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​ = 3 ΩR3​ = 10 Ω+−V1​12 VR2​6 ΩAR4​12 ΩB

Find the equivalent resistance Req seen by the source V1.

V1 = 12 VR1 = 3 ΩR2 = 6 ΩR3 = 10 ΩR4 = 12 Ω
Req = Ω
2.Series & parallel resistorsHard
R1​ = 8 ΩR3​ = 8 ΩR5​ = 12 Ω+−V1​9 VR2​30 ΩIR2​AR4​12 ΩBR6​6 Ω

Find the current IR2 through R2.

V1 = 9 VR1 = 8 ΩR2 = 30 ΩR3 = 8 ΩR4 = 12 ΩR5 = 12 ΩR6 = 6 Ω
IR2 = A
3.Nodal analysisMedium
R1​15 Ω+−V1​15 VR2​4 Ω+−V2​9 VI2​R3​8 Ω+−V3​24 VA

Three branches are connected between node A and ground, as shown. Use nodal analysis to find the current I2 in branch 2, flowing up into node A in the direction of the arrow.

V1 = 15 VR1 = 15 ΩV2 = 9 VR2 = 4 ΩV3 = 24 VR3 = 8 Ω
I2 = A
4.Nodal analysisHard
R1​ = 2 ΩR2​ = 15 ΩR4​ = 3 Ω+−V1​9 VR3​12 ΩAR5​4 ΩBIs​4 A+−V2​30 V

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

V1 = 9 VIs = 4 AV2 = 30 VR1 = 2 ΩR2 = 15 ΩR3 = 12 ΩR4 = 3 ΩR5 = 4 Ω
VA = V
5.Mesh analysisMedium
R1​ = 10 ΩR2​ = 4 Ω+−V1​18 VR3​8 ΩA+−V2​24 VI1​I2​

Use mesh analysis to find the mesh current I1 (clockwise).

V1 = 18 VV2 = 24 VR1 = 10 ΩR2 = 4 ΩR3 = 8 Ω
I1 = A
6.Mesh analysisHard
R1​ = 25 ΩR2​ = 2 ΩR3​ = 5 ΩIR3​+−V1​30 VR4​20 ΩAR5​2 ΩB+−V2​9 VI1​I2​I3​

Use mesh analysis to find the current IR3 through R3 in the direction of the arrow.

V1 = 30 VV2 = 9 VR1 = 25 ΩR2 = 2 ΩR3 = 5 ΩR4 = 20 ΩR5 = 2 Ω
IR3 = A
7.SuperpositionMedium
R1​ = 5 ΩR3​ = 20 ΩIR3​+−V1​9 VR2​20 ΩAR4​15 ΩBIs​?

Find the value of the current source Is (direction as shown) that makes the current IR3 through R3 equal to zero.

V1 = 9 VR1 = 5 ΩR2 = 20 ΩR3 = 20 ΩR4 = 15 Ω
Is = A
8.SuperpositionHard
R1​ = 20 ΩR2​ = 10 ΩR4​ = 3 ΩIR4​+−V1​10 VR3​20 ΩAIs​6 AB+−V2​9 V

Use superposition to find the current IR4 through R4 in the direction of the arrow.

V1 = 10 VIs = 6 AV2 = 9 VR1 = 20 ΩR2 = 10 ΩR3 = 20 ΩR4 = 3 Ω
IR4 = A
9.Thévenin & NortonMedium
R1​ = 8 ΩR3​ = 4 Ω+−V1​12 VR2​6 ΩARL​10 ΩIL​B

A load RL = 10 Ω is connected across a–b. Replace the rest of the circuit with its Thévenin equivalent and find the load current IL.

V1 = 12 VR1 = 8 ΩR2 = 6 ΩR3 = 4 ΩRL = 10 Ω
IL = A
10.Thévenin & NortonHard
R1​ = 10 ΩR3​ = 6 Ω+−V1​36 VR2​12 ΩAIs​1 ABab

Find the Thévenin voltage Vth seen from terminals a–b.

V1 = 36 VIs = 1 AR1 = 10 ΩR2 = 12 ΩR3 = 6 Ω
Vth = V
11.RC & RL transientsMedium
+−Vs​5 Vt = 0R = 50 ΩL220 mHi(t)

The inductor carries no current before the switch closes at t = 0. Find the voltage vL across the inductor at t = 5 ms.

