FE Electrical and Computer exam practice: cram pack

Formula sheets, the key method steps for every topic and 40 practice problems, with full solutions at the back.

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1Formulas and methods

Series & parallel resistors

Resistors in series
Req = R1 + R2 + …
Resistors in parallel
1/Req = 1/R1 + 1/R2 + …
Two in parallel
Req = R1R2 / (R1 + R2)
Ohm's law
V = I·R
Power
P = V·I = I²R = V²/R

Method

  1. Start at the end of the network furthest from the terminals.
  2. Combine resistors in series by adding them, and resistors in parallel with 1/R = 1/R₁ + 1/R₂ + …
  3. Redraw the circuit after each step.
  4. Repeat until one resistor is left between the terminals.

Nodal analysis

Kirchhoff’s current law
ΣIin = ΣIout
Branch current
I = (Va − Vb)/R
Reference node
Vground = 0

Method

  1. Choose a reference node (ground) and label the other node voltages.
  2. Write Kirchhoff’s current law at every unknown node: currents leaving through each branch equal the currents entering.
  3. Express every branch current as (Va − Vb)/R.
  4. Solve the system of equations, then find any current you need.

Mesh analysis

Kirchhoff’s voltage law
ΣV = 0 around every loop
Shared resistor
current = I1 − I2
Current source in a mesh
fixes that mesh current

Method

  1. Draw a clockwise current in every mesh (window) of the circuit.
  2. Apply Kirchhoff’s voltage law around each mesh: the sum of voltage drops is zero.
  3. In a resistor shared by two meshes the current is the difference of the two mesh currents.
  4. Solve the equations; a negative result means the current flows the other way.

Superposition

Superposition
x = x1 + x2 + … (one source at a time)
Switched-off voltage source
short circuit (0 V)
Switched-off current source
open circuit (0 A)
Voltage divider
V2 = V·R2/(R1 + R2)
Current divider
I1 = I·R2/(R1 + R2)

Method

  1. Count the independent sources. You will solve one simpler circuit per source.
  2. Keep one source and switch off the others: a voltage source becomes a short circuit (a wire), a current source becomes an open circuit (a gap).
  3. Solve the simpler circuit for the voltage or current you need, keeping track of its direction.
  4. Repeat for every source, then add the contributions with their signs.

Thévenin & Norton

Thévenin voltage
Vth = Vopen circuit
Thévenin resistance
Rth: all sources off, seen from a–b
Norton current
IN = Vth/Rth
Load current
IL = Vth/(Rth + RL)
Maximum power transfer
RL = Rth, Pmax = Vth²/(4Rth)

Method

  1. Remove the load and mark the two terminals a and b.
  2. Find the open-circuit voltage between a and b: this is Vth.
  3. Switch off all independent sources and find the resistance seen from a–b: this is Rth.
  4. Put the load back on the equivalent circuit: Vth in series with Rth.
  5. For the Norton equivalent, convert: IN = Vth/Rth, with RN = Rth in parallel.

RC & RL transients

Time constant
τ = RC | τ = L/R
Response
x(t) = x(∞) + [x(0) − x(∞)]·e−t/τ
Capacitor at DC
open circuit; vC cannot jump
Inductor at DC
short circuit; iL cannot jump
Settled
t ≈ 5τ

Method

  1. Find the initial value just after switching: a capacitor voltage and an inductor current cannot jump.
  2. Find the final value long after switching: a capacitor acts as an open circuit, an inductor as a short circuit.
  3. Find the time constant: τ = RC or τ = L/R, using the resistance seen by the capacitor or inductor.
  4. Use x(t) = x(∞) + [x(0) − x(∞)]·e−t/τ.

AC impedance & phasors

Impedances
ZR = R, ZL = jωL, ZC = 1/(jωC)
Angular frequency
ω = 2πf
Magnitude and angle
|Z| = √(R² + X²), φ = atan(X/R)
Phasor Ohm’s law
V = I·Z

Method

  1. Convert the frequency: ω = 2πf.
  2. Find each reactance: XL = ωL and XC = 1/(ωC).
  3. Add impedances like resistors, with Z = R + jX.
  4. Find the magnitude |Z| = √(R² + X²) and the angle φ = atan(X/R), then use Ohm’s law with phasors.

AC power & power factor

Real power
P = V·I·cos φ
Reactive power
Q = V·I·sin φ
Apparent power
S = V·I = √(P² + Q²)
Power factor
pf = cos φ = P/S
Correction capacitor
QC = P(tan φ1 − tan φ2), C = QC/(ωV²)

Three-phase power

Y connection
VL = √3·Vph, IL = Iph
Δ connection
VL = Vph, IL = √3·Iph
Total real power
P = √3·VL·IL·cos φ = 3·Iph²·R
Apparent and reactive power
S = √3·VL·IL, Q = P·tan φ
Correction capacitors
QC = P(tan φ1 − tan φ2), C = QC/(3ωV²)
Voltage across each capacitor
Δ: VL Y: VL/√3
Motor input
Pin = Pout/η

Transformers

Turns ratio
a = N1/N2 = V1/V2
Current ratio
I1/I2 = N2/N1 = 1/a
Rated current
I = S/V
Referred impedance
Z1′ = a²·ZL
Copper loss at part load
Pcu = x²·Pcu,fl
Efficiency
η = x·S·pf/(x·S·pf + Pcore + x²·Pcu,fl)
Maximum efficiency
x = √(Pcore/Pcu,fl)

Op-amp circuits

Inverting amplifier
Vout = −(Rf/Rin)·Vin
Non-inverting amplifier
Vout = (1 + Rf/R1)·Vin
Summing amplifier
Vout = −Rf(V1/R1 + V2/R2)
Ideal op-amp
V+ = V−, Iin = 0

Diodes & transistors

Diode (constant drop)
VD = 0.7 V when conducting
Active region
VBE = 0.7 V, IC = β·IB, IE = (β + 1)·IB
Fixed bias
IB = (VCC − 0.7)/RB
Divider bias
IB = (VTH − 0.7)/(RTH + (β + 1)RE)
Thévenin of the divider
VTH = VCC·R2/(R1 + R2), RTH = R1∥R2
Collector loop
VCE = VCC − ICRC − IERE
Saturation
IC(sat) = (VCC − VCE(sat))/RC, IB ≥ IC(sat)/β

Number systems

Place values
binary 2k, octal 8k, hex 16k
To decimal
Σ dk·bk
From decimal
divide by the base, read the remainders bottom-up
Hex ↔ binary
one hex digit = 4 bits
Two’s complement
invert the bits and add 1

Digital logic: gates, K-maps & flip-flops

Basic gates
A·B, A + B, A′, (A·B)′, (A + B)′, A ⊕ B
Boolean rules
X + X′ = 1, X·X′ = 0, X + XY = X, XY + XY′ = X
De Morgan
(X·Y)′ = X′ + Y′, (X + Y)′ = X′·Y′
Karnaugh map order
00, 01, 11, 10 (Gray code)
Group of 2ᵏ cells
loses k variables
4-to-1 multiplexer
F = A′B′I0 + A′BI1 + AB′I2 + ABI3
Flip-flops
D: Q⁺ = D, T: Q⁺ = T ⊕ Q, JK: Q⁺ = JQ′ + K′Q
Counters
n-bit: 2ⁿ states; mod-N: smallest n with 2ⁿ ≥ N; fout = fclk/N
Ripple counter
fmax = 1/(n·tpd)
Ring and Johnson counters
n and 2n states

Method

  1. For a circuit, work from the inputs to the output one gate at a time and write the value on every wire, or write its expression and fill in the truth table.
  2. For simplification, put the 1s (and the don’t-cares as X) into a Karnaugh map with Gray-code rows and columns: 00, 01, 11, 10.
  3. Cover the 1s with as few and as large groups of 1, 2, 4, 8 or 16 cells as possible, wrapping round the edges; each group is one product term made of the variables that stay constant. Group the 0s for the POS form.
  4. For flip-flops and counters, read the inputs at each active clock edge, write the state after every edge, and remember that an n-bit counter wraps round after 2ⁿ states.

