Current, R↔G (conductance), L↔C, KVL↔KCL, Series↔Parallel, Mesh↔Node analysis.
Series RLC dual ↔ Parallel RLC
V = L(di/dt) dual ↔ I = C(dv/dt)
V = L(di/dt) dual ↔ I = C(dv/dt)
Duality lets you solve one circuit and directly write the solution for its dual — saves analysis effort. Thevenin ↔ Norton are dual representations.
Q17
Explanation
Mutual Inductance (M): When changing current in one coil induces EMF in a neighbouring coil via magnetic flux linkage.
M = k√(L₁·L₂) | k = coefficient of coupling (0 ≤ k ≤ 1)
k = 1: All flux of coil 1 links coil 2 (ideal transformer). k = 0: No coupling. For air-core transformers: k ≈ 0.4–0.9. For iron-core: k ≈ 0.95–0.99.
Mutual inductance is the principle behind transformers, inductive chargers (Qi standard), and RFID systems. Dot convention determines polarity of induced EMF.
Q18
Explanation
Advantages of 3-phase:
• Constant power delivery (no pulsating power as in single-phase).
• 25% less copper needed for same power transmitted (more economical).
• Motors are self-starting with rotating magnetic field — no starting auxiliary needed.
• Higher power density per conductor.
• Neutral wire can be eliminated for balanced loads.
• Constant power delivery (no pulsating power as in single-phase).
• 25% less copper needed for same power transmitted (more economical).
• Motors are self-starting with rotating magnetic field — no starting auxiliary needed.
• Higher power density per conductor.
• Neutral wire can be eliminated for balanced loads.
P₃φ = √3 × VL × IL × cosφ (Watts)
India uses 415 V (line-to-line) / 240 V (line-to-neutral) 3-phase, 50 Hz system for distribution. Transmission is at 11 kV, 33 kV, 66 kV, 132 kV, 220 kV, 400 kV, 765 kV.
Q19
Explanation
Star: VL = √3 × Vph | IL = Iph
Delta: VL = Vph | IL = √3 × Iph
Star (Y): One end of each phase joined at neutral point. 4-wire system possible. Lower voltage per phase — safer insulation requirement. Used for loads requiring neutral (single-phase taps).Delta: VL = Vph | IL = √3 × Iph
Delta (Δ): All three phases form a closed loop. No neutral. Higher phase current — used where high-torque starting required. Common for motors and generators.
Star-Delta starter uses this conversion to reduce starting current of induction motors.
Conversion: R_delta = 3 × R_star (for equivalent impedance). Y-Δ and Δ-Y transformation simplifies complex network analysis.
Q20
Explanation
Faraday’s Law: EMF induced is proportional to rate of change of magnetic flux linkage.
Lenz’s Law Significance: Explains back-EMF in motors, braking effect in eddy current brakes, behaviour of transformers under load, and why inductors resist changes in current.
e = −N × (dΦ/dt) [Volts]
The negative sign embodies Lenz’s Law: the induced EMF always opposes the change in flux that caused it (conservation of energy). If opposing force didn’t exist, energy would be created from nothing.Lenz’s Law Significance: Explains back-EMF in motors, braking effect in eddy current brakes, behaviour of transformers under load, and why inductors resist changes in current.
Lenz’s Law is a consequence of conservation of energy. It is what makes transformers, generators, motors, and inductive sensors possible.
Electrical Machines
Q21
Explanation
A transformer works on mutual electromagnetic induction. AC in primary winding creates alternating flux in the iron core, which links the secondary winding and induces EMF (Faraday’s Law).
V1/V2 = N1/N2 = I2/I1 (ideal transformer)
Why not DC? DC produces constant (non-changing) flux. Since e = −N(dΦ/dt), zero rate of change means zero induced EMF in secondary. Also, a DC source would cause primary to draw excessive current (only resistance limits it — no back-EMF from reactance), potentially burning the primary winding.
Transformer core losses: Hysteresis loss (∝ f × B^1.6) and Eddy current loss (∝ f² × B²). To reduce eddy currents, core is laminated with silicon steel.
Q22
Explanation
Slip s = (Ns − Nr) / Ns × 100%
Ns = 120f/P (synchronous speed) | Nr = rotor speed
Slip = 0: Rotor runs at synchronous speed. No relative motion between rotating field and rotor → no induced EMF → no rotor current → no torque. Impossible at load (theoretical only).Ns = 120f/P (synchronous speed) | Nr = rotor speed
Slip = 1: Rotor is stationary (Nr = 0). Starting condition — maximum rotor current and flux cutting rate. Torque exists but motor hasn’t started yet. High starting current drawn.
Normal operating slip: 2–8% for squirrel-cage induction motors.
Induction motor cannot run at exactly synchronous speed — it always lags. This is why it’s called “asynchronous motor” in international standards.
Q23
Explanation
At start, the stator creates a rapidly rotating magnetic field (at synchronous speed). The rotor (with DC excitation) is stationary. The stator field tries to drag the rotor, but reverses direction 50 times per second — resulting in zero average torque (alternating push-pull cancels). The rotor cannot accelerate fast enough to catch the rotating field.
Starting methods:
1. Damper winding (amortisseur): Short-circuited bars on rotor face act like squirrel cage — provide induction motor starting torque. Motor is started as induction motor then excited and pulled into synchronism.
2. Starting with a variable frequency drive (VFD): Slowly ramp up frequency from 0 Hz to 50 Hz — rotor can follow.
3. Use of a small starting motor (pony motor).
Starting methods:
1. Damper winding (amortisseur): Short-circuited bars on rotor face act like squirrel cage — provide induction motor starting torque. Motor is started as induction motor then excited and pulled into synchronism.
2. Starting with a variable frequency drive (VFD): Slowly ramp up frequency from 0 Hz to 50 Hz — rotor can follow.
3. Use of a small starting motor (pony motor).
Once running at synchronous speed, DC rotor field locks into stator field and motor runs at exactly Ns. Synchronous motors are used for power factor correction (synchronous condensers).
Q24
Explanation
Core-Type: Windings surround the core. Core is like a hollow rectangle. Windings on two limbs. Better cooling (windings exposed), easier insulation, used for high-voltage applications.
Shell-Type: Core surrounds the windings. Figure-8 cross-section. Both primary and secondary on central limb — good leakage flux minimisation. Better mechanical support for windings — used for high-current, low-voltage applications and audio transformers.
Shell-Type: Core surrounds the windings. Figure-8 cross-section. Both primary and secondary on central limb — good leakage flux minimisation. Better mechanical support for windings — used for high-current, low-voltage applications and audio transformers.
Power transmission transformers are usually core-type. Distribution transformers at substations can be shell-type. Shell-type has better leakage flux containment.
Q25
Explanation
This is a dangerous condition! With field disconnected, magnetic flux drops to near zero (only residual magnetism remains). To maintain back-EMF = V − I·Ra, the motor must accelerate dramatically.
N ∝ V / Φ — if Φ → 0, N → ∞ (theoretically)
The motor races (runaway condition) — speed becomes dangerously high. Centrifugal forces can mechanically destroy the armature (“armature fly-apart”). This is especially dangerous for series motors running at no load.
A DC series motor should NEVER be run without a load. A shunt motor can survive no-load but must never have its field circuit opened. Field protection relays are essential in DC motor drives.
Q26
Explanation
When the armature rotates in a magnetic field, it generates an EMF that opposes the supply voltage — this is back-EMF (Eb).
• Limits armature current — acts as self-regulating mechanism.
• At no load, Eb ≈ V (very little current drawn).
• Under heavy load, Eb drops → Ia increases → more torque.
• Back-EMF is the motor’s way of converting electrical energy to mechanical energy.
Ia = (V − Eb) / Ra | Eb = (P·Φ·N·Z) / (60·A)
Significance:• Limits armature current — acts as self-regulating mechanism.
• At no load, Eb ≈ V (very little current drawn).
• Under heavy load, Eb drops → Ia increases → more torque.
• Back-EMF is the motor’s way of converting electrical energy to mechanical energy.
Back-EMF explains why DC motors draw huge starting current (Eb = 0 at start). Starters are used to add resistance in armature circuit during starting.
Q27
Explanation
Types of losses:
1. Copper losses (I²R): Ohmic losses in winding resistance — reduced by using larger conductors, low-resistance materials, better insulation.