Vs = 5 VR = 50 ΩL = 220 mHt = 5 ms
vL = V
12.RC & RL transientsHard
+−Vs​20 VR1​ = 20 ΩR2​ = 10 Ωopens at t = 0L47 mHi(t)

The switch across R2 has been closed for a long time, so the inductor current is steady. At t = 0 the switch opens. How long after t = 0 does the inductor current reach 0.767 A? Find t.

Vs = 20 VR1 = 20 ΩR2 = 10 ΩL = 47 mH
t = ms
13.AC impedance & phasorsMedium
100 V1000 HzR = 25 ΩL = 50 mHC = 100 µFI

A series RLC circuit is connected to a 100 V (rms), 1000 Hz supply. Find the rms current I.

V = 100 V (rms)f = 1000 HzR = 25 ΩL = 50 mHC = 100 µF
I = A
14.AC impedance & phasorsHard
5 Vf0​R = 50 ΩL = 100 mHC = 10 µF

A series RLC circuit is driven by a 5 V (rms) source whose frequency is set to the resonant frequency of the circuit. Find the rms voltage VL across the inductor.

V = 5 V (rms)R = 50 ΩL = 100 mHC = 10 µF
VL = V
15.AC power & power factorMedium
P = 34 kWQSφ

A single-phase motor takes 34 kW at a power factor of 0.9 lagging from a 230 V supply. Find the line current I.

P = 34 kWpf = 0.9V = 230 V
I = A
16.AC power & power factorHard
240 V50 Hzload17 kW, 0.7C100 µFI

A single-phase load takes 17 kW at a power factor of 0.7 lagging from a 240 V, 50 Hz supply. A 100 µF capacitor is connected in parallel with the load. Find the new power factor cos φ seen by the supply.

P = 17 kWpf1 = 0.7V = 240 Vf = 50 HzC = 100 µF
cos φ =
17.Three-phase powerMedium
ABCVL​ = 208 VNZ = 12 + j16 Ωper phase

A balanced Y-connected load with an impedance of 12 + j16 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 = 12 + j16 Ω per phase
P = kW
18.Three-phase powerHard
P = 300 kWφ1​S1​Q2​QC​

A balanced three-phase load takes 300 kW at a power factor of 0.8 lagging from a 480 V (line-to-line), 50 Hz supply. A three-phase capacitor bank in parallel with the load must raise the overall power factor to 0.92 lagging. The real power stays the same. The capacitors are connected in Y. Find the capacitance Cph of each capacitor in µF.

P = 300 kWpf1 = 0.8pf2 = 0.92VL = 480 Vf = 50 Hz
Cph = µF
19.TransformersMedium
RL​ = 12 Ω41480 VV2​I1​ = ?I2​

An ideal transformer with a turns ratio N₁:N₂ = 4:1 has 480 V applied to its primary winding. A 12 Ω resistor is connected across the secondary winding. Find the primary current I1.

N1:N2 = 4:1V1 = 480 VRL = 12 Ω
I1 = A
20.TransformersHard
pf 0.8575 kVA, 50% load

A single-phase 75 kVA transformer has a core loss of 375 W and a copper loss of 1125 W at rated load. It supplies 50% of its rated kVA at a power factor of 0.85 lagging. Find the total losses Ploss in watts at this load.

S = 75 kVAPcore = 375 WPcu,fl = 1125 Wx = 0.5pf = 0.85
Ploss = W
21.Op-amp circuitsMedium
−+Vout​Rf​ = 47 kΩR1​ = 10 kΩVin​ = −0.3 V

The op-amp is ideal and runs from ±15 V supplies. Find the output voltage Vout.

Vin = −0.3 VR1 = 10 kΩRf = 47 kΩ
Vout = V
22.Op-amp circuitsHard
−+Vout​Rf​ = 22 kΩV1​ = −1.6 VR1​ = 100 kΩV2​ = −1.6 VR2​ = 4.7 kΩ

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

V1 = −1.6 VV2 = −1.6 VR1 = 100 kΩR2 = 4.7 kΩRf = 22 kΩ
Vout = V
23.Diodes & transistorsMedium
+−9 VR = ?3 × 2 V10 mA

3 red LEDs (forward voltage 2 V each) are connected in series with a resistor to a 9 V supply. Find the resistance R that sets the current to 10 mA.

