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 ΩR3​ = 20 Ω+−V1​9 VR2​6 ΩIR2​AR4​8 ΩB

Find the current IR2 through R2.

V1 = 9 VR1 = 2 ΩR2 = 6 ΩR3 = 20 ΩR4 = 8 Ω
IR2 = A
2.Series & parallel resistorsHard
R1​ = 20 ΩR3​ = 8 ΩR5​ = 25 Ω+−V1​9 VR2​2 ΩIR2​AR4​25 ΩBR6​20 Ω

Find the current IR2 through R2.

V1 = 9 VR1 = 20 ΩR2 = 2 ΩR3 = 8 ΩR4 = 25 ΩR5 = 25 ΩR6 = 20 Ω
IR2 = A
3.Nodal analysisMedium
R1​ = 8 ΩIR1​R3​ = 12 Ω+−V1​24 VR2​6 ΩAR4​10 ΩBIs​4 A

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

V1 = 24 VIs = 4 AR1 = 8 ΩR2 = 6 ΩR3 = 12 ΩR4 = 10 Ω
IR1 = A
4.Nodal analysisHard
R1​ = 6 ΩR2​ = 3 ΩR4​ = 30 ΩIR4​+−V1​24 VR3​5 ΩAR5​8 ΩBIs​1 A+−V2​15 V

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

V1 = 24 VIs = 1 AV2 = 15 VR1 = 6 ΩR2 = 3 ΩR3 = 5 ΩR4 = 30 ΩR5 = 8 Ω
IR4 = A
5.Mesh analysisMedium
R1​ = 5 ΩR2​ = 12 ΩIR2​+−V1​12 VR3​15 ΩA+−V2​10 VI1​I2​

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

V1 = 12 VV2 = 10 VR1 = 5 ΩR2 = 12 ΩR3 = 15 Ω
IR2 = A
6.Mesh analysisHard
R1​ = 5 ΩR2​ = 2 Ω+−VR2​R3​ = 12 Ω+−V1​24 VR4​4 ΩAR5​5 ΩB+−V2​15 VI1​I2​I3​

Use mesh analysis to find the voltage VR2 across R2 with the polarity shown.

V1 = 24 VV2 = 15 VR1 = 5 ΩR2 = 2 ΩR3 = 12 ΩR4 = 4 ΩR5 = 5 Ω
VR2 = V
7.SuperpositionMedium
R1​ = 6 ΩIR1​R3​ = 3 Ω+−V1​12 VR2​10 ΩAR4​8 ΩBIs​3 A

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

V1 = 12 VIs = 3 AR1 = 6 ΩR2 = 10 ΩR3 = 3 ΩR4 = 8 Ω
IR1 = A
8.SuperpositionHard
R1​ = 12 ΩR2​ = 3 ΩR4​ = 4 Ω+−V1​9 VR3​10 ΩIR3​AIs​5 AB+−V2​?

Find the value of the voltage source V2 (polarity as shown) that makes the current IR3 through R3 equal to zero.

V1 = 9 VIs = 5 AR1 = 12 ΩR2 = 3 ΩR3 = 10 ΩR4 = 4 Ω
V2 = V
9.Thévenin & NortonMedium
R1​ = 10 ΩR3​ = 20 Ω+−V1​15 VR2​2 ΩAab

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

V1 = 15 VR1 = 10 ΩR2 = 2 ΩR3 = 20 Ω
Vth = V
10.Thévenin & NortonHard
R1​ = 3 ΩR3​ = 5 Ω+−V1​18 VR2​30 ΩAIs​5 ABRL​12 ΩIL​

A load RL = 12 Ω is connected across a–b. Use a Thévenin equivalent to find the power PL delivered to the load.

V1 = 18 VIs = 5 AR1 = 3 ΩR2 = 30 ΩR3 = 5 ΩRL = 12 Ω
PL = W
11.RC & RL transientsMedium
+−Vs​9 Vt = 0R1​ = 6.8 kΩR2​ = 1 kΩC22 µF+−vC​

The source Vₛ charges the capacitor through R₁, and R₂ is connected in parallel with C. The capacitor is uncharged when the switch closes at t = 0. Find the capacitor voltage vC at t = 40 ms.

Vs = 9 VR1 = 6.8 kΩR2 = 1 kΩC = 22 µFt = 40 ms
vC = V
12.RC & RL transientsHard
+−Vs​9 Vt = 0R = 100 kΩC?+−vC​

A timer starts charging an uncharged capacitor through a resistor from a 9 V supply at t = 0. It must trigger when the capacitor voltage reaches 8.1 V, exactly 200 ms after the start. With R = 100 kΩ, find the capacitance C needed.