Stability: Routh–Hurwitz & root locus

Stability
all roots of the characteristic polynomial in the left half-plane
Routh array, s¹ entry of a cubic
b1 = (a2a1 − a3a0)/a2
Right half-plane roots
number of sign changes in the first column
Cubic s³ + a₂s² + a₁s + a₀
stable when all a > 0 and a₂·a₁ > a₀
K/(s(s + a)(s + b))
Kmax = ab(a + b), ω = √(ab)
Characteristic equation
1 + K·G(s) = 0
Asymptotes
σa = (Σp − Σz)/(n − m), θ = (2q + 1)·180°/(n − m)
Break-away and break-in points
dK/ds = 0
Magnitude condition
K = 1/|G(s)|
Angle of departure
θd = 180° − Σ∠(from other poles) + Σ∠(from zeros)

Method

  1. Write the closed-loop characteristic polynomial: the denominator of 1 + K·G(s) = 0, multiplied out.
  2. Put the coefficients alternately into the first two rows of the Routh array and build the remaining rows.
  3. Count the sign changes in the first column: each one is a pole in the right half-plane. With K in the array, demand that every first-column entry stays positive.
  4. For a root locus, mark the poles and zeros, the real-axis segments, the asymptotes from the centroid and the break points where dK/ds = 0. Use K = 1/|G(s)| for the gain at a point.

Steady-state error & PID control

System type
number of poles of G(s) at s = 0
Error constants
Kp = lim G(s), Kv = lim s·G(s), Ka = lim s²·G(s) (s → 0)
Step A
ess = A/(1 + Kp)
Ramp A·t
ess = A/Kv
Parabola A·t²/2
ess = A/Ka
PID controller
C(s) = Kp + Ki/s + Kd·s
Second-order target
s² + 2ζωns + ωn²
Overshoot and timing
%OS = 100·e−ζπ/√(1−ζ²), tp = π/ωd, ts ≈ 4/(ζωn)

Method

  1. Count the poles of the open loop C(s)·G(s) at s = 0: that is the system type.
  2. Work out the error constant that matches the input: Kp for a step, Kv for a ramp, Ka for a parabola.
  3. Apply ess = A/(1 + Kp), A/Kv or A/Ka, or solve it for the gain you need.
  4. For a damping or speed specification, write the closed-loop characteristic polynomial and match it with s² + 2ζω_n·s + ω_n².

2Practice problems

1.Series & parallel resistorsMedium
R1​ = 2 ΩIR1​R3​ = 2 Ω+−V1​15 VR2​3 ΩAR4​4 ΩB

Find the current IR1 delivered by the source, which flows through R1.

V1 = 15 VR1 = 2 ΩR2 = 3 ΩR3 = 2 ΩR4 = 4 Ω
IR1 = A
2.Series & parallel resistorsHard
R1​ = 10 ΩR3​ = 25 ΩR5​ = 6 Ω+−V1​12 VR2​15 ΩIR2​AR4​10 ΩBR6​12 Ω

Find the current IR2 through R2.

V1 = 12 VR1 = 10 ΩR2 = 15 ΩR3 = 25 ΩR4 = 10 ΩR5 = 6 ΩR6 = 12 Ω
IR2 = A
3.Nodal analysisMedium
R1​ = 6 ΩR3​ = 12 Ω+−V1​6 VR2​20 ΩAR4​20 ΩBIs​4 A

Use nodal analysis to find the node voltage VB (measured from ground).

V1 = 6 VIs = 4 AR1 = 6 ΩR2 = 20 ΩR3 = 12 ΩR4 = 20 Ω
VB = V
4.Nodal analysisHard
R1​ = 6 ΩIR1​R2​ = 3 ΩR4​ = 20 Ω+−V1​18 VR3​2 ΩAR5​20 ΩBIs​2 A+−V2​30 V

Use nodal analysis to find the current IR1 through R1 in the direction of the arrow.

V1 = 18 VIs = 2 AV2 = 30 VR1 = 6 ΩR2 = 3 ΩR3 = 2 ΩR4 = 20 ΩR5 = 20 Ω
IR1 = A
5.Mesh analysisMedium
R1​ = 5 ΩR2​ = 3 ΩIR2​+−V1​6 VR3​6 ΩA+−V2​30 VI1​I2​

Use mesh analysis to find the current IR2 through R2 in the direction of the arrow.

V1 = 6 VV2 = 30 VR1 = 5 ΩR2 = 3 ΩR3 = 6 Ω
IR2 = A
6.Mesh analysisHard
R1​ = 15 ΩR2​ = 4 ΩIR2​R3​ = 20 Ω+−V1​9 VR4​5 ΩAR5​25 ΩB+−V2​10 VI1​I2​I3​

Use mesh analysis to find the current IR2 through R2 in the direction of the arrow.

V1 = 9 VV2 = 10 VR1 = 15 ΩR2 = 4 ΩR3 = 20 ΩR4 = 5 ΩR5 = 25 Ω
IR2 = A
7.SuperpositionMedium
R1​ = 4 ΩR3​ = 2 ΩIR3​+−V1​15 VR2​12 ΩAR4​20 ΩBIs​5 A

Use superposition to find the power PR3 absorbed by R3.

V1 = 15 VIs = 5 AR1 = 4 ΩR2 = 12 ΩR3 = 2 ΩR4 = 20 Ω
PR3 = W
8.SuperpositionHard
R1​ = 8 ΩR2​ = 2 ΩR4​ = 6 Ω+−V1​9 VR3​6 ΩIR3​AIs​2 AB+−V2​30 V

Use superposition to find the power PR3 absorbed by R3.

V1 = 9 VIs = 2 AV2 = 30 VR1 = 8 ΩR2 = 2 ΩR3 = 6 ΩR4 = 6 Ω
PR3 = W
9.Thévenin & NortonMedium
R1​ = 3 ΩR3​ = 8 Ω+−V1​15 VR2​2 ΩAab

Find the Norton current IN: the current that flows from a to b if the terminals are shorted.

V1 = 15 VR1 = 3 ΩR2 = 2 ΩR3 = 8 Ω
IN = A
10.Thévenin & NortonHard
R1​ = 30 ΩR3​ = 20 Ω+−V1​12 VR2​5 ΩAIs​4 ABRL​4 ΩIL​

A load RL = 4 Ω is connected across a–b. Use a Thévenin equivalent to find the power PL delivered to the load.

V1 = 12 VIs = 4 AR1 = 30 ΩR2 = 5 ΩR3 = 20 ΩRL = 4 Ω
PL = W
11.RC & RL transientsMedium
+−Vs​12 Vt = 0R = 10 ΩL47 mHi(t)

The inductor carries no current before the switch closes at t = 0. How long after the switch closes does the current reach 99% of its final value? Find t.

Vs = 12 VR = 10 ΩL = 47 mH
t = ms
12.RC & RL transientsHard
+−Vs​9 Vopens at t = 0R1​ = 3.3 kΩR2​ = 4.7 kΩi2​C33 µF+−vC​

The switch has been closed for a long time, so the circuit is in steady state. At t = 0 the switch opens. Find the current i2 through R2 at t = 50 ms.

Vs = 9 VR1 = 3.3 kΩR2 = 4.7 kΩC = 33 µFt = 50 ms
i2 = mA
13.AC impedance & phasorsMedium
Vf0​ = 100 HzRL = ?C = 22 µF

A series RLC circuit with C = 22 µF must resonate at 100 Hz. Find the inductance L needed.

f0 = 100 HzC = 22 µF
L = mH
14.AC impedance & phasorsHard
VfR = 50 ΩL = 10 mHC = 0.047 µF

A series RLC circuit has R = 50 Ω, L = 10 mH and C = 0.047 µF. Find its bandwidth B (the width of the band between the half-power frequencies), in Hz.

R = 50 ΩL = 10 mHC = 0.047 µF
B = Hz
15.AC power & power factorMedium
P = 23 kWQ = ?Sφ

A single-phase motor takes 23 kW at a power factor of 0.85 lagging from a 230 V supply. Find the reactive power Q it draws.

P = 23 kWpf = 0.85V = 230 V
Q = kvar
16.AC power & power factorHard
P1​ = 125 kWQ1​S1​φ

A 200 kVA single-phase transformer supplies a load of 125 kW at a power factor of 0.75 lagging. How much extra real power ΔP can be added as a resistive (unity power factor) load before the transformer reaches its kVA rating?

Smax = 200 kVAP1 = 125 kWpf1 = 0.75
ΔP = kW
17.Three-phase powerMedium
ABCVL​ = 208 VNZ = 3 + j4 Ωper phase

A balanced Y-connected load with an impedance of 3 + j4 Ω per phase is connected to a balanced three-phase supply with a line-to-line voltage of 208 V. Find the total real power P absorbed by the load in kW.