Vs = 9 VVF = 2 Vn = 3I = 10 mA
R = Ω
24.Diodes & transistorsHard
V (V)I (mA)0.6510.64Q = ?

A diode is modelled as 0.6 V in series with 25 Ω (it conducts above 0.6 V). It is in series with a 470 Ω resistor across a 5 V supply. Find the operating current ID where the diode line meets the load line.

Vs = 5 VR = 470 ΩV0 = 0.6 Vrd = 25 Ω
ID = mA
25.Number systemsMedium
8-bit two's complement0−12806403201608040201

Set the bits so they store −107 in 8-bit two's complement. Read as an unsigned number, what is the pattern's value U?

N = −1078 bit
U =
26.Number systemsHard
8 bit1 px1920 px1080 pxM = ? KiB

An uncompressed image is 1920 × 1080 pixels with 8 bits per pixel. How much memory M does it take, in KiB (1 KiB = 1024 bytes)?

1920 × 1080 px8 bit/px1 KiB = 1024 B
M = KiB
27.Digital logic: gates, K-maps & flip-flopsMedium
ABC00011110010001030204151716

Use the Karnaugh map to find the minimal product-of-sums (POS) form of F(A, B, C) = Σm(5, 6, 7). How many sum terms (factors) N does it have?

F(A, B, C) = Σm(5, 6, 7)
N =
28.Digital logic: gates, K-maps & flip-flopsHard
ABCD00011110000111100001031214150716X121130150140809X11010

Find the minimal SOP form of F(A, B, C, D) = Σm(2, 4, 5, 6, 13) + d(11, 12), where d marks the don't-care conditions. How many product terms N does it have?

F(A, B, C, D) = Σm(2, 4, 5, 6, 13) + d(11, 12)
N =
29.Laplace transformsMedium
t (s)f(t)t = 0.4f(0.4) = ?

Find f(t) for F(s) = 15/(s(s + 2)(s + 3)) by partial fractions, and evaluate f(0.4).

F(s) = 15/(s(s + 2)(s + 3))t = 0.4 s
f(0.4) =
30.Laplace transformsHard
ReIm−2−4−6−8−10−12

A system is described by the differential equation y″ + 7y′ + 10y = u′ + 12u, 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 = 0.6 s. Find g(0.6).

y″ + 7y′ + 10y = u′ + 12ut = 0.6 s
g(0.6) =
31.Block diagramsMedium
R(s)+K(s + 9)(s + 11)G(s)C(s)−

The plant G(s) = K/((s + 9)(s + 11)) is in a unity negative feedback loop. Find the gain K for which the closed loop is critically damped (two equal real poles).

G(s) = K/((s + 9)(s + 11))unity negative feedback
K =
32.Block diagramsHard
R(s)+46s(s + 5)G(s)C(s)2H−

The plant G(s) = 46/(s(s + 5)) is in a negative feedback loop with sensor gain H = 2. The closed-loop poles are complex. Find their imaginary part ωd (the positive value), in rad/s.

G(s) = 46/(s(s + 5))H = 2
ωd = rad/s
33.Step responseMedium
t (s)y(t)1

A system has the transfer function G(s) = 35/(s² + 5s + 35) and receives a unit step input. The poles are s = σ ± jωd. Find the real part σ.

G(s) = 35/(s² + 5s + 35)
σ =
34.Step responseHard
R(s)+135s(s + 16)G(s)C(s)−

A unity negative feedback loop has G(s) = 135/(s(s + 16)). Find the 2 % settling time ts of the closed-loop step response, using ts ≈ 4/(ζωₙ).

G(s) = 135/(s(s + 16))
ts = s
35.Bode plots & marginsMedium
vin​C = 47 nFR = 2.2 kΩvout​

The RC high-pass filter shown has R = 2.2 kΩ, C = 47 nF. A sinusoidal input of 310 Hz is applied. Find the phase shift φ of vout relative to vin, in degrees.

R = 2.2 kΩC = 47 nFf = 310 Hz
φ = °
36.Bode plots & marginsHard
|H| (dB)0.10.111101010010010001000−60−40−200204060ω (rad/s)φ (°)ω (rad/s)−180−135−90−450ωc​

A unity-feedback loop has the open-loop transfer function L(s) = 144/(s(s + 4)). Find the phase margin PM in degrees.