2. Core/Iron losses: Hysteresis (use grain-oriented silicon steel) + Eddy current (use laminated core).
3. Mechanical losses: Friction (bearings), windage (cooling fan) — reduced by good bearings, aerodynamic design.
4. Stray load losses: Due to leakage flux, non-uniform current distribution.
1. Copper losses (I²R): Ohmic losses in winding resistance — reduced by using larger conductors, low-resistance materials, better insulation.
2. Core/Iron losses: Hysteresis (use grain-oriented silicon steel) + Eddy current (use laminated core).
3. Mechanical losses: Friction (bearings), windage (cooling fan) — reduced by good bearings, aerodynamic design.
4. Stray load losses: Due to leakage flux, non-uniform current distribution.
Efficiency η = (Output Power) / (Output + All Losses) × 100%
Transformer efficiency is highest (>98%) at full load for power transformers. Maximum efficiency occurs when copper loss = iron loss (constant).
Q28
Explanation
Crawling: Due to harmonic components (particularly 7th harmonic) in flux waveform, motor may achieve a stable running speed at 1/7th of synchronous speed (about 1/7 × Ns). Motor “crawls” at low speed instead of accelerating to rated speed. Caused by slot harmonic interaction. Remedied by skewing rotor slots.
Cogging (Magnetic Locking): Rotor teeth lock with stator teeth due to magnetic attraction when number of rotor slots equals stator slots. Motor refuses to start. Remedied by: using a different number of rotor and stator slots, or skewing rotor bars.
Cogging (Magnetic Locking): Rotor teeth lock with stator teeth due to magnetic attraction when number of rotor slots equals stator slots. Motor refuses to start. Remedied by: using a different number of rotor and stator slots, or skewing rotor bars.
Cogging: starting problem. Crawling: running problem. Both are eliminated by skewing rotor slots — the standard manufacturing practice for squirrel-cage induction motors.
Q29
Explanation
Squirrel Cage: Rotor has short-circuited aluminium/copper bars — simple, rugged, low cost. Low starting torque, high starting current. Cannot add external resistance. Used for pumps, fans, compressors.
Slip-Ring (Wound Rotor): Rotor has 3-phase windings brought out via slip rings. External resistance can be added to rotor circuit → high starting torque, reduced starting current. Speed can be controlled. Used for cranes, elevators, mills requiring high starting torque.
Slip-Ring (Wound Rotor): Rotor has 3-phase windings brought out via slip rings. External resistance can be added to rotor circuit → high starting torque, reduced starting current. Speed can be controlled. Used for cranes, elevators, mills requiring high starting torque.
Adding external resistance to slip-ring rotor increases starting torque (up to max) while limiting starting current. At maximum torque, rotor resistance = rotor reactance (R₂ = X₂).
Q30
Explanation
Essential conditions for parallel operation of transformers:
1. Same voltage ratio (turns ratio) — else circulating current flows at no load.
2. Same percentage impedance — for proportional load sharing.
3. Same polarity — to avoid short circuit.
4. Same phase sequence (for 3-phase) — to avoid circulating currents.
5. Same phase displacement (same vector group, e.g., Dyn11 + Dyn11).
1. Same voltage ratio (turns ratio) — else circulating current flows at no load.
2. Same percentage impedance — for proportional load sharing.
3. Same polarity — to avoid short circuit.
4. Same phase sequence (for 3-phase) — to avoid circulating currents.
5. Same phase displacement (same vector group, e.g., Dyn11 + Dyn11).
Unequal impedances cause unequal load sharing — the lower impedance transformer gets overloaded. Unequal turns ratio causes circulating current even at no load, causing heating.
Q31
Explanation
DC Shunt Motor: Flux is approximately constant (field winding connected directly across supply). Speed is nearly constant from no-load to full load. Good speed regulation — used for constant-speed drives (lathes, fans, pumps).
DC Series Motor: Field winding in series with armature → Φ ∝ Ia. As load increases, current & flux both increase → torque increases rapidly (T ∝ Ia²). Speed decreases sharply with load. Extremely high starting torque. Used for traction (trains), cranes, elevators.
DC Series Motor: Field winding in series with armature → Φ ∝ Ia. As load increases, current & flux both increase → torque increases rapidly (T ∝ Ia²). Speed decreases sharply with load. Extremely high starting torque. Used for traction (trains), cranes, elevators.
Series motor has highest starting torque of all DC motors. Shunt motor has best speed regulation. Compound motor is a compromise between the two.
Q32
Explanation
An auto-transformer has a single winding with a tapping point. Part of the winding is common to both primary and secondary — power transfer is via both conduction AND magnetic induction.
Advantages: Less copper, smaller size and weight, better voltage regulation, lower leakage reactance, higher efficiency for same rating.
Limitations: No electrical isolation between primary and secondary (safety hazard). Cannot be used where isolation is required. High short-circuit current if fault occurs.
Advantages: Less copper, smaller size and weight, better voltage regulation, lower leakage reactance, higher efficiency for same rating.
Limitations: No electrical isolation between primary and secondary (safety hazard). Cannot be used where isolation is required. High short-circuit current if fault occurs.
Auto-transformer starters reduce induction motor starting voltage to 65% or 80% of supply. Also used in lab variacs (variable auto-transformers) and HVDC transformers.
Q33
Explanation
The commutator is a mechanical rectifier in DC machines. In a generator, it converts the alternating EMF generated in armature conductors into unidirectional (DC) output. In a motor, it reverses current in armature coils at the right moment to maintain continuous torque in one direction.
Without commutator, output would be AC (alternating) — the machine would behave as an AC machine. Brushes and commutator are the major maintenance points in DC machines — subject to sparking, wear, and require periodic replacement.
Without commutator, output would be AC (alternating) — the machine would behave as an AC machine. Brushes and commutator are the major maintenance points in DC machines — subject to sparking, wear, and require periodic replacement.
This is why brushless DC (BLDC) motors use electronic commutation (via inverter + Hall sensors) instead of mechanical commutator — enabling maintenance-free operation. ISRO uses BLDC motors in spacecraft mechanisms.
Q34
Explanation
When load current flows through armature, it creates its own magnetic field that distorts and weakens the main field flux — this effect is armature reaction. Effects: flux weakening (reduces torque/EMF), flux distortion (shifts magnetic neutral axis), sparking at brushes.
Compensation methods:
1. Brush shift (advance or retard by geometric neutral axis shift — temporary fix).
2. Interpoles (commutating poles between main poles): Cancel armature reaction in commutation zone.
3. Compensating winding: Embedded in pole faces, connected in series with armature — best method for large machines.
Compensation methods:
1. Brush shift (advance or retard by geometric neutral axis shift — temporary fix).
2. Interpoles (commutating poles between main poles): Cancel armature reaction in commutation zone.
3. Compensating winding: Embedded in pole faces, connected in series with armature — best method for large machines.
Compensating windings and interpoles together completely neutralise armature reaction — essential for DC motors in steel mill drives and traction applications.
Q35
Explanation
The Buchholz relay is a gas-actuated protection device used in oil-immersed transformers to detect internal faults. It is installed in the pipe connecting transformer tank to the conservator tank.
Working: Any internal fault (arc, insulation deterioration) decomposes transformer oil and generates gas. Gas bubbles rise and collect in the Buchholz relay. Minor faults: float activates alarm. Severe faults: oil surge actuates trip coil, disconnecting the transformer.
It detects: inter-turn faults, core faults, partial discharge, oil level drop.
Working: Any internal fault (arc, insulation deterioration) decomposes transformer oil and generates gas. Gas bubbles rise and collect in the Buchholz relay. Minor faults: float activates alarm. Severe faults: oil surge actuates trip coil, disconnecting the transformer.
It detects: inter-turn faults, core faults, partial discharge, oil level drop.
Buchholz relay is used ONLY for oil-immersed transformers with conservator tank. Dry-type transformers use temperature detectors and overcurrent relays instead.
Power Systems & Protection
Q36
Explanation
Per-unit (pu) value = Actual quantity / Base quantity.
Typically: Base VA (MVA), Base Voltage (kV) are chosen; Base current and Base impedance are derived.
• Eliminates the need to carry actual transformers ratios in calculations (transformer appears as series impedance).
• Simplifies analysis of interconnected systems at different voltage levels.
• Typical per-unit values of machines fall in similar ranges — easy comparison.
• Reduces computational complexity in power flow, fault analysis.
Typically: Base VA (MVA), Base Voltage (kV) are chosen; Base current and Base impedance are derived.
Z_pu = Z_actual / Z_base | Z_base = V_base² / S_base
Advantages:• Eliminates the need to carry actual transformers ratios in calculations (transformer appears as series impedance).