VL = 208 VZ = 3 + j4 Ω per phase
P = kW
18.Three-phase powerHard
P = 120 kWφ1​S1​Q2​QC​

A balanced three-phase load takes 120 kW at a power factor of 0.7 lagging from a 690 V (line-to-line), 50 Hz supply. A three-phase capacitor bank in parallel with the load must raise the overall power factor to 0.95 lagging. The real power stays the same. The capacitors are connected in Δ. Find the capacitance Cph of each capacitor in µF.

P = 120 kWpf1 = 0.7pf2 = 0.95VL = 690 Vf = 50 Hz
Cph = µF
19.TransformersMedium
RL​ = 40 Ω1012300 VV2​I1​ = ?I2​

An ideal transformer with a turns ratio N₁:N₂ = 10:1 has 2300 V applied to its primary winding. A 40 Ω resistor is connected across the secondary winding. Find the primary current I1.

N1:N2 = 10:1V1 = 2300 VRL = 40 Ω
I1 = A
20.TransformersHard
pf 0.95200 kVA, η = 96%

A single-phase 200 kVA transformer has a core loss of 800 W. At rated load and a power factor of 0.95 lagging its efficiency is 96%. Find the full-load copper loss Pcu,fl in watts.

S = 200 kVAPcore = 800 Wpf = 0.95η = 96%
Pcu,fl = W
21.Op-amp circuitsMedium
−+Vout​Rf​ = ?R1​ = 22 kΩVin​

Choose the feedback resistor Rf that gives this non-inverting amplifier a voltage gain of 6.

R1 = 22 kΩAv = 6
Rf = kΩ
22.Op-amp circuitsHard
−+Vout​Rf​ = 10 kΩV1​ = −1.1 VR1​ = 47 kΩV2​ = 0.4 VR2​ = 1 kΩ

The summing amplifier uses an ideal op-amp with ±15 V supplies. Find the output voltage Vout.

V1 = −1.1 VV2 = 0.4 VR1 = 47 kΩR2 = 1 kΩRf = 10 kΩ
Vout = V
23.Diodes & transistorsMedium
+−12 V100 Ω3.3 V680 ΩIZ​ = ?

A 3.3 V Zener regulator is fed from 12 V through 100 Ω and supplies a 680 Ω load. Find the Zener current IZ.

Vin = 12 VVZ = 3.3 VR = 100 ΩRL = 680 Ω
IZ = mA
24.Diodes & transistorsHard
V (V)I (mA)0.7640Q = ?

A diode is modelled as 0.7 V in series with 10 Ω (it conducts above 0.7 V). It is in series with a 150 Ω resistor across a 6 V supply. Find the operating current ID where the diode line meets the load line.

Vs = 6 VR = 150 ΩV0 = 0.7 Vrd = 10 Ω
ID = mA
25.Number systemsMedium
8-bit two's complement?−128?64?32?16?8?4?2?1

Write −87 as an 8-bit two's complement pattern. Read the pattern as an unsigned binary number: what is its value U in decimal?

N = −878 bit
U =
26.Number systemsHard
12-bit two's complement, N = ??sign???????????

What is the most negative integer N that can be stored in 12-bit two's complement?

12 bit
N =
27.Digital logic: gates, K-maps & flip-flopsMedium
ABCD000111100001111000011312040507161120131151141819011110

Use the Karnaugh map to find the minimal sum-of-products (SOP) form of F(A, B, C, D) = Σm(2, 3, 6, 8, 9, 10, 12, 14, 15). How many product terms N does it have?

F(A, B, C, D) = Σm(2, 3, 6, 8, 9, 10, 12, 14, 15)
N =
28.Digital logic: gates, K-maps & flip-flopsHard
ABCD00011110000111101011X3X20405X7161120131150140819X11110

Find the minimal SOP form of F(A, B, C, D) = Σm(0, 1, 6, 9, 10, 12, 15) + d(2, 3, 7, 11), where d marks the don't-care conditions. How many product terms N does it have?

F(A, B, C, D) = Σm(0, 1, 6, 9, 10, 12, 15) + d(2, 3, 7, 11)
N =
29.Laplace transformsMedium
t (s)f(t)t = 0.3f(0.3) = ?

Find f(t) for F(s) = 10/(s(s + 2)(s + 4)) by partial fractions, and evaluate f(0.3).

F(s) = 10/(s(s + 2)(s + 4))t = 0.3 s
f(0.3) =
30.Laplace transformsHard
ReIm−0.5−1−1.5−2−2.5−3−3.5−4−4.50.51

A system is described by the differential equation y″ + 3y′ + 2y = 2u′ + 8u, with input u(t) and output y(t). Find its transfer function G(s) = Y(s)/U(s) (zero initial conditions) and evaluate the impulse response g(t) at t = 0.8 s. Find g(0.8).

y″ + 3y′ + 2y = 2u′ + 8ut = 0.8 s
g(0.8) =
31.Block diagramsMedium
R(s)+7K+2s + 7G(s)C(s)5H₁−−

The plant G(s) = 2/(s + 7) has an inner (minor) negative feedback loop with gain H₁ = 5. A controller gain K = 7 and an outer unity negative feedback loop close the system. Find the closed-loop DC gain T(0).

G(s) = 2/(s + 7)H₁ = 5K = 7
T(0) =
32.Block diagramsHard
R(s)+20controller+D(s)+9s + 1plantC(s)−

A proportional controller K = 20 drives the plant G(s) = 9/(s + 1) in a unity negative feedback loop. A disturbance D enters at the plant input (it is added to the controller output). A reference step of size 5 and a disturbance step of size 5 are applied together. Find the steady-state output css.

K = 20G(s) = 9/(s + 1)D = 5R = 5
css =
33.Step responseMedium
t (s)y(t)1?

A system has the transfer function G(s) = 51/(s² + 10s + 51) and receives a unit step input. Find the percent overshoot %OS of the step response.

G(s) = 51/(s² + 10s + 51)
%OS = %
34.Step responseHard
+−5 VR = 62 ΩL = 500 mHC = 47 µFvC​

A series RLC circuit with R = 62 Ω, L = 500 mH and C = 47 µF is connected to a 5 V step at t = 0. The capacitor is uncharged and no current flows before the step. Find the time tp of the first voltage peak, in ms.

R = 62 ΩL = 500 mHC = 47 µFV = 5 V
tp = ms
35.Bode plots & marginsMedium
|H| (dB)0.11101001000−80−60−40−20020ω (rad/s)ω = 30

Find the exact magnitude |G(jω)| of G(s) = 360/((s + 3)(s + 20)) at ω = 30 rad/s, in dB.

G(s) = 360/((s + 3)(s + 20))ω = 30 rad/s
|G(jω)| = dB
36.Bode plots & marginsHard
|H| (dB)0.10.1111010100100−100−80−60−40−20020ω (rad/s)φ (°)ω (rad/s)−270−180−900ω180​

A unity-feedback loop has the open-loop transfer function L(s) = 2/(s(s + 1)(s + 2)). Find the gain margin GM in dB.

L(s) = 2/(s(s + 1)(s + 2))
GM = dB
37.Stability: Routh–Hurwitz & root locusMedium
R(s)+K1s(s + 5)(s + 8)C(s)−

The loop in the diagram has the open-loop transfer function L(s) = K/(s(s + 5)(s + 8)). Find the largest gain Kmax for which the closed loop is stable.

L(s) = K/(s(s + 5)(s + 8))
Kmax =
38.Stability: Routh–Hurwitz & root locusHard
ReIm−2−4−6−8−10−12j2

The root locus of L(s) = K/(s(s + 6)(s + 10)) leaves the real axis between s = 0 and s = −6. Find the break-away point sb.

L(s) = K/(s(s + 6)(s + 10))
sb =
39.Steady-state error & PID controlMedium
R(s)+K = 142s + 1C(s)−

A process G(s) = 4/(2s + 1) is controlled by a proportional gain K = 1 in a unity-feedback loop. Find the steady-state error ess for a step, as a percentage of the step size.

G(s) = 4/(2s + 1)K = 1
ess = %
40.Steady-state error & PID controlHard
R(s)+K1s(s + 4)C(s)−

A proportional controller K drives the plant G(s) = 1/(s(s + 4)) in a unity-feedback loop. Find the gain K that gives the closed loop a damping ratio ζ = 0.707.

G(s) = 1/(s(s + 4))ζ = 0.707
K =

3Solutions

1.Series & parallel resistors

Answer: IR1 = 3.75 A

Series and parallel resistors: in series the same current flows through each resistor and R = R₁ + R₂ + …. In parallel each resistor has the same voltage and 1/R = 1/R₁ + 1/R₂ + …. A ladder network is reduced one pair at a time until a single equivalent resistance remains.