L(s) = 144/(s(s + 4))
PM = °
37.Stability: Routh–Hurwitz & root locusMedium
R(s)+K = 161s(s + 2)(s + 4)C(s)−

The loop in the diagram runs with K = 16 and L(s) = K/(s(s + 2)(s + 4)). By what factor m can the gain be raised before the closed loop becomes unstable?

L(s) = K/(s(s + 2)(s + 4))K = 16
m =
38.Stability: Routh–Hurwitz & root locusHard
ReIm−0.5−1−1.5−2−2.5−3−3.5−40.5j0.5j1

The root locus of L(s) = K(s + 3)/(s(s + 2)) leaves the real axis between s = 0 and s = −2, circles round and joins the real axis again to the left of the zero. Find the break-away point sb.

L(s) = K(s + 3)/(s(s + 2))
sb =
39.Steady-state error & PID controlMedium
R(s)+K = 12.510s + 1C(s)−

A process G(s) = 2.5/(10s + 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) = 2.5/(10s + 1)K = 1
ess = %
40.Steady-state error & PID controlHard
R(s)+K = 504s(s + 4)C(s)−

A proportional controller K = 50 drives the plant G(s) = 4/(s(s + 4)) in a unity-feedback loop. Find the peak time tp of the step response.

G(s) = 4/(s(s + 4))K = 50
tp = s

3Solutions

1.Series & parallel resistors

Answer: Req = 7.714 Ω

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​ = 3 ΩR3​ = 10 Ω+−V1​12 VR2​6 ΩAR4​12 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 = 10 + 12 = 22 Ω
R2 ∥ 22 = 6·22/(6+22) = 4.714 Ω
Req = R1 + 4.714 = 3 + 4.714 = 7.714 Ω

Answer

Req = 7.714 Ω
2.Series & parallel resistors

Answer: IR2 = 0.1673 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​ = 8 ΩR3​ = 8 ΩR5​ = 12 Ω+−V1​9 VR2​30 ΩAR4​12 ΩBR6​6 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 = 12 + 6 = 18 Ω
R4 ∥ 18 = 7.2 Ω
R3 + 7.2 = 15.2 Ω
R2 ∥ 15.2 = 10.09 Ω
Req = R1 + 10.09 = 8 + 10.09 = 18.09 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 = 9/18.09 = 0.4976 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 = 9 − 0.4976·8 = 5.02 V
IR2 = VA/R2 = 5.02/30 = 0.1673 A

Answer

IR2 = 0.1673 A
3.Nodal analysis

Answer: I2 = −1.288 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.

KCL at node A

Take the bottom wire as ground. Each branch carries (VA − Vk)/Rk away from A, where Vk is the voltage of its source (zero for a plain resistor). The currents leaving A add up to zero.

(VA − 15)/15 + (VA − 9)/4 + (VA − 24)/8 = 0

Solve for VA

VA = (15/15 + 9/4 + 24/8) / (1/15 + 1/4 + 1/8) = 6.25/0.4417 = 14.15 V

Branch current

The arrow points up through the branch, into node A.

I2 = (9 − VA)/R2 = (9 − 14.15)/4 = −1.288 A

Answer

I2 = −1.288 A

A negative result means the real current flows against the arrow.

4.Nodal analysis

Answer: VA = 9.229 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​ = 2 ΩR2​ = 15 ΩR4​ = 3 Ω+−V1​9 VR3​12 ΩAR5​4 ΩBIs​4 A+−V2​30 V

Set up the nodes

Ground is the bottom wire. Known node voltages come straight from the sources (V1 = 9 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/12 + (VA − 9)/2 + (VA − VB)/15 = 0
0.65·VA − 0.06667·VB = 4.5

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/4 + (VB − VA)/15 + (VB − 30)/3 = 4
−0.06667·VA + 0.65·VB = 14

Solve

Δ = (0.65)(0.65) − (−0.06667)(−0.06667) = 0.4181
VA = Δ1/Δ = 3.858/0.4181 = 9.229 V
VB = Δ2/Δ = 9.4/0.4181 = 22.49 V

Answer

VA = 9.229 V
5.Mesh analysis

Answer: I1 = 0.1579 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​ = 10 ΩR2​ = 4 Ω+−V1​18 VR3​8 ΩA+−V2​24 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
10·I1 + 8(I1 − I2) = 18
18·I1 − 8·I2 = 18

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
4·I2 + 8(I2 − I1) = (−24)
−8·I1 + 12·I2 = −24

Solve

Δ = (18)(12) − (−8)(−8) = 152
I1 = Δ1/Δ = 24/152 = 0.1579 A
I2 = Δ2/Δ = −288/152 = −1.895 A

Answer

I1 = 0.1579 A

A negative mesh current flows anticlockwise.