• Simplifies analysis of interconnected systems at different voltage levels.
• Typical per-unit values of machines fall in similar ranges — easy comparison.
• Reduces computational complexity in power flow, fault analysis.
In per-unit system, 1 pu voltage across a transformer means normal voltage on both sides regardless of turns ratio. Essential for load flow (Newton-Raphson), fault analysis, and transient stability studies.
Q37
Explanation
Fuse: Sacrificial element — melts and destroys itself on overcurrent. Single use. Fast acting. Low cost. No moving parts. Used for small loads, branch circuit protection.
Circuit Breaker (CB): Reusable switching device — trips on fault and can be reset. Can interrupt at specific current values. Adjustable trip settings. Suitable for high voltages and fault currents. Used in distribution panels, transmission line protection.
CB Types: Air CB (low voltage), Oil CB, SF6 CB (high voltage), Vacuum CB (medium voltage — maintenance-free, used in DRDO/ISRO applications).
Circuit Breaker (CB): Reusable switching device — trips on fault and can be reset. Can interrupt at specific current values. Adjustable trip settings. Suitable for high voltages and fault currents. Used in distribution panels, transmission line protection.
CB Types: Air CB (low voltage), Oil CB, SF6 CB (high voltage), Vacuum CB (medium voltage — maintenance-free, used in DRDO/ISRO applications).
SF6 (sulphur hexafluoride) gas circuit breakers are used for EHV lines (132 kV and above). Vacuum CBs are preferred for medium voltage (11–33 kV) due to maintenance advantages. SF6 is a greenhouse gas — being phased out gradually.
Q38
Explanation
Differential protection compares the current entering the protected equipment with the current leaving it. Under normal conditions, (scaled) input current ≈ output current → differential current ≈ 0 → no trip. During an internal fault, current difference becomes significant → relay trips.
Challenge: Magnetising inrush current (at switch-on) has large differential component but no fault — solved using harmonic restraint (2nd harmonic blocking).
I_diff = |I1 − I2| (exceeds threshold → trip)
Advantages: Highly sensitive to internal faults, immune to external faults (through faults), fast operation, selective (only trips faulted equipment).Challenge: Magnetising inrush current (at switch-on) has large differential component but no fault — solved using harmonic restraint (2nd harmonic blocking).
Differential protection (87T) is the primary protection for large power transformers. Biased differential relays with harmonic blocking are standard in modern digital protection relays (IEDs).
Q39
Explanation
Ferranti Effect: In long transmission lines under no-load or light load conditions, the receiving-end voltage is higher than the sending-end voltage. Caused by the charging current of the line’s distributed capacitance flowing through the line inductance, creating a voltage rise.
Occurs prominently in: Long EHV cables (underground), long overhead lines at no load (>300 km), long HVDC cables.
Occurs prominently in: Long EHV cables (underground), long overhead lines at no load (>300 km), long HVDC cables.
V_R > V_S under no-load/capacitive loads
Mitigation: Shunt reactors at receiving end or along the line to absorb the leading reactive current and suppress the voltage rise.
Ferranti effect can cause overvoltage damage to insulation and equipment. Shunt reactors are installed at substations of long EHV lines specifically to address this. Relevant in India’s 765 kV transmission system.
Q40
Explanation
Earthing (Grounding) connects metallic parts of electrical installation to earth at zero potential. Purposes:
1. Safety: Provides a low-resistance path for fault current → trips protective devices → prevents electric shock.
2. Voltage stabilization: Limits overvoltages (lightning, switching surges).
3. EMI reduction: Shields against electromagnetic interference.
4. Lightning protection: Dissipates lightning energy to earth safely.
Types: Solid earthing (neutral directly connected), resistance earthing, reactance earthing, isolated neutral.
1. Safety: Provides a low-resistance path for fault current → trips protective devices → prevents electric shock.
2. Voltage stabilization: Limits overvoltages (lightning, switching surges).
3. EMI reduction: Shields against electromagnetic interference.
4. Lightning protection: Dissipates lightning energy to earth safely.
Types: Solid earthing (neutral directly connected), resistance earthing, reactance earthing, isolated neutral.
IS 3043 governs earthing practice in India. Earth resistance should be less than 1 ohm for large stations. Earth electrodes are tested periodically using Earth Resistance Tester (Megger).
Electronics — Analog & Devices
Q61
Explanation
BJT (Bipolar Junction Transistor): Current-controlled device. Base current controls collector current. Uses both holes and electrons (bipolar). Low input impedance. Better for high-speed, high-current applications. Faster switching at moderate voltages.
FET (Field Effect Transistor): Voltage-controlled device. Gate voltage controls drain current. High input impedance (MOSFET gate draws virtually zero current). Lower noise. Better for signal amplification, analog switches, op-amps. MOSFET dominates digital IC design.
Choose MOSFET: Digital logic, power electronics, low-power circuits, RF switching.
FET (Field Effect Transistor): Voltage-controlled device. Gate voltage controls drain current. High input impedance (MOSFET gate draws virtually zero current). Lower noise. Better for signal amplification, analog switches, op-amps. MOSFET dominates digital IC design.
BJT: Ic = β × Ib | MOSFET: Id = k(Vgs − Vth)²
Choose BJT: High-current linear amplifiers, audio power stages, high-speed ECL logic.Choose MOSFET: Digital logic, power electronics, low-power circuits, RF switching.
Power MOSFETs dominate power electronics (inverters, SMPS) due to voltage control, fast switching, and ease of paralleling. IGBTs combine BJT current-handling with MOSFET gate control — used in high-power inverters (drives, solar, EVs).
Q62
Explanation
Ideal Op-Amp Properties:
• Infinite open-loop gain (A = ∞)
• Infinite input impedance (Zin = ∞ → Iin = 0)
• Zero output impedance (Zo = 0)
• Infinite bandwidth (BW = ∞)
• Zero offset voltage, zero noise
• CMRR = ∞ (perfectly rejects common-mode signals)
Virtual Ground (Virtual Short): In a closed-loop inverting/non-inverting op-amp with negative feedback, since gain is infinite, the differential input voltage must be essentially zero (V+ ≈ V−). The inverting input is not actually connected to ground — but it appears to be at ground potential → “virtual ground.”
• Infinite open-loop gain (A = ∞)
• Infinite input impedance (Zin = ∞ → Iin = 0)
• Zero output impedance (Zo = 0)
• Infinite bandwidth (BW = ∞)
• Zero offset voltage, zero noise
• CMRR = ∞ (perfectly rejects common-mode signals)
Virtual Ground (Virtual Short): In a closed-loop inverting/non-inverting op-amp with negative feedback, since gain is infinite, the differential input voltage must be essentially zero (V+ ≈ V−). The inverting input is not actually connected to ground — but it appears to be at ground potential → “virtual ground.”
Virtual ground concept is key to analysing all op-amp circuits. It simplifies KCL analysis at the summing junction. Real op-amps (741, LM358, TL071) have finite gain (~100 dB), finite BW, and small input bias currents.
Q63
Explanation
CMRR (Common Mode Rejection Ratio): Ratio of differential-mode gain to common-mode gain.
Why important? In sensor applications (ECG, instrumentation amplifiers, strain gauges), the signal is small and differential, while noise (50 Hz hum, electromagnetic interference) appears equally on both inputs as common-mode. High CMRR ensures only the real signal is amplified.
CMRR = Ad / Acm (in dB: 20 log(Ad/Acm))
A high CMRR means the op-amp amplifies the differential signal strongly but rejects signals common to both inputs (noise, interference). For a 741 op-amp: CMRR ≈ 90 dB typically.Why important? In sensor applications (ECG, instrumentation amplifiers, strain gauges), the signal is small and differential, while noise (50 Hz hum, electromagnetic interference) appears equally on both inputs as common-mode. High CMRR ensures only the real signal is amplified.
Instrumentation amplifiers (INA128, AD620) have CMRR > 100 dB and are designed specifically for sensor signal conditioning in medical, industrial, and aerospace applications.
Q64
Explanation
Regular PN Diode (Reverse Bias): Very small leakage current flows. If reverse voltage exceeds breakdown voltage, catastrophic (destructive) breakdown occurs — device damaged.
Zener Diode: Heavily doped. Undergoes controlled, reversible breakdown at a precise voltage (Zener voltage, Vz). After breakdown, voltage remains nearly constant despite large changes in current. This is its operating point — used intentionally.