R1​ = 2 ΩR3​ = 2 Ω+−V1​15 VR2​3 ΩAR4​4 ΩB

Combine resistors from the far end

Start at the end farthest from the source and work back towards it. Resistors carrying the same current are in series; resistors across the same two nodes are in parallel.

R3 + R4 = 2 + 4 = 6 Ω
R2 ∥ 6 = 3·6/(3+6) = 2 Ω
Req = R1 + 2 = 2 + 2 = 4 Ω

Current from the source

The source sees only Req, so Ohm’s law gives the current it delivers. That current flows through R₁.

IR1 = V1/Req = 15/4 = 3.75 A

Answer

IR1 = 3.75 A
2.Series & parallel resistors

Answer: IR2 = 0.4031 A

Series and parallel resistors: in series the same current flows through each resistor and R = R₁ + R₂ + …. In parallel each resistor has the same voltage and 1/R = 1/R₁ + 1/R₂ + …. A ladder network is reduced one pair at a time until a single equivalent resistance remains.

R1​ = 10 ΩR3​ = 25 ΩR5​ = 6 Ω+−V1​12 VR2​15 ΩAR4​10 ΩBR6​12 Ω

Combine resistors from the far end

Start at the end farthest from the source and work back towards it. Resistors carrying the same current are in series; resistors across the same two nodes are in parallel.

R5 + R6 = 6 + 12 = 18 Ω
R4 ∥ 18 = 6.429 Ω
R3 + 6.429 = 31.43 Ω
R2 ∥ 31.43 = 10.15 Ω
Req = R1 + 10.15 = 10 + 10.15 = 20.15 Ω

Current from the source

The source sees only Req, so Ohm’s law gives the current it delivers. That current flows through R₁.

IR1 = V1/Req = 12/20.15 = 0.5954 A

Current through R₂

Subtract the drop across R₁ to get the voltage at node A, which is the voltage across R₂.

VA = V1 − IR1·R1 = 12 − 0.5954·10 = 6.046 V
IR2 = VA/R2 = 6.046/15 = 0.4031 A

Answer

IR2 = 0.4031 A
3.Nodal analysis

Answer: VB = 38.82 V

Nodal analysis: choose a reference node, label the unknown node voltages, write Kirchhoff’s current law at each unknown node using Ohm’s law (I = ΔV/R), and solve the resulting equations.

R1​ = 6 ΩR3​ = 12 Ω+−V1​6 VR2​20 ΩAR4​20 ΩBIs​4 A

Set up the nodes

Ground is the bottom wire. Known node voltages come straight from the sources (V1 = 6 V). Unknowns: VA, VB.

KCL at node A

Currents leaving A through the resistors equal the current pushed into A by sources.

VA/R2 + (VA − V1)/R1 + (VA − VB)/R3 = 0
VA/20 + (VA − 6)/6 + (VA − VB)/12 = 0
0.3·VA − 0.08333·VB = 1

KCL at node B

Currents leaving B through the resistors equal the current pushed into B by sources.

VB/R4 + (VB − VA)/R3 = Is
VB/20 + (VB − VA)/12 = 4
−0.08333·VA + 0.1333·VB = 4

Solve

Δ = (0.3)(0.1333) − (−0.08333)(−0.08333) = 0.03306
VA = Δ1/Δ = 0.4667/0.03306 = 14.12 V
VB = Δ2/Δ = 1.283/0.03306 = 38.82 V

Answer

VB = 38.82 V
4.Nodal analysis

Answer: IR1 = 1.724 A

Nodal analysis: choose a reference node, label the unknown node voltages, write Kirchhoff’s current law at each unknown node using Ohm’s law (I = ΔV/R), and solve the resulting equations.

R1​ = 6 ΩR2​ = 3 ΩR4​ = 20 Ω+−V1​18 VR3​2 ΩAR5​20 ΩBIs​2 A+−V2​30 V

Set up the nodes

Ground is the bottom wire. Known node voltages come straight from the sources (V1 = 18 V, V2 = 30 V). Unknowns: VA, VB.

KCL at node A

Currents leaving A through the resistors equal the current pushed into A by sources.

VA/R3 + (VA − V1)/R1 + (VA − VB)/R2 = 0
VA/2 + (VA − 18)/6 + (VA − VB)/3 = 0
VA − 0.3333·VB = 3

KCL at node B

Currents leaving B through the resistors equal the current pushed into B by sources.

VB/R5 + (VB − VA)/R2 + (VB − V2)/R4 = Is
VB/20 + (VB − VA)/3 + (VB − 30)/20 = 2
−0.3333·VA + 0.4333·VB = 3.5

Solve

Δ = (1)(0.4333) − (−0.3333)(−0.3333) = 0.3222
VA = Δ1/Δ = 2.467/0.3222 = 7.655 V
VB = Δ2/Δ = 4.5/0.3222 = 13.97 V

Answer

IR1 = (V1 − VA)/R1 = (18 − 7.655)/6 = 1.724 A
5.Mesh analysis

Answer: IR2 = −4.667 A

Mesh analysis: give each window of a planar circuit its own loop current, write Kirchhoff’s voltage law around each loop (sum of drops = sum of rises), and solve. Branch currents are the mesh current, or the difference of two mesh currents on a shared branch.

R1​ = 5 ΩR2​ = 3 Ω+−V1​6 VR3​6 ΩA+−V2​30 VI1​I2​

Assign mesh currents

Draw a clockwise current in each window: I1, I2. A resistor shared by two meshes carries the difference of their currents.

KVL around mesh 1

Going clockwise, the voltage drops across resistors equal the source voltage rises (− to + in the direction of travel).

R1·I1 + R3(I1 − I2) = V1
5·I1 + 6(I1 − I2) = 6
11·I1 − 6·I2 = 6

KVL around mesh 2

Going clockwise, the voltage drops across resistors equal the source voltage rises (− to + in the direction of travel).

R2·I2 + R3(I2 − I1) = −V2
3·I2 + 6(I2 − I1) = (−30)
−6·I1 + 9·I2 = −30

Solve

Δ = (11)(9) − (−6)(−6) = 63
I1 = Δ1/Δ = −126/63 = −2 A
I2 = Δ2/Δ = −294/63 = −4.667 A

Answer

IR2 = I2 = −4.667 A

A negative mesh current flows anticlockwise.

6.Mesh analysis

Answer: IR2 = −0.1753 A

Mesh analysis: give each window of a planar circuit its own loop current, write Kirchhoff’s voltage law around each loop (sum of drops = sum of rises), and solve. Branch currents are the mesh current, or the difference of two mesh currents on a shared branch.

R1​ = 15 ΩR2​ = 4 ΩR3​ = 20 Ω+−V1​9 VR4​5 ΩAR5​25 ΩB+−V2​10 VI1​I2​I3​

Assign mesh currents

Draw a clockwise current in each window: I1, I2, I3. A resistor shared by two meshes carries the difference of their currents.

KVL around mesh 1

Going clockwise, the voltage drops across resistors equal the source voltage rises (− to + in the direction of travel).

R1·I1 + R4(I1 − I2) = V1
15·I1 + 5(I1 − I2) = 9
20·I1 − 5·I2 = 9

KVL around mesh 2

Going clockwise, the voltage drops across resistors equal the source voltage rises (− to + in the direction of travel).

R2·I2 + R4(I2 − I1) + R5(I2 − I3) = 0
4·I2 + 5(I2 − I1) + 25(I2 − I3) = 0
−5·I1 + 34·I2 − 25·I3 = 0

KVL around mesh 3

Going clockwise, the voltage drops across resistors equal the source voltage rises (− to + in the direction of travel).

R3·I3 + R5(I3 − I2) = −V2
20·I3 + 25(I3 − I2) = (−10)
−25·I2 + 45·I3 = −10

Solve

Δ = det of the coefficient matrix = 16975
I1 = Δ1/Δ = 6895/16975 = 0.4062 A
I2 = Δ2/Δ = −2975/16975 = −0.1753 A
I3 = Δ3/Δ = −5425/16975 = −0.3196 A

Answer

IR2 = I2 = −0.1753 A

A negative mesh current flows anticlockwise.

7.Superposition

Answer: PR3 = 25.2 W

Superposition: in a linear circuit, any voltage or current is the sum of the responses to each independent source acting alone. To switch a source off, replace an ideal voltage source with a short circuit and an ideal current source with an open circuit. Resistors stay where they are.