6.Mesh analysis

Answer: IR3 = −1.074 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​ = 25 ΩR2​ = 2 ΩR3​ = 5 Ω+−V1​30 VR4​20 ΩAR5​2 ΩB+−V2​9 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
25·I1 + 20(I1 − I2) = 30
45·I1 − 20·I2 = 30

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
2·I2 + 20(I2 − I1) + 2(I2 − I3) = 0
−20·I1 + 24·I2 − 2·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
5·I3 + 2(I3 − I2) = (−9)
−2·I2 + 7·I3 = −9

Solve

Δ = det of the coefficient matrix = 4580
I1 = Δ1/Δ = 4560/4580 = 0.9956 A
I2 = Δ2/Δ = 3390/4580 = 0.7402 A
I3 = Δ3/Δ = −4920/4580 = −1.074 A

Answer

IR3 = I3 = −1.074 A

A negative mesh current flows anticlockwise.

7.Superposition

Answer: Is = 0.48 A

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​ = 5 ΩR3​ = 20 Ω+−V1​9 VR2​20 ΩAR4​15 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 = 20+15 = 35 Ω
R2 ∥ (R3+R4) = 20·35/(20+35) = 12.73 Ω
VA = 9·12.73/(5+12.73) = 6.462 V
VB = VA·R4/(R3+R4) = 6.462·15/35 = 2.769 V
IR3′ = (VA − VB)/R3 = (6.462 − 2.769)/20 = 0.1846 A

Case 2 · Is acting alone

V₁ becomes a short, so R₁ ∥ R₂ hangs from A to ground. Iₛ splits at B between R₄ and the path R₃ + R₁∥R₂; the part through R₃ flows from B to A, against the arrow.

R1 ∥ R2 = 4 Ω
IR3″ = −Is·R4/(R4 + R3 + R1∥R2) = −Is·15/39 = −0.3846·Is

Set the total to zero

IR3′ + IR3″ = 0.1846 − 0.3846·Is = 0
Is = 0.1846/0.3846 = 0.48 A

Answer

Is = 0.48 A
8.Superposition

Answer: IR4 = 5.043 A

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​ = 20 ΩR2​ = 10 ΩR4​ = 3 Ω+−V1​10 VR3​20 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) = 20 ∥ 13 = 7.879 Ω
VA = 10·7.879/(20+7.879) = 2.826 V
VB = VA·R4/(R2+R4) = 2.826·3/13 = 0.6522 V
IR4′ = (VB − V2)/R4 = (0.6522 − 0)/3 = 0.2174 A
R1​ = 20 ΩR2​ = 10 ΩR4​ = 3 ΩSHORTR3​20 ΩAIs​6 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 = 10 Ω, so the left path is R2+10 = 20 Ω
Req = R4 ∥ 20 = 2.609 Ω
VB = Is·Req = 6·2.609 = 15.65 V
VA = VB·10/20 = 7.826 V
IR4″ = (VB − V2)/R4 = (15.65 − 0)/3 = 5.217 A
R1​ = 20 ΩR2​ = 10 ΩR4​ = 3 ΩSHORTR3​20 ΩAOPENB+−V2​9 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 = 20·20/(20+20) = 10 Ω
VB = V2·(R2+R1∥R3)/(R4+R2+R1∥R3) = 9·20/23 = 7.826 V
VA = VB·(R1∥R3)/(R2+R1∥R3) = 7.826·10/20 = 3.913 V
IR4‴ = (VB − V2)/R4 = (7.826 − 9)/3 = −0.3913 A

Add the contributions

IR4 = IR4′ + IR4″ + IR4‴
IR4 = 0.2174 + 5.217 + (−0.3913) = 5.043 A

A negative result means the real current flows against the arrow.