Vs = 9 VVth = 8.1 VT = 200 msR = 100 kΩ
C = µF
13.AC impedance & phasorsMedium
230 V100 HzR = 50 ΩL = 20 mHC = 22 µF

A series RLC circuit is connected to a 230 V (rms), 100 Hz supply. Find the phase angle φ of the impedance, in degrees (positive when the current lags the voltage).

V = 230 V (rms)f = 100 HzR = 50 ΩL = 20 mHC = 22 µF
φ = °
14.AC impedance & phasorsHard
230 V500 HzR1​ = 20 ΩR2​ = 30 ΩC = 4.7 µFI

A resistor R1 is connected in series with a parallel combination of R2 and a capacitor C, across a 230 V (rms), 500 Hz supply. Find the rms current I.

V = 230 V (rms)f = 500 HzR1 = 20 ΩR2 = 30 ΩC = 4.7 µF
I = A
15.AC power & power factorMedium
P = 39 kWQSφ

A single-phase motor takes 39 kW at a power factor of 0.75 lagging from a 400 V supply. Find the line current I.

P = 39 kWpf = 0.75V = 400 V
I = A
16.AC power & power factorHard
240 V50 Hzload25 kW, 0.8C150 µFI = ?

A single-phase load takes 25 kW at a power factor of 0.8 lagging from a 240 V, 50 Hz supply. A 150 µF capacitor is connected in parallel with the load. Find the new line current I.

P = 25 kWpf1 = 0.8V = 240 Vf = 50 HzC = 150 µF
I = A
17.Three-phase powerMedium
ABCVL​ = 480 VNZ = 12 + j5 Ωper phase

A balanced Y-connected load with an impedance of 12 + j5 Ω per phase is connected to a balanced three-phase supply with a line-to-line voltage of 480 V. Find the total real power P absorbed by the load in kW.

VL = 480 VZ = 12 + j5 Ω per phase
P = kW
18.Three-phase powerHard
P = 75 kWφ1​S1​Q2​QC​ = ?

A balanced three-phase load takes 75 kW at a power factor of 0.75 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. Find the total reactive power QC the capacitor bank must supply, in kvar.

P = 75 kWpf1 = 0.75pf2 = 0.92VL = 480 Vf = 50 Hz
QC = kvar
19.TransformersMedium
4160 V480 VIHV​ILV​ = ?250 kVA

A single-phase 250 kVA, 4160/480 V transformer operates at its rated load. Treat it as ideal. Find the current ILV in the low-voltage winding.

S = 250 kVAV1 = 4160 VV2 = 480 V
ILV = A
20.TransformersHard
pf 0.9200 kVA, η = 98%

A single-phase 200 kVA transformer has a core loss of 1200 W. At rated load and a power factor of 0.9 lagging its efficiency is 98%. Find the full-load copper loss Pcu,fl in watts.

S = 200 kVAPcore = 1200 Wpf = 0.9η = 98%
Pcu,fl = W
21.Op-amp circuitsMedium
−+Vout​Rf​ = 10 kΩR1​ = 10 kΩVin​ = 0.5 VRa​ = 10 kΩRb​ = 47 kΩ

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

Vin = 0.5 VRa = 10 kΩRb = 47 kΩR1 = 10 kΩRf = 10 kΩ
Vout = V
22.Op-amp circuitsHard
−+Vout​C = 1 µFVin​ = 1.8 VR = 10 kΩ

The integrator uses an ideal op-amp with ±15 V supplies; its output saturates at ±12 V. The capacitor is uncharged when a constant input Vin = 1.8 V is applied at t = 0. Find the output voltage Vout at t = 50 ms.

Vin = 1.8 VR = 10 kΩC = 1 µFVsat = ±12 Vt = 50 ms
Vout = V
23.Diodes & transistorsMedium
RC​ = 1.5 kΩβ = 80VCC​ = 15 VRB​ = 560 kΩ

An NPN transistor with β = 80 is biased by a base resistor RB = 560 kΩ from the supply VCC = 15 V. The collector resistor is RC = 1.5 kΩ and the emitter is grounded. Take VBE = 0.7 V and assume the transistor is in the active region. Find the collector–emitter voltage VCE.

VCC = 15 VRB = 560 kΩRC = 1.5 kΩβ = 80VBE = 0.7 V
VCE = V
24.Diodes & transistorsHard
+−≤ 27 V470 Ω5.1 V

A 5.1 V Zener regulator has a 470 Ω series resistor. The input can rise to 27 V, and the load may be disconnected. Find the largest power PZ,max the Zener must dissipate.

Vin,max = 27 VVZ = 5.1 VR = 470 Ω
PZ,max = mW
25.Number systemsMedium
place values in two's complement1−12816403201618141201

The 8-bit pattern 1100 1110 stores a signed integer in two's complement. What is its value N in decimal?