R1​ = 4 ΩR3​ = 2 Ω+−V1​15 VR2​12 ΩAR4​20 ΩBOPEN

Case 1 · V1 acting alone

Iₛ becomes an open circuit, so R₃ and R₄ form one series branch from A to ground, in parallel with R₂.

R3+R4 = 2+20 = 22 Ω
R2 ∥ (R3+R4) = 12·22/(12+22) = 7.765 Ω
VA = 15·7.765/(4+7.765) = 9.9 V
VB = VA·R4/(R3+R4) = 9.9·20/22 = 9 V
IR3′ = (VA − VB)/R3 = (9.9 − 9)/2 = 0.45 A
R1​ = 4 ΩR3​ = 2 ΩSHORTR2​12 ΩAR4​20 ΩBIs​5 A

Case 2 · Is acting alone

V₁ becomes a short, so R₁ is in parallel with R₂. Iₛ splits at B between R₄ and the path through R₃.

R1 ∥ R2 = 4·12/(4+12) = 3 Ω
Req = R4 ∥ (R3+R1∥R2) = 20 ∥ 5 = 4 Ω
VB = Is·Req = 5·4 = 20 V
VA = VB·(R1∥R2)/(R3+R1∥R2) = 20·3/5 = 12 V
IR3″ = (VA − VB)/R3 = (12 − 20)/2 = −4 A

Add the current contributions

IR3 = IR3′ + IR3″ = 0.45 + (−4) = −3.55 A

Power in the resistor

Power depends on the square of the current, so it does not obey superposition: add the currents first, then square.

PR3 = IR3²·R3 = (−3.55)²·2 = 25.2 W

Answer

PR3 = 25.2 W

Adding the powers of the separate cases would give 32.4 W, which is wrong.

8.Superposition

Answer: PR3 = 39.02 W

Superposition: in a linear circuit, any voltage or current is the sum of the responses to each independent source acting alone. To switch a source off, replace an ideal voltage source with a short circuit and an ideal current source with an open circuit. Resistors stay where they are.

R1​ = 8 ΩR2​ = 2 ΩR4​ = 6 Ω+−V1​9 VR3​6 ΩAOPENBSHORT

Case 1 · V1 acting alone

V₂ becomes a short and Iₛ an open circuit. Seen from A, R₃ is in parallel with the series pair R₂+R₄.

R3 ∥ (R2+R4) = 6 ∥ 8 = 3.429 Ω
VA = 9·3.429/(8+3.429) = 2.7 V
VB = VA·R4/(R2+R4) = 2.7·6/8 = 2.025 V
IR3′ = (VA − 0)/R3 = (2.7 − 0)/6 = 0.45 A
R1​ = 8 ΩR2​ = 2 ΩR4​ = 6 ΩSHORTR3​6 ΩAIs​2 ABSHORT

Case 2 · Is acting alone

Both voltage sources become shorts. Iₛ splits at B between R₄ (now to ground) and R₂ in series with R₁ ∥ R₃.

R1 ∥ R3 = 3.429 Ω, so the left path is R2+3.429 = 5.429 Ω
Req = R4 ∥ 5.429 = 2.85 Ω
VB = Is·Req = 2·2.85 = 5.7 V
VA = VB·3.429/5.429 = 3.6 V
IR3″ = (VA − 0)/R3 = (3.6 − 0)/6 = 0.6 A
R1​ = 8 ΩR2​ = 2 ΩR4​ = 6 ΩSHORTR3​6 ΩAOPENB+−V2​30 V

Case 3 · V2 acting alone

V₁ becomes a short and Iₛ an open circuit. R₁ ∥ R₃ hangs from A, in series with R₂ back to B.

R1 ∥ R3 = 8·6/(8+6) = 3.429 Ω
VB = V2·(R2+R1∥R3)/(R4+R2+R1∥R3) = 30·5.429/11.43 = 14.25 V
VA = VB·(R1∥R3)/(R2+R1∥R3) = 14.25·3.429/5.429 = 9 V
IR3‴ = (VA − 0)/R3 = (9 − 0)/6 = 1.5 A

Add the current contributions

IR3 = IR3′ + IR3″ + IR3‴ = 0.45 + 0.6 + 1.5 = 2.55 A

Power in the resistor

Power depends on the square of the current, so it does not obey superposition: add the currents first, then square.

PR3 = IR3²·R3 = 2.55²·6 = 39.02 W

Answer

PR3 = 39.02 W

Adding the powers of the separate cases would give 16.88 W, which is wrong.

9.Thévenin & Norton

Answer: IN = 0.6522 A

Thévenin’s theorem: any linear two-terminal network behaves like a single voltage source Vth in series with a resistance Rth. Norton’s theorem gives the same network as a current source IN = Vth/Rth in parallel with Rth.

R1​ = 3 ΩR3​ = 8 ΩSHORTR2​2 ΩAabRth​

Find Rth with every source switched off

Replace voltage sources with shorts and current sources with opens, then look into the circuit from a–b.

R1 ∥ R2 = 3·2/(3+2) = 1.2 Ω
Rth = (R1 ∥ R2) + R3 = 1.2 + 8 = 9.2 Ω
R1​ = 3 ΩR3​ = 8 Ω+−V1​15 VR2​2 ΩAab+−Vth​

Find Vth, the open-circuit voltage

With a–b open, no current flows through R₃, so there is no drop across it and V_b = V_A. R₁ and R₂ form a voltage divider.

Vth = V1·R2/(R1+R2) = 15·2/(3+2) = 6 V
IN​0.6522 ARth​9.2 Ωab

Norton equivalent

A Norton source is the same circuit seen as a current source in parallel with R_th. Its current is the short-circuit current at a–b.

IN = Vth/Rth = 6/9.2 = 0.6522 A
10.Thévenin & Norton

Answer: PL = 48.86 W

Thévenin’s theorem: any linear two-terminal network behaves like a single voltage source Vth in series with a resistance Rth. Norton’s theorem gives the same network as a current source IN = Vth/Rth in parallel with Rth.

R1​ = 30 ΩR3​ = 20 ΩSHORTR2​5 ΩAOPENBabRth​

Find Rth with every source switched off

Replace voltage sources with shorts and current sources with opens, then look into the circuit from a–b.

R1 ∥ R2 = 30·5/(30+5) = 4.286 Ω
Rth = (R1 ∥ R2) + R3 = 4.286 + 20 = 24.29 Ω
R1​ = 30 ΩR3​ = 20 Ω+−V1​12 VR2​5 ΩAIs​4 ABab+−Vth​

Find Vth, the open-circuit voltage

With a–b open, the only path for Iₛ is through R₃ into node A. Find V_A by superposition of V₁ and Iₛ, then add the drop across R₃.

VA = V1·R2/(R1+R2) + Is·(R1∥R2) = 1.714 + 4·4.286 = 18.86 V
Vth = VB = VA + Is·R3 = 18.86 + 4·20 = 98.86 V
Rth​ = 24.29 Ω+−Vth​98.86 VRL​4 ΩIL​

Connect the load to the Thévenin equivalent

The Thévenin source and R_th in series behave exactly like the original circuit at a–b, so the load sees a simple series loop.

IL = Vth/(Rth + RL) = 98.86/(24.29 + 4) = 3.495 A
PL = IL²·RL = 3.495²·4 = 48.86 W
11.RC & RL transients

Answer: t = 21.64 ms

First-order transients: in a circuit with one capacitor or one inductor, every voltage and current moves exponentially from its initial value to its final value: x(t) = x(∞) + [x(0) − x(∞)]·e−t/τ, with τ = RC or τ = L/R. After about 5τ the circuit has settled.

Time constant and final current

Long after the switch closes the inductor behaves like a short circuit, so the final current is set by R alone.

τ = L/R = 47 mH / 10 Ω = 4.7 ms
i(∞) = Vs/R = 12/10 = 1.2 A

Solve for the time

0.99 = 1 − e−t/τ → t = −τ·ln(1 − 0.99)
t = −4.7·ln(0.01) = 21.64 ms

Answer

t = 21.64 ms
12.RC & RL transients

Answer: i2 = 0.815 mA

First-order transients: in a circuit with one capacitor or one inductor, every voltage and current moves exponentially from its initial value to its final value: x(t) = x(∞) + [x(0) − x(∞)]·e−t/τ, with τ = RC or τ = L/R. After about 5τ the circuit has settled.