9.Thévenin & Norton

Answer: IL = 0.2951 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​ = 8 ΩR3​ = 4 ΩSHORTR2​6 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 = 8·6/(8+6) = 3.429 Ω
Rth = (R1 ∥ R2) + R3 = 3.429 + 4 = 7.429 Ω
R1​ = 8 ΩR3​ = 4 Ω+−V1​12 VR2​6 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) = 12·6/(8+6) = 5.143 V
Rth​ = 7.429 Ω+−Vth​5.143 VRL​10 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) = 5.143/(7.429 + 10) = 0.2951 A
10.Thévenin & Norton

Answer: Vth = 8.182 V

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​ = 10 ΩR3​ = 6 ΩSHORTR2​12 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 = 10·12/(10+12) = 5.455 Ω
Rth = (R1 ∥ R2) + R3 = 5.455 + 6 = 11.45 Ω
R1​ = 10 ΩR3​ = 6 Ω+−V1​36 VR2​12 ΩAIs​1 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) = 19.64 + (−1)·5.455 = 14.18 V
Vth = VB = VA + Is·R3 = 14.18 + (−1)·6 = 8.182 V
11.RC & RL transients

Answer: vL = 1.605 V

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 = 220 mH / 50 Ω = 4.4 ms
i(∞) = Vs/R = 5/50 = 0.1 A

Inductor voltage

At t = 0 the whole supply voltage appears across the inductor; it then decays to zero.

vL(t) = Vs·e−t/τ = 5·e−5/4.4 = 1.605 V

Answer

vL = 1.605 V
12.RC & RL transients

Answer: t = 1.881 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.

Initial value, final value, time constant

Before t = 0 the closed switch bypasses R₂; afterwards R₁ and R₂ are both in the loop.

i(0) = 20/20 = 1 A
i(∞) = 20/(20 + 10) = 0.6667 A
τ = L/R = 47/30 = 1.567 ms
i(t) = 0.6667 + (1 − 0.6667)·e−t/τ

Solve for the time

e−t/τ = (0.767 − 0.6667)/(1 − 0.6667) = 0.301
t = 1.567·ln(3.322) = 1.881 ms

Answer

t = 1.881 ms
13.AC impedance & phasors

Answer: I = 0.3189 A

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|.

Reactances

ω = 2πf = 2π·1000 = 6283 rad/s
XL = ωL = 6283·0.05 = 314.2 Ω
XC = 1/(ωC) = 1/(6283·100·10⁻⁶) = 1.592 Ω

Impedance

In series the impedances add as complex numbers: Z = R + j(XL − XC).

|Z| = √(R² + (XL − XC)²) = √(25² + (312.6)²) = 313.6 Ω

Current

The same current flows through every element of a series circuit.

I = V/|Z| = 100/313.6 = 0.3189 A

Answer

I = 0.3189 A
14.AC impedance & phasors

Answer: VL = 10 V

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

At resonance the reactances cancel, so the impedance is just R.

ω₀ = 1/√(LC) = 1/√(0.1·10·10⁻⁶) = 1000 rad/s
I = V/R = 5/50 = 0.1 A

Voltage across the inductor

XL = ω₀L = 1000·0.1 = 100 Ω
VL = I·XL = 0.1·100 = 10 V

Answer

VL = 10 V

This is Q = 2 times the supply voltage.

15.AC power & power factor

Answer: I = 164.3 A

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.

Line current

Only the real part of the power does work, so divide by the power factor.

I = P/(V·cos φ) = 34000/(230·0.9) = 164.3 A

Answer

I = 164.3 A
16.AC power & power factor

Answer: cos φ = 0.7382

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 before and after

The real power P does not change; only the reactive power drawn from the supply does.

Q1 = 17·tan(arccos 0.7) = 17.34 kvar
QC = V²·2πf·C = 240²·2π·50·100·10⁻⁶ = 1810 var = 1.81 kvar
Q2 = 17.34 − 1.81 = 15.53 kvar

New apparent power

S2 = √(17² + 15.53²) = 23.03 kVA

New power factor

cos φ = P/S2 = 17/23.03 = 0.7382

Answer

cos φ = 0.7382
17.Three-phase power

Answer: P = 1.298 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| = √(12² + 16²) = 20 Ω
Iph = 120.1/20 = 6.004 A

Total real power

Only the resistive part of each impedance absorbs real power.