Zener Diode: Heavily doped. Undergoes controlled, reversible breakdown at a precise voltage (Zener voltage, Vz). After breakdown, voltage remains nearly constant despite large changes in current. This is its operating point — used intentionally.
Zener mechanism: <5V → Zener effect (tunnelling)
5–8V → Both | >8V → Avalanche effect
Uses: Voltage reference, voltage regulator, overvoltage protection, clipping circuits.
5–8V → Both | >8V → Avalanche effect
Zener diode is always used in reverse bias for regulation. In forward bias, it behaves like a regular diode (Vf ≈ 0.7 V). The LM431 is a precision adjustable shunt regulator based on Zener principle, widely used in SMPS.
Q65
Explanation
A PLL is a feedback control system that locks the phase of its output oscillator to the phase of an input signal. Components: Phase Detector (PD), Low Pass Filter (LPF), Voltage Controlled Oscillator (VCO).
The PD compares input phase with VCO output phase → generates error voltage. LPF smooths the error → drives VCO until output frequency/phase matches input (locked state).
The PD compares input phase with VCO output phase → generates error voltage. LPF smooths the error → drives VCO until output frequency/phase matches input (locked state).
f_out = N × f_ref (when divided by N in loop)
Applications: Frequency synthesis (radio tuners), FM demodulation, clock recovery in communication, motor speed control, GPS receivers, ISRO satellite transponders, carrier recovery in modems.
PLLs are essential in spacecraft communication systems. ISRO uses PLLs for coherent signal processing in GSAT and PSLV telemetry systems. CD74HC4046 and LMX2594 are common PLL ICs.
Q66
Explanation
Gain-Bandwidth Product (GBW or GBP) is a constant for a given op-amp. As gain increases, bandwidth decreases proportionally.
GBW = Av × BW = constant
BW = GBW / Av = 1 MHz / 100 = 10 kHz
So if GBW = 1 MHz and gain is configured to 100 (40 dB), the usable bandwidth is only 10 kHz. At unity gain (Av = 1), bandwidth = 1 MHz (full GBW).
BW = GBW / Av = 1 MHz / 100 = 10 kHz
This is why high-gain amplifier stages have limited bandwidth. To amplify a 100 kHz signal with gain of 100, you need an op-amp with GBW ≥ 10 MHz. Cascading stages reduces total gain requirement per stage, restoring bandwidth.
Q67
Explanation
Linear Power Supply: Uses a pass transistor in its active (linear) region to drop excess voltage. Simple, low noise, very stable. Low efficiency (40–60% typical — excess energy dissipated as heat). Heavy (large transformer). Good for analog, audio, RF circuits.
Switching Power Supply (SMPS): Transistor switches ON/OFF at high frequency (100 kHz–MHz) — inductor/capacitor filter output. High efficiency (85–95%). Compact, lightweight. Generates electromagnetic interference (EMI). Used almost everywhere: computers, phones, adapters, DRDO radar PSUs.
Switching Power Supply (SMPS): Transistor switches ON/OFF at high frequency (100 kHz–MHz) — inductor/capacitor filter output. High efficiency (85–95%). Compact, lightweight. Generates electromagnetic interference (EMI). Used almost everywhere: computers, phones, adapters, DRDO radar PSUs.
ISRO spacecraft power systems use highly efficient DC-DC converters (switching) due to tight power budgets. Linear regulators (LDO) are used where noise is critical (ADC references, PLL supply). Key metric: SMPS efficiency reduces thermal dissipation and battery weight.
Q68
Explanation
A comparator compares input with a single reference threshold. If input > reference → high output; else low. Very sensitive to noise — noisy input near threshold causes rapid output toggling (multiple transitions).
A Schmitt Trigger uses hysteresis — it has two different thresholds: upper trigger point (UTP) and lower trigger point (LTP). Output switches HIGH only when input exceeds UTP, and switches LOW only when input falls below LTP.
A Schmitt Trigger uses hysteresis — it has two different thresholds: upper trigger point (UTP) and lower trigger point (LTP). Output switches HIGH only when input exceeds UTP, and switches LOW only when input falls below LTP.
Hysteresis = UTP − LTP | Noise immunity improved
This hysteresis makes the Schmitt trigger immune to noise — it won’t oscillate from small noise around the threshold. Used in: signal conditioning, wave shaping, touch switches, oscillators.
The 74HC14 is a hex inverting Schmitt trigger IC commonly used to “clean up” noisy digital signals. Schmitt triggers convert slow or noisy analog transitions into clean digital edges — essential before feeding signals into microcontrollers or FPGAs.
Q69
Explanation
A rectifier converts AC to pulsating DC by allowing current flow in one direction only.
Full-Wave (Bridge): Uses 4 diodes. Both half-cycles used. Lower ripple, higher efficiency (81.2%), better regulation. Ripple frequency = 2×supply frequency (100 Hz for 50 Hz input).
Half-wave: V_dc = Vm/π ≈ 0.318Vm | Ripple factor: 1.21
Full-wave: V_dc = 2Vm/π ≈ 0.636Vm | Ripple factor: 0.48
Half-Wave: Uses 1 diode. Only positive half-cycle used. Wasteful, high ripple, poor efficiency (40.6%). Simple, cheap.Full-wave: V_dc = 2Vm/π ≈ 0.636Vm | Ripple factor: 0.48
Full-Wave (Bridge): Uses 4 diodes. Both half-cycles used. Lower ripple, higher efficiency (81.2%), better regulation. Ripple frequency = 2×supply frequency (100 Hz for 50 Hz input).
Bridge rectifier is standard in SMPS front-ends. The ripple voltage is filtered by a bulk capacitor. Larger capacitor → less ripple → better regulation. Peak Inverse Voltage (PIV) = 2Vm for center-tap FWR, Vm for bridge FWR.
Q70
Explanation
A standard differential amplifier has low and unequal input impedance — loading the sensor source and having poor CMRR.
An Instrumentation Amplifier (In-Amp) uses three op-amps: two input buffer stages (very high input impedance, no loading) feeding a third difference stage. Gain is set by a single resistor.
An Instrumentation Amplifier (In-Amp) uses three op-amps: two input buffer stages (very high input impedance, no loading) feeding a third difference stage. Gain is set by a single resistor.
Gain = 1 + 2R/Rg (three op-amp configuration)
Properties: Very high input impedance (>10 GΩ), excellent CMRR (>80 dB), precise adjustable gain, very low offset and noise.
In-amps are used for sensor signal conditioning: strain gauges (Wheatstone bridge output), thermocouples, ECG/EEG bio-signals, RTDs. AD620, INA128 are industry-standard IC in-amps used in DRDO and BEL sensor systems.
Digital Electronics & Microprocessors
Q91
Explanation
A flip-flop is a bistable multivibrator — a 1-bit memory element that stores one of two states.
SR (Set-Reset): S=1,R=0 → Q=1; S=0,R=1 → Q=0; S=R=1 → forbidden (undefined) state.
D (Data): Q follows D input at clock edge. Eliminates forbidden state. Used in registers, buffers.
JK: Like SR but J=K=1 toggles output. Universal FF — can be configured as SR, D, or T.
T (Toggle): T=1 → output toggles on each clock; T=0 → holds. Used in counters.
SR (Set-Reset): S=1,R=0 → Q=1; S=0,R=1 → Q=0; S=R=1 → forbidden (undefined) state.
D (Data): Q follows D input at clock edge. Eliminates forbidden state. Used in registers, buffers.
JK: Like SR but J=K=1 toggles output. Universal FF — can be configured as SR, D, or T.
T (Toggle): T=1 → output toggles on each clock; T=0 → holds. Used in counters.
JK is the most versatile flip-flop. D flip-flop is most common in digital design (used in registers, FIFO). T flip-flop is used in binary counters (divide-by-2 circuits). Racing/glitch issues in asynchronous designs led to master-slave implementations.
Q92
Explanation
Setup Time (tsu): Minimum time data must be stable BEFORE the active clock edge for reliable capture.
Hold Time (th): Minimum time data must remain stable AFTER the active clock edge.
Violation: If setup or hold time is violated, the flip-flop enters a metastable state — an unstable equilibrium where the output is neither valid HIGH nor valid LOW. It will eventually resolve, but unpredictably. This can cause system malfunction — timing errors, spurious operations, or system crash.
Mitigation: Synchronizers, margin in timing closure, slower clock, careful PCB layout to minimise propagation delays.
Hold Time (th): Minimum time data must remain stable AFTER the active clock edge.