Initial capacitor voltage

In steady state the capacitor is an open circuit, so R₁ and R₂ form a voltage divider. The capacitor voltage cannot jump when the switch opens.

vC(0) = 9·4.7/(3.3 + 4.7) = 5.288 V

Time constant after the switch opens

τ = R2·C = 4.7·33 = 155.1 ms

Discharge

vC(t) = 5.288·e−50/155.1 = 3.83 V
i2 = vC/R2 = 3.83/4.7 = 0.815 mA

Answer

i2 = 0.815 mA
13.AC impedance & phasors

Answer: L = 115.1 mH

AC circuits with phasors: resistors, inductors and capacitors have impedances R, jωL and 1/(jωC), with ω = 2πf. In series, impedances add like resistances, but as complex numbers. Rms current and voltage follow Ohm’s law with |Z|.

Resonance condition

At resonance the inductive and capacitive reactances cancel: ωL = 1/(ωC).

ω₀ = 2π·100 = 628.3 rad/s
L = 1/(ω₀²·C) = 1/(628.3²·22·10⁻⁶) = 115.1 mH

Answer

L = 115.1 mH
14.AC impedance & phasors

Answer: B = 795.8 Hz

AC circuits with phasors: resistors, inductors and capacitors have impedances R, jωL and 1/(jωC), with ω = 2πf. In series, impedances add like resistances, but as complex numbers. Rms current and voltage follow Ohm’s law with |Z|.

Resonant frequency

f0 = 1/(2π·√(0.01·0.047·10⁻⁶)) = 7341 Hz

Quality factor

Q compares the reactance at resonance with the resistance: Q = ω₀L/R.

Q = (1/R)·√(L/C) = (1/50)·√(0.01/(0.047·10⁻⁶)) = 9.225

Bandwidth

B = f0/Q = 7341/9.225 = 795.8 Hz

Answer

B = 795.8 Hz
15.AC power & power factor

Answer: Q = 14.25 kvar

AC power: apparent power S = V·I (VA) splits into real power P = S·cos φ (W), which does useful work, and reactive power Q = S·sin φ (var), which moves back and forth between source and load. The power factor is cos φ. A capacitor in parallel supplies reactive power locally, so the line current drops for the same real power.

Angle

φ = arccos(0.85) = 31.79°, tan φ = 0.6197

Reactive power

Q = P·tan φ = 23·0.6197 = 14.25 kvar

Answer

Q = 14.25 kvar
16.AC power & power factor

Answer: ΔP = 41.87 kW

AC power: apparent power S = V·I (VA) splits into real power P = S·cos φ (W), which does useful work, and reactive power Q = S·sin φ (var), which moves back and forth between source and load. The power factor is cos φ. A capacitor in parallel supplies reactive power locally, so the line current drops for the same real power.

Reactive power of the existing load

Q1 = 125·tan(arccos 0.75) = 110.2 kvar

Largest total real power

At full rating S = Smax, and Q is unchanged by the resistive load.

P = √(Smax² − Q1²) = √(200² − 110.2²) = 166.9 kW

Extra real power

ΔP = 166.9 − 125 = 41.87 kW

Answer

ΔP = 41.87 kW
17.Three-phase power

Answer: P = 5.192 kW

Balanced three-phase systems: in a Y (star) connection the line-to-line voltage is √3 times the phase voltage, VL = √3·Vph, and the line current equals the phase current. In a Δ (delta) connection the line-to-line voltage equals the phase voltage and the line current is √3 times the phase current, IL = √3·Iph. The total power is three times the power of one phase: P = 3·Vph·Iph·cos φ = √3·VL·IL·cos φ.

Phase voltage

Vph = 208/√3 = 120.1 V

Phase current

|Z| = √(3² + 4²) = 5 Ω
Iph = 120.1/5 = 24.02 A

Total real power

Only the resistive part of each impedance absorbs real power.

P = 3·Iph²·R = 3·24.02²·3 = 5.192 kW

Answer

P = 5.192 kW

Check: cos φ = R/|Z| = 0.6, and √3·VL·IL·cos φ gives the same power.

18.Three-phase power

Answer: Cph = 184.9 µF

Balanced three-phase systems: in a Y (star) connection the line-to-line voltage is √3 times the phase voltage, VL = √3·Vph, and the line current equals the phase current. In a Δ (delta) connection the line-to-line voltage equals the phase voltage and the line current is √3 times the phase current, IL = √3·Iph. The total power is three times the power of one phase: P = 3·Vph·Iph·cos φ = √3·VL·IL·cos φ. Power factor correction: capacitors supply reactive power locally, QC = P·(tan φ1 − tan φ2). Each of the three capacitors supplies QC/3 = V²·ω·C, where V is the voltage across that capacitor: VL in a Δ bank, VL/√3 in a Y bank.

Reactive power before and after

The real power is unchanged, so each power factor fixes the reactive power: Q = P·tan φ.

Q1 = 120·tan(acos 0.7) = 120·1.02 = 122.4 kvar
Q2 = 120·tan(acos 0.95) = 120·0.3287 = 39.44 kvar

Reactive power from the capacitors

QC = Q1 − Q2 = 82.98 kvar

Capacitance per phase

In a Δ bank each capacitor is connected between two lines.

V = 690 V, ω = 2π·50 = 314.2 rad/s
Cph = (QC/3)/(ω·V²) = 27661/(314.2·690²) = 184.9 µF

Answer

Cph = 184.9 µF
19.Transformers

Answer: I1 = 0.575 A

Ideal transformer: the voltages are in the ratio of the turns and the currents in the inverse ratio: V₁/V₂ = N₁/N₂ = a and I₁/I₂ = N₂/N₁ = 1/a, so the power in equals the power out, V₁·I₁ = V₂·I₂. A load impedance Z on the secondary looks like a²·Z from the primary.

Secondary voltage and current

V2 = 2300/10 = 230 V
I2 = 230/40 = 5.75 A

Primary current

An ideal transformer has no losses: V₁·I₁ = V₂·I₂.

I1 = I2/10 = 0.575 A

Answer

I1 = 0.575 A

Check: the load seen from the primary is a²·RL = 4000 Ω, and 2300/4000 gives the same current.

20.Transformers

Answer: Pcu,fl = 7117 W

Transformer losses: the core loss (hysteresis and eddy currents) depends on the voltage and is the same at any load. The copper loss in the windings goes with the current squared, so at a fraction x of rated load it is x²·Pcu,fl. Efficiency η = Pout/(Pout + Pcore + Pcu), with Pout = x·S·pf. The efficiency is highest at the load where the copper loss equals the core loss.

Output and input power

Pout = 200·0.95 = 190 kW
Pin = 190000/0.96 = 197917 W

Total and copper losses

Ploss = 197917 − 190000 = 7917 W
Pcu,fl = 7917 − 800 = 7117 W

Answer

Pcu,fl = 7117 W
21.Op-amp circuits

Answer: Rf = 110 kΩ

Ideal op-amp rules: with negative feedback, the op-amp drives its output so that its two inputs sit at the same voltage (V₋ = V₊), and no current flows into either input. Writing KCL at the inverting input with these two facts gives the output.

Gain of a non-inverting amplifier

V₋ = V₊ = Vin, and the current through R₁ also flows through Rf, so Vout = Vin·(1 + Rf/R₁).

Av = 1 + Rf/R1
Rf = (6 − 1)·22 = 110 kΩ

Answer

Rf = 110 kΩ
22.Op-amp circuits

Answer: Vout = −3.766 V

Ideal op-amp rules: with negative feedback, the op-amp drives its output so that its two inputs sit at the same voltage (V₋ = V₊), and no current flows into either input. Writing KCL at the inverting input with these two facts gives the output.

Input currents

V₋ = 0, so each input resistor has its full input voltage across it.

I1 = V1/R1 = −1.1/47 = −0.0234 mA
I2 = V2/R2 = 0.4/1 = 0.4 mA
If = I1 + I2 = 0.3766 mA

Output voltage

Vout = −Rf·If = −10·0.3766 = −3.766 V

Answer

Vout = −3.766 V
23.Diodes & transistors

Answer: IZ = 82.15 mA

Zener regulator: a reverse-biased Zener diode holds its voltage VZ while its current stays above a minimum IZ,min. The series resistor R takes the difference between input and output: IR = (Vin − VZ)/R. That current splits between the load, IL = VZ/RL, and the Zener: IZ = IR − IL. Design for the worst cases: the lowest input with the largest load must still leave IZ,min, and the highest input with no load gives the largest Zener power PZ = VZ·IZ.