P = 3·Iph²·R = 3·6.004²·12 = 1.298 kW

Answer

P = 1.298 kW

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

18.Three-phase power

Answer: Cph = 1343 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 = 300·tan(acos 0.8) = 300·0.75 = 225 kvar
Q2 = 300·tan(acos 0.92) = 300·0.426 = 127.8 kvar

Reactive power from the capacitors

QC = Q1 − Q2 = 97.2 kvar

Capacitance per phase

In a Y bank each capacitor is connected between a line and the star point.

V = 480/√3 = 277.1 V, ω = 2π·50 = 314.2 rad/s
Cph = (QC/3)/(ω·V²) = 32400/(314.2·277.1²) = 1343 µF

Answer

Cph = 1343 µF
19.Transformers

Answer: I1 = 2.5 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 = 480/4 = 120 V
I2 = 120/12 = 10 A

Primary current

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

I1 = I2/4 = 2.5 A

Answer

I1 = 2.5 A

Check: the load seen from the primary is a²·RL = 192 Ω, and 480/192 gives the same current.

20.Transformers

Answer: Ploss = 656.3 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.

Copper loss at this load

Pcu = x²·Pcu,fl = 0.25·1125 = 281.3 W

Total losses

The core loss is the same at any load.

Ploss = 375 + 281.3 = 656.3 W

Answer

Ploss = 656.3 W

The efficiency at this load is η = 97.98%.

21.Op-amp circuits

Answer: Vout = −1.71 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.

Inverting input follows the input

V₋ = V₊ = −0.3 V
I = V₋/R1 = −0.3/10 = −0.03 mA

Output voltage

The current through R₁ also flows through Rf.

Vout = V₋ + I·Rf = −0.3 + (−0.03)·47 = −1.71 V

Answer

Vout = −1.71 V
22.Op-amp circuits

Answer: Vout = 7.841 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 = −1.6/100 = −0.016 mA
I2 = V2/R2 = −1.6/4.7 = −0.3404 mA
If = I1 + I2 = −0.3564 mA

Output voltage

Vout = −Rf·If = −22·(−0.3564) = 7.841 V

Answer

Vout = 7.841 V
23.Diodes & transistors

Answer: R = 300 Ω

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).

Voltage across the resistor

VR = 9 − 3·2 = 3 V

Resistance

R = 3/0.01 = 300 Ω

Answer

R = 300 Ω

The resistor dissipates 30 mW.

24.Diodes & transistors

Answer: ID = 8.889 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

5 = 0.6 + I·(470 + 25)

Operating current

ID = 4.4/495 = 8.889 mA
VD = 0.6 + 0.008889·25 = 0.8222 V

Answer

ID = 8.889 mA
25.Number systems

Answer: U = 149

Setting bits: each bit is worth a power of two (128, 64, …, 1). One hex digit is exactly four bits, and in 8-bit two's complement the leftmost bit is worth −128. Bitwise operations work on each bit position separately.

Invert and add one

107 = 0110 1011
inverted: 1001 0100
+1 → 1001 0101

Read it as unsigned

1001 0101₂ = 256 − 107 = 149

Answer

U = 149
26.Number systems

Answer: M = 2025 KiB

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.

Bits and bytes

1920·1080·8 = 16588800 bit = 2073600 B

Convert to KiB

2073600/1024 = 2025 KiB

Answer

M = 2025 KiB
27.Digital logic: gates, K-maps & flip-flops

Answer: N = 2

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.

ABC00011110010001030204151716

Group the 0s

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

(B + C)
A

Minimal POS form

F = (B + C)A
N = 2

Answer

N = 2
28.Digital logic: gates, K-maps & flip-flops

Answer: N = 2

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.

BC′, A′CD′, A′BD′
ABCD00011110000111100001031214150716X121130150140809X11010

Minimal cover

F = BC′ + A′CD′
N = 2

Answer

N = 2
29.Laplace transforms

Answer: f(0.4) = 0.636

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 + 3)
A = 15/(2·3) = 2.5
B = 15/((−2)·1) = −7.5
C = 15/((−3)·(−1)) = 5

Inverse transform

f(t) = 2.5 − 7.5·e−2t + 5·e−3t

Evaluate

f(0.4) = 2.5 − 7.5·e−2·0.4 + 5·e−3·0.4 = 0.636

Answer

f(0.4) = 0.636
30.Laplace transforms

Answer: g(0.6) = 0.8878

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) = (s + 12)/(s² + 7s + 10)

Partial fractions

s² + 7s + 10 = (s + 2)(s + 5)
A = 3.333, B = −2.333

Impulse response

g(t) = 3.333·e−2t − 2.333·e−5t
g(0.6) = 0.8878

Answer

g(0.6) = 0.8878
31.Block diagrams

Answer: K = 1

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).