1100 11108 bit
N =
26.Number systemsHard
4775 codes, b = ? bits?2ᵇ⁻¹…?4?2?1

A system must give every one of 4775 items its own binary code of the same length. What is the smallest number of bits b needed?

4775
b = bit
27.Digital logic: gates, K-maps & flip-flopsMedium
ABCD0001111000011110111111

In this Karnaugh map exactly one 1 has no neighbouring 1, so it stays a group of one cell (a full minterm of four literals) in the minimal SOP form. Neighbours across the map edges count. Click that cell.

F = Σm(5, 6, 7, 8, 13, 14)
  1. 1AB = 00, CD = 00
  2. 2AB = 00, CD = 01
  3. 3AB = 00, CD = 11
  4. 4AB = 00, CD = 10
  5. 5AB = 01, CD = 00
  6. 6AB = 01, CD = 01
  7. 7AB = 01, CD = 11
  8. 8AB = 01, CD = 10
  9. 9AB = 11, CD = 00
  10. 10AB = 11, CD = 01
  11. 11AB = 11, CD = 11
  12. 12AB = 11, CD = 10
  13. 13AB = 10, CD = 00
  14. 14AB = 10, CD = 01
  15. 15AB = 10, CD = 11
  16. 16AB = 10, CD = 10
28.Digital logic: gates, K-maps & flip-flopsHard
ABCD0001111000011110X0010312X4150706112013015X141809011010

Find the minimal SOP form of F(A, B, C, D) = Σm(2, 5, 8, 12) + d(0, 4, 14), where d marks the don't-care conditions. How many literals L does it contain?

F(A, B, C, D) = Σm(2, 5, 8, 12) + d(0, 4, 14)
L =
29.Laplace transformsMedium
ReIm−1−2−3−4−51

F(s) = 17/(s² + 9s + 20). Its inverse transform has the form f(t) = A·e−4t + B·e−5t. Find the coefficient A by partial fractions.

F(s) = 17/(s² + 9s + 20)
A =
30.Laplace transformsHard
t (s)y(t)t = 0.3y(0.3) = ?

Solve y″ + 10y′ + 24y = 0 with y(0) = 3 and y′(0) = 4 using the Laplace transform, and find y(0.3).

y″ + 10y′ + 24y = 0y(0) = 3y′(0) = 4t = 0.3 s
y(0.3) =
31.Block diagramsMedium
R(s)+K(s + 10)(s + 12)G(s)C(s)−

The plant G(s) = K/((s + 10)(s + 12)) 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 + 10)(s + 12))unity negative feedback
K =
32.Block diagramsHard
R(s)+3controller+D(s)+10s + 10plantC(s)−

A proportional controller K = 3 drives the plant G(s) = 10/(s + 10) 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 10 and a disturbance step of size 0.5 are applied together. Find the steady-state output css.

K = 3G(s) = 10/(s + 10)D = 0.5R = 10
css =
33.Step responseMedium
t (s)y(t)3?

A system has the transfer function G(s) = 132/(s² + 9s + 44) and receives a unit step input. Find the percent overshoot %OS of the step response.

G(s) = 132/(s² + 9s + 44)
%OS = %
34.Step responseHard
k = 2000 N/mc = 27 N·s/mm = 4 kgF = 100 Nx(t)

A mass m = 4 kg hangs on a spring k = 2000 N/m with a viscous damper c = 27 N·s/m (m·x″ + c·x′ + k·x = F). At rest in equilibrium, a constant force F = 100 N is suddenly applied. Find the time tp at which the displacement is largest.

m = 4 kgk = 2000 N/mc = 27 N·s/mF = 100 N
tp = s
35.Bode plots & marginsMedium
vin​R = 2.2 kΩC = 4.7 nFvout​

The RC low-pass filter shown has R = 2.2 kΩ, C = 4.7 nF. A sinusoidal input of 31 kHz is applied. Find the gain |H| = |vout/vin| in dB.

R = 2.2 kΩC = 4.7 nFf = 31 kHz
|H| = dB
36.Bode plots & marginsHard
|H| (dB)0.10.1111010100100−80−60−40−2002040ω (rad/s)φ (°)ω (rad/s)−270−180−900ω180​ = ?

A unity-feedback loop has the open-loop transfer function L(s) = 476/(s(s + 6)(s + 8)). Find the phase crossover frequency ω180, where ∠L(jω) = −180°.

L(s) = 476/(s(s + 6)(s + 8))
ω180 = rad/s
37.Stability: Routh–Hurwitz & root locusMedium
R(s)+K1(s + 2)(s + 4)(s + 5)C(s)−

A unity-feedback loop has L(s) = K/((s + 2)(s + 4)(s + 5)), with K > 0. Find the largest gain Kmax for which the closed loop is stable.