Resistor current

IR = 8.7/100 = 87 mA

Load current

IL = 3.3/680 = 4.853 mA

Zener current

IZ = 87 − 4.853 = 82.15 mA

Answer

IZ = 82.15 mA
24.Diodes & transistors

Answer: ID = 33.13 mA

LED and diode circuits: a forward-biased LED drops roughly its forward voltage VF (about 2 V for red, 3 V for blue or white), whatever the current. A series resistor sets the current: R = (Vs − n·VF)/I for n LEDs in series. With a more exact diode model V = V₀ + I·rd, the operating point is where the diode line meets the load line I = (Vs − V)/R, so I = (Vs − V₀)/(R + rd).

Combine the two equations

6 = 0.7 + I·(150 + 10)

Operating current

ID = 5.3/160 = 33.13 mA
VD = 0.7 + 0.03313·10 = 1.031 V

Answer

ID = 33.13 mA
25.Number systems

Answer: U = 169

Positional number systems: each digit is worth its value times a power of the base. In binary the places are worth 1, 2, 4, 8, 16, …; in hexadecimal 1, 16, 256, …, with A–F standing for 10–15. In 8-bit two's complement the leftmost bit is worth −128 instead of +128, which is how negative numbers are stored.

Invert and add one

87 = 0101 0111
inverted: 1010 1000
+1 → 1010 1001

Read it as unsigned

1010 1001₂ = 256 − 87 = 169

Answer

U = 169
26.Number systems

Answer: N = −2048

Positional number systems: each digit is worth its value times a power of the base. In binary the places are worth 1, 2, 4, 8, 16, …; in hexadecimal 1, 16, 256, …, with A–F standing for 10–15. In 8-bit two's complement the leftmost bit is worth −128 instead of +128, which is how negative numbers are stored.

Most negative value

−211 = −2048

Answer

N = −2048
27.Digital logic: gates, K-maps & flip-flops

Answer: N = 5

Karnaugh maps: the cells are ordered in Gray code (00, 01, 11, 10), so neighbouring cells, including the ones across the edges, differ in exactly one variable. Group the 1s in rectangles of 1, 2, 4, 8 or 16 cells, as large as possible and as few as possible, until every 1 is covered. Each group is one product term: the variables that stay constant inside it. A group of 2ᵏ cells loses k variables. Don't-cares (X) may be used to make groups bigger but never have to be covered. Grouping the 0s instead gives the minimal POS form.

ABCD000111100001111000011312040507161120131151141819011110

Group the 1s

Every group is a rectangle of 2ᵏ cells; edge cells are neighbours of the cells on the opposite edge.

CD′
AD′
A′B′C
AB′C′
ABC

Minimal SOP form

F = CD′ + AD′ + A′B′C + AB′C′ + ABC
N = 5

Answer

N = 5
28.Digital logic: gates, K-maps & flip-flops

Answer: N = 6

Karnaugh maps: the cells are ordered in Gray code (00, 01, 11, 10), so neighbouring cells, including the ones across the edges, differ in exactly one variable. Group the 1s in rectangles of 1, 2, 4, 8 or 16 cells, as large as possible and as few as possible, until every 1 is covered. Each group is one product term: the variables that stay constant inside it. A group of 2ᵏ cells loses k variables. Don't-cares (X) may be used to make groups bigger but never have to be covered. Grouping the 0s instead gives the minimal POS form.

Prime implicants

The largest groups that can be formed from 1s and Xs.

CD, B′D, B′C, A′C, A′B′, ABC′D′
ABCD00011110000111101011X3X20405X7161120131150140819X11110

Minimal cover

F = CD + B′D + B′C + A′C + A′B′ + ABC′D′
N = 6

Answer

N = 6
29.Laplace transforms

Answer: f(0.3) = 0.2545

Laplace transform: F(s) = ∫₀∞ f(t)·e−st dt turns derivatives into multiplications by s: ℒ{f′} = sF(s) − f(0), ℒ{f″} = s²F(s) − s·f(0) − f′(0). Standard pairs: 1 ↔ 1/s, e−at ↔ 1/(s + a), t·e−at ↔ 1/(s + a)², sin ωt ↔ ω/(s² + ω²), cos ωt ↔ s/(s² + ω²), and a shift s → s + σ multiplies the time function by e−σt. To invert a rational F(s), split it into partial fractions: the residue of a simple pole p is A = [(s − p)·F(s)] at s = p. Final value theorem: f(∞) = lims→0 s·F(s), valid only when all poles of s·F(s) lie in the left half-plane. Initial value theorem: f(0⁺) = lims→∞ s·F(s).

Partial fractions

F(s) = A/s + B/(s + 2) + C/(s + 4)
A = 10/(2·4) = 1.25
B = 10/((−2)·2) = −2.5
C = 10/((−4)·(−2)) = 1.25

Inverse transform

f(t) = 1.25 − 2.5·e−2t + 1.25·e−4t

Evaluate

f(0.3) = 1.25 − 2.5·e−2·0.3 + 1.25·e−4·0.3 = 0.2545

Answer

f(0.3) = 0.2545
30.Laplace transforms

Answer: g(0.8) = 1.888

Laplace transform: F(s) = ∫₀∞ f(t)·e−st dt turns derivatives into multiplications by s: ℒ{f′} = sF(s) − f(0), ℒ{f″} = s²F(s) − s·f(0) − f′(0). Standard pairs: 1 ↔ 1/s, e−at ↔ 1/(s + a), t·e−at ↔ 1/(s + a)², sin ωt ↔ ω/(s² + ω²), cos ωt ↔ s/(s² + ω²), and a shift s → s + σ multiplies the time function by e−σt. To invert a rational F(s), split it into partial fractions: the residue of a simple pole p is A = [(s − p)·F(s)] at s = p. Final value theorem: f(∞) = lims→0 s·F(s), valid only when all poles of s·F(s) lie in the left half-plane. Initial value theorem: f(0⁺) = lims→∞ s·F(s).

Transfer function

G(s) = Y(s)/U(s) = (2s + 8)/(s² + 3s + 2)

Partial fractions

s² + 3s + 2 = (s + 1)(s + 2)
A = 6, B = −4

Impulse response

g(t) = 6·e−t − 4·e−2t
g(0.8) = 1.888

Answer

g(0.8) = 1.888
31.Block diagrams

Answer: T(0) = 0.4516

Block-diagram algebra: blocks in series multiply (G₁·G₂), blocks in parallel add (G₁ + G₂), and a loop with forward path G and feedback path H reduces to T = G/(1 + G·H) for negative feedback and G/(1 − G·H) for positive feedback. Reduce inner loops first, then work outwards. The closed-loop poles are the roots of the characteristic equation 1 + G(s)H(s) = 0. For a stable loop, a step input of size A gives the steady-state output A·T(0); with unity feedback the steady-state error to a step is A/(1 + Kp) with Kp = G(0).

Inner loop

Gᵢ = G/(1 + G·H₁) = 2/(s + 7 + 2·5) = 2/(s + 17)

Outer loop

T(s) = K·Gᵢ/(1 + K·Gᵢ) = 14/(s + 17 + 14) = 14/(s + 31)

Result

T(0) = 14/31 = 0.4516

Answer

T(0) = 0.4516
32.Block diagrams

Answer: css = 5.221

Block-diagram algebra: blocks in series multiply (G₁·G₂), blocks in parallel add (G₁ + G₂), and a loop with forward path G and feedback path H reduces to T = G/(1 + G·H) for negative feedback and G/(1 − G·H) for positive feedback. Reduce inner loops first, then work outwards. The closed-loop poles are the roots of the characteristic equation 1 + G(s)H(s) = 0. For a stable loop, a step input of size A gives the steady-state output A·T(0); with unity feedback the steady-state error to a step is A/(1 + Kp) with Kp = G(0).

Transfer functions

C/D = G/(1 + K·G) = 9/(s + 1 + 180)
C/R = K·G/(1 + K·G) = 180/(s + 1 + 180)

Steady state

css = 5·180/181 + 5·9/181 = 5.221

Answer

css = 5.221

A larger K reduces the effect of the disturbance, but never to zero with a proportional controller.

33.Step response

Answer: %OS = 4.593 %

Step response: a first-order system G(s) = K/(τs + 1) answers a step of size U with y(t) = K·U·(1 − e−t/τ): it reaches 63.2 % of the final value K·U after one time constant τ and 98 % after 4τ. A second-order system G(s) = K·ωₙ²/(s² + 2ζωₙs + ωₙ²) has the poles s = −ζωₙ ± jωd with ωd = ωₙ√(1 − ζ²). For 0 < ζ < 1 the step response overshoots: percent overshoot %OS = 100·e−ζπ/√(1−ζ²), peak time tp = π/ωd, and the 2 % settling time ts ≈ 4/(ζωₙ). Compare the denominator with s² + 2ζωₙs + ωₙ² to read off ωₙ and ζ. For a mass–spring–damper ωₙ = √(k/m) and ζ = c/(2√(km)); for a series RLC circuit ωₙ = 1/√(LC) and ζ = (R/2)·√(C/L).