Characteristic equation

1 + K/((s + 9)(s + 11)) = 0 → s² + 20s + 99 + K = 0

Repeated root

A quadratic s² + βs + γ has a double root when β² = 4γ.

20² = 4(99 + K) → K = 400/4 − 99 = 1

Answer

K = 1
Both closed-loop poles are then at s = −10.
32.Block diagrams

Answer: ωd = 9.26 rad/s

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).

Characteristic equation

s(s + 5) + 46·2 = 0 → s² + 5s + 92 = 0

Roots

s = −2.5 ± j·√(92 − 6.25) = −2.5 ± j9.26
ωd = 9.26 rad/s

Answer

ωd = 9.26 rad/s
33.Step response

Answer: σ = −2.5

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 = 35 → ωₙ = 5.916 rad/s
2ζωₙ = 5 → ζ = 5/(2·5.916) = 0.4226

Result

σ = −ζωₙ = −5/2 = −2.5

Answer

σ = −2.5
34.Step response

Answer: ts = 0.5 s

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).

Closed-loop transfer function

T(s) = 135/(s² + 16s + 135): ωₙ = 11.62 rad/s, ζ = 0.6885

Settling time

ζωₙ = 16/2 = 8
ts ≈ 4/(ζωₙ) = 0.5 s

Answer

ts = 0.5 s

For this loop ζωₙ = a/2 whatever K is: raising K adds overshoot but does not shorten the settling time.

35.Bode plots & margins

Answer: φ = 78.61 °

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.

Corner frequency

ωc = 1/(RC) = 1/(2200·4.7 × 10⁻⁸) = 9671 rad/s
fc = 1539 Hz → f/fc = 310/1539 = 0.2014

Phase

φ = 90° − atan(0.2014) = 78.61°

Answer

φ = 78.61°
36.Bode plots & margins

Answer: PM = 18.92 °

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.

Gain crossover

ω⁴ + 16ω² − 20736 = 0
ω² = (−16 + √(256 + 4·20736))/2 = 136.2
ωc = 11.67 rad/s

Phase margin

∠L(jωc) = −90° − atan(11.67/4) = −161.1°
PM = 180° + ∠L = 18.92°

Answer

PM = 18.92°
37.Stability: Routh–Hurwitz & root locus

Answer: m = 3

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.

Routh array

s³ + 6s² + 8s + K = 0
s³: 1, 8
s²: 6, K
s¹: (6·8 − K)/6
s⁰: K

Largest stable gain

Kmax = 6·8 = 48

Factor

m = 48/16 = 3

Answer

m = 3

This factor is the gain margin as a ratio: 9.542 dB.

38.Stability: Routh–Hurwitz & root locus

Answer: sb = −1.268

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) = −(s² + 2s)/(s + 3)

Stationary points

Differentiate with the quotient rule and set the numerator to zero.

(2s + 2)(s + 3) − (s² + 2s) = s² + 6s + 6 = 0
s = −3 ± √3 = −1.268, −4.732

Break-away point

sb = −1.268

Answer

sb = −1.268

Between the two break points the locus is a circle centred on the zero, with radius √3 = 1.732.

39.Steady-state error & PID control

Answer: ess = 28.57 %

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 = 1·2.5 = 2.5

Step error

ess = 100/(1 + 2.5) = 28.57 %

Answer

ess = 28.57 %
40.Steady-state error & PID control

Answer: tp = 0.2244 s

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) + 50·4 = s² + 4s + 200

ωₙ and ζ

ωₙ = √200 = 14.14 rad/s
ζ = 4/(2·14.14) = 0.1414

Peak time

ωd = 14.14·√(1 − 0.1414²) = 14 rad/s
tp = π/14 = 0.2244 s

Answer

tp = 0.2244 s

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