Violation: If setup or hold time is violated, the flip-flop enters a metastable state — an unstable equilibrium where the output is neither valid HIGH nor valid LOW. It will eventually resolve, but unpredictably. This can cause system malfunction — timing errors, spurious operations, or system crash.
Mitigation: Synchronizers, margin in timing closure, slower clock, careful PCB layout to minimise propagation delays.
Metastability is a fundamental limitation in all synchronous digital design, especially at clock-domain crossing (CDC) interfaces. ISRO embeds synchronisers in FPGA designs for inter-domain signals. Flip-flop MTBF depends on frequency and metastability resolution time.
Q93
Explanation
SRAM (Static RAM): Uses 6 transistor bistable latch per bit. Holds data as long as powered (no refresh). Fast (5–25 ns), expensive, high power, low density. Used for cache memory (L1, L2, L3).
DRAM (Dynamic RAM): Uses 1 transistor + 1 capacitor per bit. Data stored as charge on capacitor. Capacitor leaks charge → must be refreshed periodically (every 64 ms typically).
Slower, cheaper, lower power per bit, high density. Used for main memory (DDR4, DDR5 RAM).
DRAM (Dynamic RAM): Uses 1 transistor + 1 capacitor per bit. Data stored as charge on capacitor. Capacitor leaks charge → must be refreshed periodically (every 64 ms typically).
Slower, cheaper, lower power per bit, high density. Used for main memory (DDR4, DDR5 RAM).
DRAM refresh is handled by the memory controller automatically — transparent to the CPU. During refresh, DRAM cannot respond to memory accesses — called “refresh cycle overhead”. DRAM density advantage: 1T1C vs SRAM’s 6T per bit.
Q94
Explanation
FPGA (Field Programmable Gate Array): Reconfigurable hardware — contains configurable logic blocks (CLBs), interconnects, and I/O cells that can be programmed after manufacturing using HDL (VHDL/Verilog). Programmed via bitstream loaded from flash. Re-programmable anytime.
ASIC (Application-Specific IC): Custom chip fixed at fabrication — cannot be changed. Much faster, lower power, lower cost at volume. High NRE (Non-Recurring Engineering) cost for design & fabrication (crores of rupees).
Microcontroller (MCU): Fixed processor executing software — sequential, flexible via programming but fundamentally software-based. Cannot do true parallel hardware operations.
ASIC (Application-Specific IC): Custom chip fixed at fabrication — cannot be changed. Much faster, lower power, lower cost at volume. High NRE (Non-Recurring Engineering) cost for design & fabrication (crores of rupees).
Microcontroller (MCU): Fixed processor executing software — sequential, flexible via programming but fundamentally software-based. Cannot do true parallel hardware operations.
ISRO uses radiation-hardened FPGAs (RTAX series from Microchip/Actel, now Microsemi) for satellite on-board data handling and spacecraft control. DRDO uses FPGAs for radar signal processing. BARC uses FPGAs for nuclear instrument data acquisition.
Q95
Explanation
2’s complement is the standard method for representing signed integers in binary. To get 2’s complement: invert all bits (1’s complement) then add 1.
• Subtraction becomes addition (A − B = A + (−B) in 2’s complement) → single hardware adder handles both add and subtract.
• Single representation for zero (unlike 1’s complement which has +0 and −0).
• Range for 8 bits: −128 to +127 (2^7 negative values, 2^7−1 positive).
• Hardware simplicity — all modern processors, microcontrollers use 2’s complement arithmetic.
−5 in 8-bit: 00000101 → invert → 11111010 → +1 → 11111011
Why important?• Subtraction becomes addition (A − B = A + (−B) in 2’s complement) → single hardware adder handles both add and subtract.
• Single representation for zero (unlike 1’s complement which has +0 and −0).
• Range for 8 bits: −128 to +127 (2^7 negative values, 2^7−1 positive).
• Hardware simplicity — all modern processors, microcontrollers use 2’s complement arithmetic.
Overflow detection in 2’s complement: when signs of operands are same but result sign is different. For 8-bit signed: adding two positive numbers should give positive result — if not, overflow occurred. Signed vs unsigned overflow detection differs.
Control Systems
Q116
Explanation
The transfer function G(s) is the ratio of the Laplace transform of output Y(s) to input X(s), with all initial conditions zero.
Poles: roots of denominator — determine natural modes and stability.
Zeros: roots of numerator — shape the response, create notches in frequency response.
G(s) = Y(s) / X(s) = Numerator polynomial / Denominator polynomial
It carries: natural frequencies (poles), zeros, gain, stability information (pole locations in s-plane), steady-state gain (G(0)), frequency response (Bode plot via G(jω)).Poles: roots of denominator — determine natural modes and stability.
Zeros: roots of numerator — shape the response, create notches in frequency response.
Poles in left half s-plane → stable system. Poles on jω axis → marginally stable. Poles in right half plane → unstable. Transfer function is defined only for linear, time-invariant (LTI) systems. Used in spacecraft attitude control in ISRO’s PSLV and GSLV.
Q117
Explanation
The Routh-Hurwitz criterion determines stability of a system without computing actual poles. A system is stable if all elements in the first column of the Routh array are positive (same sign).
For characteristic polynomial:
If any element is zero or negative → system is unstable.
For characteristic polynomial:
a₀s³ + a₁s² + a₂s + a₃ = 0
Routh Array first column: a₀, a₁, (a₁a₂−a₀a₃)/a₁, a₃
Stability: all > 0 → a₁a₂ > a₀a₃ (Hurwitz condition)
Number of sign changes in first column = number of RHP poles.Stability: all > 0 → a₁a₂ > a₀a₃ (Hurwitz condition)
If any element is zero or negative → system is unstable.
Routh-Hurwitz gives stability condition but not the location of poles. It’s a necessary and sufficient condition for stability of LTI systems. Used in ISRO launch vehicle control loop stability analysis.
Q118
Explanation
Phase Margin (PM): How much additional phase lag the system can tolerate before becoming unstable. PM = 180° + ∠G(jω) at the gain crossover frequency (where |G(jω)| = 0 dB).
Stable if: PM > 0° and GM > 1 (GM > 0 dB). Good design: PM ≈ 45°–60°, GM ≥ 6 dB — provides robustness to plant uncertainty.
PM = 180° + phase of G(jω_gc)
Gain Margin (GM): How much gain can be increased before instability. GM = 1/|G(jω_pc)| at phase crossover frequency (where phase = −180°). In dB: GM = −20log|G(jω_pc)|.
Stable if: PM > 0° and GM > 1 (GM > 0 dB). Good design: PM ≈ 45°–60°, GM ≥ 6 dB — provides robustness to plant uncertainty.
PM directly relates to damping ratio: ζ ≈ PM(degrees)/100 (approximate). Low PM → underdamped, oscillatory response. PM = 0° → marginally stable (sustained oscillation). Bode plot and Nyquist plot are tools to read GM and PM graphically.
Q119
Explanation
u(t) = Kp·e(t) + Ki·∫e(t)dt + Kd·de(t)/dt
Proportional (P): Output proportional to error. Reduces rise time and steady-state error. Large Kp → oscillation, instability.Integral (I): Eliminates steady-state error (accumulates past error). Slows response, can cause windup. Used for type-1 systems that need zero steady-state error for step input.
Derivative (D): Anticipates future error (rate of change). Improves stability, reduces overshoot. Sensitive to noise — usually filtered in practice.
PID tuning methods: Ziegler-Nichols, Cohen-Coon, IMC, model-based, auto-tune.
PID controllers are the workhorses of industrial control — >90% of process controllers use PID. ISRO uses advanced control (LQR, H-infinity) for spacecraft attitude control, but PID is used for less critical loops. Anti-windup is essential for I-term when actuator saturates.
Q120
Explanation
Steady-state error (e_ss) is the difference between desired output and actual output as t→∞. Determined by system type (number of open-loop poles at origin).
Adding integral term (adding pole at origin) increases system type by 1 — eliminates steady-state error for that input class.
Type 0: Step → finite e_ss, Ramp → infinite e_ss
Type 1: Step → 0 e_ss, Ramp → finite e_ss, Parabola → ∞
Type 2: Step → 0, Ramp → 0, Parabola → finite e_ss
Error constants: Kp (position), Kv (velocity), Ka (acceleration) determine the magnitude of steady-state error.Type 1: Step → 0 e_ss, Ramp → finite e_ss, Parabola → ∞
Type 2: Step → 0, Ramp → 0, Parabola → finite e_ss
Adding integral term (adding pole at origin) increases system type by 1 — eliminates steady-state error for that input class.