Compare with the standard form

The denominator must match s² + 2ζωₙs + ωₙ².

ωₙ² = 51 → ωₙ = 7.141 rad/s
2ζωₙ = 10 → ζ = 10/(2·7.141) = 0.7001

Result

%OS = 100·e−ζπ/√(1−ζ²) = 100·e−3.081 = 4.593 %

Answer

%OS = 4.593 %
34.Step response

Answer: tp = 15.97 ms

Step response: a first-order system G(s) = K/(τs + 1) answers a step of size U with y(t) = K·U·(1 − e−t/τ): it reaches 63.2 % of the final value K·U after one time constant τ and 98 % after 4τ. A second-order system G(s) = K·ωₙ²/(s² + 2ζωₙs + ωₙ²) has the poles s = −ζωₙ ± jωd with ωd = ωₙ√(1 − ζ²). For 0 < ζ < 1 the step response overshoots: percent overshoot %OS = 100·e−ζπ/√(1−ζ²), peak time tp = π/ωd, and the 2 % settling time ts ≈ 4/(ζωₙ). Compare the denominator with s² + 2ζωₙs + ωₙ² to read off ωₙ and ζ. For a mass–spring–damper ωₙ = √(k/m) and ζ = c/(2√(km)); for a series RLC circuit ωₙ = 1/√(LC) and ζ = (R/2)·√(C/L).

Natural frequency and damping ratio

ωₙ = 1/√(LC) = 1/√(0.5·4.7 × 10⁻⁵) = 206.3 rad/s
ζ = (R/2)·√(C/L) = (62/2)·√(4.7 × 10⁻⁵/0.5) = 0.3006

Result

ωd = 196.7 rad/s
tp = π/ωd = 15.97 ms

Answer

tp = 15.97 ms
35.Bode plots & margins

Answer: |G(jω)| = −9.599 dB

Frequency response: substitute s = jω in the transfer function. The magnitude in decibels is 20·log₁₀|H(jω)| and the phase is the sum of the angles of the numerator factors minus those of the denominator factors. A first-order RC or RL filter has its corner (−3 dB) frequency at ωc = 1/(RC) or R/L, and fc = ωc/(2π); a low-pass filter gives |H| = 1/√(1 + (ω/ωc)²) and φ = −atan(ω/ωc). In the asymptotic (straight-line) Bode plot each pole bends the magnitude down by 20 dB/decade at its corner frequency, each zero bends it up by 20 dB/decade, and an integrator 1/s gives −20 dB/decade at all frequencies. Gain crossover ωc: |L(jω)| = 1 (0 dB); phase margin PM = 180° + ∠L(jωc). Phase crossover ω180: ∠L(jω) = −180°; gain margin GM = −20·log₁₀|L(jω180)| dB. The closed loop is stable when both margins are positive.

Multiply the magnitudes

|G(j30)| = 360/(√(30² + 3²)·√(30² + 20²)) = 360/(30.15·36.06) = 0.3312

Result

20·log₁₀(0.3312) = −9.599 dB

Answer

|G(jω)| = −9.599 dB
36.Bode plots & margins

Answer: GM = 9.542 dB

Frequency response: substitute s = jω in the transfer function. The magnitude in decibels is 20·log₁₀|H(jω)| and the phase is the sum of the angles of the numerator factors minus those of the denominator factors. A first-order RC or RL filter has its corner (−3 dB) frequency at ωc = 1/(RC) or R/L, and fc = ωc/(2π); a low-pass filter gives |H| = 1/√(1 + (ω/ωc)²) and φ = −atan(ω/ωc). In the asymptotic (straight-line) Bode plot each pole bends the magnitude down by 20 dB/decade at its corner frequency, each zero bends it up by 20 dB/decade, and an integrator 1/s gives −20 dB/decade at all frequencies. Gain crossover ωc: |L(jω)| = 1 (0 dB); phase margin PM = 180° + ∠L(jωc). Phase crossover ω180: ∠L(jω) = −180°; gain margin GM = −20·log₁₀|L(jω180)| dB. The closed loop is stable when both margins are positive.

Phase crossover

(ω/1)·(ω/2) = 1 → ω180 = √(1·2) = 1.414 rad/s

Magnitude at phase crossover

|L(jω180)| = K/(ω·√(ω² + 1)·√(ω² + 4)) = K/(1·2·(1 + 2)) = K/6

Gain margin

GM = 20·log₁₀(6/2) = 9.542 dB

Answer

GM = 9.542 dB
37.Stability: Routh–Hurwitz & root locus

Answer: Kmax = 520

Routh–Hurwitz criterion: a linear system is stable when every root of its characteristic polynomial lies in the left half of the s-plane. Write the coefficients alternately into the first two rows of the Routh array. Each entry of a new row comes from the two rows above it; for a cubic a₃s³ + a₂s² + a₁s + a₀ the s¹ entry is b₁ = (a₂·a₁ − a₃·a₀)/a₂. The number of sign changes in the first column equals the number of roots in the right half-plane. With a gain K in the coefficients, every first-column entry must stay positive: the gain that makes the s¹ entry zero is the stability limit, and the s² row then gives the frequency of the sustained oscillation.

Characteristic equation

s³ + 13s² + 40s + K = 0

Routh array

s³: 1, 40
s²: 13, K
s¹: (13·40 − K)/13
s⁰: K

Conditions

Every entry of the first column must be positive.

K > 0
13·40 − K > 0 → K < 520

Answer

Kmax = 520

At K = 520 the closed loop oscillates at ω = √40 = 6.325 rad/s.

38.Stability: Routh–Hurwitz & root locus

Answer: sb = −2.427

Root locus: as the gain K goes from 0 to ∞, the closed-loop poles, the roots of 1 + K·G(s) = 0, move from the open-loop poles to the open-loop zeros or to infinity. A point on the real axis belongs to the locus when the number of real poles and zeros to its right is odd. The n − m branches that go to infinity follow asymptotes at the angles (2q + 1)·180°/(n − m), which start from the centroid σₐ = (Σ poles − Σ zeros)/(n − m). Branches leave or join the real axis where dK/ds = 0. The angle condition ∠G(s) = 180° fixes the shape, and the magnitude condition K = 1/|G(s)| gives the gain at any point of the locus.

Gain along the real axis

K(s) = −s(s + 6)(s + 10) = −(s³ + 16s² + 60s)

Stationary points

dK/ds = −(3s² + 32s + 60) = 0
s = (−32 ± √(1024 − 720))/6 = −2.427, −8.239

Pick the point on the locus

The locus lies on the real axis between 0 and −6; the other root is not on the locus.

sb = −2.427

Answer

sb = −2.427
39.Steady-state error & PID control

Answer: ess = 20 %

Steady-state error: in a unity-feedback loop with open-loop transfer function G(s) the error is E(s) = R(s)/(1 + G(s)), and by the final value theorem ess = lims→0 s·E(s). The system type is the number of poles of G(s) at s = 0. The error constants are Kp = lim G(s), Kv = lim s·G(s) and Ka = lim s²·G(s), all for s → 0. A step of size A gives ess = A/(1 + Kp), a ramp A·t gives A/Kv and a parabola A·t²/2 gives A/Ka. A type-0 loop follows a step with a finite error, a type-1 loop follows it exactly and a ramp with a finite error.

Position constant

Kp = 1·4 = 4

Step error

ess = 100/(1 + 4) = 20 %

Answer

ess = 20 %
40.Steady-state error & PID control

Answer: K = 8.002

P, PI and PID control: the controller C(s) = Kp + Ki/s + Kd·s acts on the error. A proportional gain makes the loop faster and reduces the error of a type-0 plant, but never removes it. The integral term adds a pole at s = 0: the system type rises by one, and a step is followed without error. The derivative term adds damping. To choose gains, write the closed-loop characteristic polynomial and compare it with s² + 2ζωns + ωn². Then %OS = 100·e−ζπ/√(1−ζ²), tp = π/ωd with ωd = ωn√(1 − ζ²), and ts ≈ 4/(ζωn).

Characteristic polynomial

s(s + 4) + 1K = s² + 4s + 1K

Natural frequency

2·0.707·ωₙ = 4 → ωₙ = 2.829 rad/s

Gain

1K = ωₙ² = 8.002 → K = 8.002

Answer

K = 8.002

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