This is why PID integral action is essential for eliminating steady-state error. But increasing type number reduces relative stability — there is a fundamental trade-off between accuracy and stability in feedback systems.
Signals & Measurements
Q131
Explanation
Nyquist Theorem: A bandlimited signal with maximum frequency f_max can be perfectly reconstructed if sampled at a rate f_s ≥ 2×f_max.
Prevention: Anti-aliasing filter (low-pass filter) applied before sampling to remove frequency components above f_s/2 (Nyquist frequency). Then sample at ≥ Nyquist rate.
f_s ≥ 2 × f_max (Nyquist rate)
Aliasing: If sampling rate is too low (f_s < 2×f_max), high-frequency components appear as low-frequency components in the sampled signal — the frequency “folds” and aliases. Signal is distorted and cannot be recovered.
Prevention: Anti-aliasing filter (low-pass filter) applied before sampling to remove frequency components above f_s/2 (Nyquist frequency). Then sample at ≥ Nyquist rate.
Audio CD sampling rate = 44.1 kHz (covers up to 22.05 kHz — beyond human hearing limit of ~20 kHz). ADC datasheets specify anti-aliasing filter requirements. ISRO telemetry ADCs use anti-aliasing filters before all sensor data digitization.
Q132
Explanation
AM: Carrier amplitude varies with message signal. Constant carrier frequency. Bandwidth = 2×f_m. Susceptible to noise/interference (noise affects amplitude). Simple receiver circuit. Used: MW/SW broadcast radio, aircraft comms (VHF AM).
FM: Carrier frequency varies with message signal. Constant amplitude. Bandwidth = 2(Δf + f_m) (Carson’s rule). Much better noise immunity (noise appears as amplitude variation — limiters remove it). Better audio quality. Used: VHF/FM broadcast (88–108 MHz), two-way radios, DRDO tactical comms.
FM: Carrier frequency varies with message signal. Constant amplitude. Bandwidth = 2(Δf + f_m) (Carson’s rule). Much better noise immunity (noise appears as amplitude variation — limiters remove it). Better audio quality. Used: VHF/FM broadcast (88–108 MHz), two-way radios, DRDO tactical comms.
AM: s(t) = Ac[1 + m·cos(ωmt)]cos(ωct)
FM: s(t) = Ac·cos(ωct + kf∫m(τ)dτ)
FM: s(t) = Ac·cos(ωct + kf∫m(τ)dτ)
FM has better SNR performance than AM for same transmitted power — specifically, FM SNR advantage = 3/2 × β² (where β = modulation index). This is why FM is used for music broadcasting (better audio quality) while AM is used for talk radio and long-range broadcasts (narrower bandwidth, travels farther).
Q133
Explanation
Fourier Transform: Decomposes a time-domain signal into its constituent frequencies. Exists only for signals that satisfy Dirichlet conditions (absolutely integrable). Shows frequency spectrum — magnitude and phase vs frequency (real axis only, s = jω).
F(ω) = ∫ f(t)e^(−jωt)dt | Laplace: F(s) = ∫ f(t)e^(−st)dt
Laplace Transform: Extension of Fourier — uses complex frequency s = σ + jω. Applicable to a wider class of signals (including growing exponentials). Used for system analysis — transfer functions, stability (s-plane). Handles initial conditions. Fourier is a special case when σ = 0.
Fourier: frequency analysis and signal processing (spectra, filters). Laplace: control system design (transfer functions, stability). Z-transform is the discrete-time equivalent of Laplace — used in digital signal processing and digital control design.
Q134
Explanation
A Wheatstone bridge consists of four resistors in a diamond configuration with a voltage source and a galvanometer. Bridge is balanced when the galvanometer reads zero.
Used for: Strain gauge measurement, RTD (temperature) sensing, precision resistance comparison.
Balance condition: R1/R2 = R3/R4 ⟹ Unknown Rx = R3 × R2/R1
Accuracy advantage: At balance, measurement is independent of supply voltage variations and contact resistance. Only relative resistance ratios matter. Galvanometer null detection avoids loading errors.Used for: Strain gauge measurement, RTD (temperature) sensing, precision resistance comparison.
Wheatstone bridge in strain gauges: mechanical strain changes resistance → bridge unbalance → output voltage proportional to strain. Used in load cells (weighing scales), pressure transducers, accelerometers. Four-active-arm bridge gives 4× sensitivity and excellent temperature compensation.
Q135
Explanation
Accuracy: How close measurement is to the true value. Affected by systematic/calibration errors.
Precision: Repeatability — how closely repeated measurements agree with each other. Affected by random errors. A measurement can be precise but inaccurate (systematically wrong).
Resolution: Smallest change in input that produces detectable output change. For 12-bit ADC with 3.3V range: resolution = 3.3/4096 ≈ 0.8 mV.
Sensitivity: Ratio of change in output to change in input. Units: V/°C, mV/Pa, etc. Higher sensitivity → easier to detect small changes.
Precision: Repeatability — how closely repeated measurements agree with each other. Affected by random errors. A measurement can be precise but inaccurate (systematically wrong).
Resolution: Smallest change in input that produces detectable output change. For 12-bit ADC with 3.3V range: resolution = 3.3/4096 ≈ 0.8 mV.
Sensitivity: Ratio of change in output to change in input. Units: V/°C, mV/Pa, etc. Higher sensitivity → easier to detect small changes.
A sharp shooter analogy: Accurate = hits bullseye consistently. Precise = tight grouping even if off-center. Accurate AND precise = tight grouping at bullseye. You can calibrate away inaccuracy but not imprecision. This distinction is critical in BARC and DRDO test & evaluation work.
Q136
Explanation
PWM: A fixed-frequency digital signal whose ON-time (duty cycle) is varied to control average power delivered to a load.
Advantages: High efficiency (transistor is either fully ON or fully OFF — minimal power dissipation), precise control, simple digital control from microcontroller PWM peripheral.
V_avg = Duty Cycle × V_supply = (t_on/T) × V
Motor speed control: PWM signal fed to power MOSFET/IGBT switching the motor supply. At high frequency (>1 kHz), motor inductance smooths the current. Varying duty cycle from 0–100% controls average voltage/current → motor speed varies continuously.Advantages: High efficiency (transistor is either fully ON or fully OFF — minimal power dissipation), precise control, simple digital control from microcontroller PWM peripheral.
PWM frequency choice: Too low → audible noise (< 20 kHz), motor vibration. Too high → switching losses increase. Typical: 15–25 kHz for motor drives. ISRO uses PWM for deployment mechanism control, reaction wheel speed control, and solar panel drive electronics.
Q137
Explanation
Energy Spectral Density (ESD) S_E(f): Used for energy signals (finite total energy, finite duration — e.g., a pulse). ESD = |F(f)|² where F(f) is the Fourier transform. Total energy = ∫S_E(f)df (Parseval’s theorem).
Power Spectral Density (PSD) S_x(f): Used for power signals (infinite duration, finite average power — e.g., noise, periodic signals, random signals). PSD = Fourier transform of autocorrelation function (Wiener-Khinchin theorem). Total power = ∫S_x(f)df.
Power Spectral Density (PSD) S_x(f): Used for power signals (infinite duration, finite average power — e.g., noise, periodic signals, random signals). PSD = Fourier transform of autocorrelation function (Wiener-Khinchin theorem). Total power = ∫S_x(f)df.
Noise is always characterised by PSD (W/Hz). White noise: flat PSD across all frequencies. Thermal noise PSD = 4kTR (W/Hz) where k = Boltzmann constant, T = temperature, R = resistance. PSD is critical in BARC detector noise analysis and DRDO radar receiver design.
Q138
Explanation
CT (Current Transformer): Steps down high current for measurement. Primary has few turns (1–5) in series with the power line. Secondary gives 5A or 1A to meters/relays. Primary current ≈ fixed by system — CT secondary current mirrors primary at ratio N1/N2.
PT (Potential Transformer): Steps down high voltage for measurement. Primary connected across power line. Secondary gives 110V or 63.5V to meters. Standard operating condition: secondary close to open circuit (high burden impedance).
Why CT secondary MUST NOT be open-circuited: CT primary current is forced by the system (line current) and cannot change. With secondary open, no ampere-turn balance → all primary MMF drives the core → enormous flux → very high induced EMF in secondary (kV range) → insulation breakdown, fire hazard, fatal voltage.
PT (Potential Transformer): Steps down high voltage for measurement. Primary connected across power line. Secondary gives 110V or 63.5V to meters. Standard operating condition: secondary close to open circuit (high burden impedance).
Why CT secondary MUST NOT be open-circuited: CT primary current is forced by the system (line current) and cannot change. With secondary open, no ampere-turn balance → all primary MMF drives the core → enormous flux → very high induced EMF in secondary (kV range) → insulation breakdown, fire hazard, fatal voltage.
CT secondary is always short-circuited or kept under burden when primary is energised. CT accuracy class: 0.1, 0.2, 0.5, 1, 3, 5 (% error at rated current). Metering CTs use classes 0.1–0.5; protection CTs use class 5P, 10P with high saturation knee point.
Q139
Explanation
OFDM (Orthogonal Frequency Division Multiplexing): Transmits data by splitting it across many closely spaced orthogonal subcarriers, each carrying a low data rate. Implemented efficiently using IFFT (transmitter) and FFT (receiver).
Advantages:
• Robust against multipath fading (cyclic prefix eliminates ISI).
• Efficient spectral use — subcarriers are orthogonal (don’t interfere).
• Easy equalization — each subcarrier is flat fading (simple 1-tap equalizer).
• Scales to very high bandwidths (LTE: 20 MHz, 5G NR: up to 400 MHz).
Advantages:
• Robust against multipath fading (cyclic prefix eliminates ISI).
• Efficient spectral use — subcarriers are orthogonal (don’t interfere).
• Easy equalization — each subcarrier is flat fading (simple 1-tap equalizer).
• Scales to very high bandwidths (LTE: 20 MHz, 5G NR: up to 400 MHz).
OFDM is used in: LTE/4G, 5G NR, Wi-Fi (802.11a/g/n/ac/ax), DVB-T (digital TV), ADSL, WiMAX. ISRO’s GSAT satellites carry transponders for 4G backhaul using OFDM-based technologies. The key mathematics is the IFFT/FFT pair — O(N log N) complexity makes it computationally feasible.
Q140
Explanation
Seebeck Effect: When two dissimilar metals are joined at two junctions maintained at different temperatures, an EMF is generated proportional to the temperature difference. This is the thermoelectric effect.
Types: K (Chromel-Alumel, −200 to 1260°C), J (Iron-Constantan, 0–760°C), T (Copper-Constantan, cryogenic), R/S (Platinum — high temperature).
V_EMF = α × (T_hot − T_cold) | α = Seebeck coefficient
Cold Junction Compensation (CJC): Thermocouple output depends on BOTH hot and cold junction temperatures. The cold junction (reference junction at measurement electronics) must be at a known temperature. CJC adds a correction voltage (measured by RTD or thermistor at cold junction) to give true hot junction temperature.
Types: K (Chromel-Alumel, −200 to 1260°C), J (Iron-Constantan, 0–760°C), T (Copper-Constantan, cryogenic), R/S (Platinum — high temperature).
K-type thermocouple is most common industrially (-200°C to +1260°C, sensitivity ~41 µV/°C). BARC uses thermocouples extensively for nuclear reactor core temperature monitoring. AD8495, MAX31855 are dedicated thermocouple interface ICs with built-in CJC.
Q141
Explanation
Analog Filter: Operates on continuous-time signals using R, L, C components or op-amps. Butterworth, Chebyshev, Bessel types.
Digital Filter: Operates on discrete-time sampled data using arithmetic operations (multiplications, additions, delays). Implemented in DSP, FPGA, microcontroller.
FIR (Finite Impulse Response): Output depends only on past and current inputs — no feedback. Always stable. Linear phase (constant group delay — important for audio and data comms). Can require many taps (hundreds) for sharp cutoff.
IIR (Infinite Impulse Response): Includes feedback (poles). Similar to analog filters (bilinear transformation). Fewer coefficients needed for same selectivity. Non-linear phase. Can be unstable if not designed carefully. Based on Butterworth, Chebyshev, Elliptic designs.
Digital Filter: Operates on discrete-time sampled data using arithmetic operations (multiplications, additions, delays). Implemented in DSP, FPGA, microcontroller.
FIR (Finite Impulse Response): Output depends only on past and current inputs — no feedback. Always stable. Linear phase (constant group delay — important for audio and data comms). Can require many taps (hundreds) for sharp cutoff.
IIR (Infinite Impulse Response): Includes feedback (poles). Similar to analog filters (bilinear transformation). Fewer coefficients needed for same selectivity. Non-linear phase. Can be unstable if not designed carefully. Based on Butterworth, Chebyshev, Elliptic designs.
FIR: preferred when linear phase is critical (ECG, audio, data recovery). IIR: preferred when computation efficiency matters and phase distortion is acceptable (audio equalisers, control systems). DRDO radar signal processors use both — FIR for pulse compression, IIR for clutter suppression filters.
Q142
Explanation
ADC (Analog-to-Digital Converter): Converts continuous analog signal to discrete digital code. Resolution in bits (8, 12, 16, 24 bit). Sampling rate in samples/second (kSPS, MSPS, GSPS).
DAC (Digital-to-Analog Converter): Converts digital code to analog voltage/current. Output waveform must be filtered (reconstruction filter) to remove staircase quantisation artifacts.
Key parameters:
• Resolution (N bits) → 2^N levels, LSB = V_ref/2^N
• INL (Integral Non-Linearity) — deviation from ideal transfer function
• DNL (Differential Non-Linearity) — step size uniformity
• SNR (Signal-to-Noise Ratio): ideal SNR = 6.02N + 1.76 dB for N-bit ADC
• SINAD, SFDR, ENOB (Effective Number of Bits)
DAC (Digital-to-Analog Converter): Converts digital code to analog voltage/current. Output waveform must be filtered (reconstruction filter) to remove staircase quantisation artifacts.
Key parameters:
• Resolution (N bits) → 2^N levels, LSB = V_ref/2^N
• INL (Integral Non-Linearity) — deviation from ideal transfer function
• DNL (Differential Non-Linearity) — step size uniformity
• SNR (Signal-to-Noise Ratio): ideal SNR = 6.02N + 1.76 dB for N-bit ADC
• SINAD, SFDR, ENOB (Effective Number of Bits)
ISRO’s IRNSS/NavIC satellite receivers use high-speed ADCs to digitise L5 & S-band signals. BARC uses high-resolution (24-bit) ADCs for nuclear detector signal integration. ADC selection: match resolution to required dynamic range, speed to signal bandwidth.
Q143
Explanation
Quantisation noise arises because ADC maps a continuous range of analog values to discrete digital codes. The error (difference between actual and quantised value) is at most ±½ LSB.
Oversampling and noise-shaping (sigma-delta ADCs) push quantisation noise out of the signal band, allowing higher ENOB than the raw bit count suggests.
SQNR = 6.02N + 1.76 dB (N = number of bits)
Each additional bit adds ~6 dB SNR improvement
Quantisation noise is modelled as uniformly distributed noise with RMS value = LSB/√12. For a 12-bit ADC: SQNR ≈ 74 dB. For 16-bit: SQNR ≈ 98 dB.Each additional bit adds ~6 dB SNR improvement
Oversampling and noise-shaping (sigma-delta ADCs) push quantisation noise out of the signal band, allowing higher ENOB than the raw bit count suggests.
Sigma-Delta (ΣΔ) ADCs: oversample by 64x–256x and use noise-shaping filter. Result: 24-bit effective resolution from 1-bit comparator. Used in precision instrumentation (BARC, weighing, audio). Successive approximation (SAR) ADCs: fast, moderate resolution (12–18 bit) — used in microcontrollers and ISRO data acquisition.
Q144
Explanation
EMC (Electromagnetic Compatibility): Ability of a device to function satisfactorily in its electromagnetic environment without causing unacceptable interference to others and without being susceptible to interference from others.
EMI (Electromagnetic Interference): The interference itself — disturbances that degrade performance. Can be conducted (through power/signal wires) or radiated (through air).
EMS (Electromagnetic Susceptibility): The susceptibility of a device to EMI — how much interference it can withstand.
Standards: CISPR, IEC 61000, MIL-STD-461 (defence), DO-160 (aerospace). India: BIS IS 13252.
EMI (Electromagnetic Interference): The interference itself — disturbances that degrade performance. Can be conducted (through power/signal wires) or radiated (through air).
EMS (Electromagnetic Susceptibility): The susceptibility of a device to EMI — how much interference it can withstand.
Standards: CISPR, IEC 61000, MIL-STD-461 (defence), DO-160 (aerospace). India: BIS IS 13252.
DRDO defence equipment must meet MIL-STD-461 (very stringent). ISRO spacecraft follow ECSS-E-20 EMC standards. EMI mitigation techniques: shielding (Faraday cage), filtering (ferrite beads, EMI filters), grounding, PCB layout (ground planes, trace impedance matching), cable routing separation.
Q145
Explanation
In space and nuclear environments, high-energy particles (protons, heavy ions, electrons, gamma rays) damage semiconductor devices causing:
1. TID (Total Ionising Dose): Cumulative charge buildup in oxide layers → shifts threshold voltages, increases leakage current, degrades performance.
2. SEE (Single Event Effects): Single particle strikes → SEU (bit flip in memory), SEL (latch-up — destructive), SET (transient glitch).
3. Displacement damage: Crystal lattice defects from neutron bombardment.
Rad-hard techniques: SOI (Silicon-on-Insulator) process, guard rings, triple-redundancy (TMR), EDAC for memories, specialised fab processes.
1. TID (Total Ionising Dose): Cumulative charge buildup in oxide layers → shifts threshold voltages, increases leakage current, degrades performance.
2. SEE (Single Event Effects): Single particle strikes → SEU (bit flip in memory), SEL (latch-up — destructive), SET (transient glitch).
3. Displacement damage: Crystal lattice defects from neutron bombardment.
Rad-hard techniques: SOI (Silicon-on-Insulator) process, guard rings, triple-redundancy (TMR), EDAC for memories, specialised fab processes.
ISRO uses radiation-hardened FPGAs (Microsemi RTAX), microprocessors (LEON3 SPARC), and memories for all satellite electronics. BARC designs radiation-tolerant ASICs for reactor instrumentation. Commercial-off-the-shelf (COTS) parts require qualification screening and shielding for use in radiation environments.
Q146
Explanation
SCADA (Supervisory Control And Data Acquisition): Distributed industrial control system for monitoring and controlling field devices at remote locations from a central control room.
Components: RTUs (Remote Terminal Units)/PLCs at field, communication network (fiber, radio, satellite), SCADA master station (HMI, historian, alarm management).
In NTPC power plants: SCADA monitors turbine parameters (speed, temperature, steam pressure), generator outputs (MW, MVAR, frequency), switchyard breaker status, transformer oil temperature, alarms, and provides operator control of set points.
Components: RTUs (Remote Terminal Units)/PLCs at field, communication network (fiber, radio, satellite), SCADA master station (HMI, historian, alarm management).
In NTPC power plants: SCADA monitors turbine parameters (speed, temperature, steam pressure), generator outputs (MW, MVAR, frequency), switchyard breaker status, transformer oil temperature, alarms, and provides operator control of set points.
Modern SCADA uses IEC 60870-5-101/104 (telecontrol), DNP3 protocols. Industrial networks: Modbus, PROFIBUS, IEC 61850 (substation automation). Cybersecurity (IEC 62443) is increasingly critical — SCADA cyberattacks (e.g., Stuxnet on nuclear facilities) highlight vulnerability. NTPC uses ABB/Siemens/GE SCADA platforms.
Q147
Explanation
Spread spectrum intentionally spreads the signal energy over a much wider bandwidth than the minimum required. Techniques: DSSS (Direct Sequence SS — XOR with PN code), FHSS (Frequency Hopping SS).
Processing gain: BW_spread/BW_original — determines how much the SNR is improved at the receiver (knowing the spreading code) vs a jammer who doesn’t know the code.
• Low probability of intercept (LPI): signal below noise floor — hard to detect.
• Anti-jam: jammer must cover entire spread bandwidth — much higher power needed to jam.
• Multiple access: CDMA — multiple users share same bandwidth using different PN codes.
• Precise ranging: GPS uses C/A and P(Y) DSSS codes for timing precision.
Processing gain: BW_spread/BW_original — determines how much the SNR is improved at the receiver (knowing the spreading code) vs a jammer who doesn’t know the code.
PG = 10 log(BW_spread / BW_data) dB
Why GPS/military use it:• Low probability of intercept (LPI): signal below noise floor — hard to detect.
• Anti-jam: jammer must cover entire spread bandwidth — much higher power needed to jam.
• Multiple access: CDMA — multiple users share same bandwidth using different PN codes.
• Precise ranging: GPS uses C/A and P(Y) DSSS codes for timing precision.
ISRO’s NavIC (IRNSS) uses BPSK-modulated spread spectrum on L5 (1176.45 MHz) and S-band (2492.08 MHz). DRDO’s tactical communication systems (TACT, AREN) use frequency-hopping spread spectrum for jam-resistant secure communications. Modern 5G NR also uses DSSS principles in its physical layer.
Q148
Explanation
Hall Effect: When current flows through a conductor (or semiconductor) in the presence of a perpendicular magnetic field, a voltage (Hall voltage) develops perpendicular to both current and field.
Advantages: Isolation (high-voltage measurement safely), DC and AC capable, fast response, wide range.
V_H = (I × B) / (n × e × d) [Volts]
Current measurement (clamp-on): A Hall sensor placed in the air gap of a magnetic core that surrounds the current-carrying conductor. The magnetic field in the gap is proportional to the current. Output voltage is proportional to current — no galvanic connection needed.
Advantages: Isolation (high-voltage measurement safely), DC and AC capable, fast response, wide range.
Hall effect sensors (ACS712, LEM LA series) are used in electric vehicle battery management, inverter current feedback loops, industrial drives (DRDO EV programs), solar inverter control, and BARC instrumentation for measuring beam currents in particle accelerators.
Q149
Explanation
SAW (Surface Acoustic Wave) Filter: Uses piezoelectric substrate (quartz, lithium niobate). Input electrode converts electrical signal to surface acoustic wave; output electrode reconverts. The device passband is determined by electrode geometry — extremely precise, stable center frequency.
Frequency range: 10 MHz to 3 GHz. Very sharp selectivity. Extremely small size (mm scale). No tuning needed. Excellent out-of-band rejection. Low insertion loss. Mass-produced at low cost.
Why preferred in RF: LC filters at GHz require impractically small inductors. SAW achieves high-Q bandpass filtering without external components — ideal for mobile phones, GPS, satellite receivers.
Frequency range: 10 MHz to 3 GHz. Very sharp selectivity. Extremely small size (mm scale). No tuning needed. Excellent out-of-band rejection. Low insertion loss. Mass-produced at low cost.
Why preferred in RF: LC filters at GHz require impractically small inductors. SAW achieves high-Q bandpass filtering without external components — ideal for mobile phones, GPS, satellite receivers.
Every smartphone contains multiple SAW filters — for GSM, LTE, Wi-Fi, GPS band selection. BEL manufactures SAW devices for defence radios and radar receivers. BAW (Bulk Acoustic Wave) filters extend this to 5G millimetre-wave frequencies. DRDO uses SAW-based channel filters in software-defined radios.
Q150
Explanation
The Haversine formula calculates the great-circle distance between two points on a sphere given their latitudes and longitudes.
• Antenna pointing: Ground station engineers use it to compute azimuth and elevation angles for dish antennas tracking satellites — critical for S-band and X-band telemetry/telecommand links.
• Link budget: Free-space path loss = 20log(d) + 20log(f) + 92.4 dB — distance d from Haversine.
• Doppler shift calculation: Rate of change of distance → Doppler frequency → important for tracking PSLV/GSLV during ascent.
• NavIC/GPS receiver algorithms: Navigation solution uses spherical geometry to compute position from pseudoranges.
a = sin²(Δφ/2) + cos φ₁ · cos φ₂ · sin²(Δλ/2)
d = 2R · arcsin(√a) [km]
Why an ISRO EE needs it:d = 2R · arcsin(√a) [km]
• Antenna pointing: Ground station engineers use it to compute azimuth and elevation angles for dish antennas tracking satellites — critical for S-band and X-band telemetry/telecommand links.
• Link budget: Free-space path loss = 20log(d) + 20log(f) + 92.4 dB — distance d from Haversine.
• Doppler shift calculation: Rate of change of distance → Doppler frequency → important for tracking PSLV/GSLV during ascent.
• NavIC/GPS receiver algorithms: Navigation solution uses spherical geometry to compute position from pseudoranges.
This interdisciplinary question tests whether you connect electrical/electronics knowledge to system-level engineering. ISRO interview often probes “spacecraft to ground station link establishment” — requiring RF knowledge (antenna gain, EIRP, G/T, SNR), orbital mechanics (satellite position, visibility window), and signal processing (ranging, Doppler) — all computed using spherical geometry starting from Haversine.
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