L(s) = K/((s + 2)(s + 4)(s + 5))
Kmax =
38.Stability: Routh–Hurwitz & root locusHard
ReIm−2−4−6−8−10−12j2sb​

The root locus of L(s) = K/((s + 4)(s + 10)) is shown. Find the gain K at the break-away point sb, where the two closed-loop poles meet on the real axis.

L(s) = K/((s + 4)(s + 10))
K =
39.Steady-state error & PID controlMedium
r(t) = 0.5·t²/2+2(s + 2)s²(s + 1)C(s)−

The parabolic input r(t) = 0.5·t²/2 is applied to a unity-feedback loop with G(s) = 2(s + 2)/(s²(s + 1)). Find the steady-state error ess.

G(s) = 2(s + 2)/(s²(s + 1))r(t) = 0.5·t²/2
ess =
40.Steady-state error & PID controlHard
R(s)+2 + Kd​s4s(s + 1)C(s)−

A PD controller C(s) = 2 + Kd·s drives the plant G(s) = 4/(s(s + 1)) in a unity-feedback loop. Find the derivative gain Kd that gives the closed loop a damping ratio ζ = 0.8.

G(s) = 4/(s(s + 1))Kp = 2ζ = 0.8
Kd = s

3Solutions

1.Series & parallel resistors

Answer: IR2 = 1.068 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​ = 20 Ω+−V1​9 VR2​6 ΩAR4​8 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 = 20 + 8 = 28 Ω
R2 ∥ 28 = 6·28/(6+28) = 4.941 Ω
Req = R1 + 4.941 = 2 + 4.941 = 6.941 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 = 9/6.941 = 1.297 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 − 1.297·2 = 6.407 V
IR2 = VA/R2 = 6.407/6 = 1.068 A

Answer

IR2 = 1.068 A
2.Series & parallel resistors

Answer: IR2 = 0.3804 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​ = 20 ΩR3​ = 8 ΩR5​ = 25 Ω+−V1​9 VR2​2 ΩAR4​25 ΩBR6​20 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 = 25 + 20 = 45 Ω
R4 ∥ 45 = 16.07 Ω
R3 + 16.07 = 24.07 Ω
R2 ∥ 24.07 = 1.847 Ω
Req = R1 + 1.847 = 20 + 1.847 = 21.85 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 = 9/21.85 = 0.412 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 − 0.412·20 = 0.7607 V
IR2 = VA/R2 = 0.7607/2 = 0.3804 A

Answer

IR2 = 0.3804 A
3.Nodal analysis

Answer: IR1 = 1.213 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​ = 8 ΩR3​ = 12 Ω+−V1​24 VR2​6 ΩAR4​10 ΩBIs​4 A

Set up the nodes

Ground is the bottom wire. Known node voltages come straight from the sources (V1 = 24 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/6 + (VA − 24)/8 + (VA − VB)/12 = 0
0.375·VA − 0.08333·VB = 3

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/10 + (VB − VA)/12 = 4
−0.08333·VA + 0.1833·VB = 4

Solve

Δ = (0.375)(0.1833) − (−0.08333)(−0.08333) = 0.06181
VA = Δ1/Δ = 0.8833/0.06181 = 14.29 V
VB = Δ2/Δ = 1.75/0.06181 = 28.31 V

Answer

IR1 = (V1 − VA)/R1 = (24 − 14.29)/8 = 1.213 A
4.Nodal analysis

Answer: IR4 = −0.1591 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​ = 30 Ω+−V1​24 VR3​5 ΩAR5​8 ΩBIs​1 A+−V2​15 V

Set up the nodes

Ground is the bottom wire. Known node voltages come straight from the sources (V1 = 24 V, V2 = 15 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/5 + (VA − 24)/6 + (VA − VB)/3 = 0
0.7·VA − 0.3333·VB = 4

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/8 + (VB − VA)/3 + (VB − 15)/30 = 1
−0.3333·VA + 0.4917·VB = 1.5

Solve

Δ = (0.7)(0.4917) − (−0.3333)(−0.3333) = 0.2331
VA = Δ1/Δ = 2.467/0.2331 = 10.58 V
VB = Δ2/Δ = 2.383/0.2331 = 10.23 V

Answer

IR4 = (VB − V2)/R4 = (10.23 − 15)/30 = −0.1591 A
5.Mesh analysis

Answer: IR2 = −0.06349 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​ = 12 Ω+−V1​12 VR3​15 ΩA+−V2​10 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 + 15(I1 − I2) = 12
20·I1 − 15·I2 = 12

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
12·I2 + 15(I2 − I1) = (−10)
−15·I1 + 27·I2 = −10

Solve

Δ = (20)(27) − (−15)(−15) = 315
I1 = Δ1/Δ = 174/315 = 0.5524 A
I2 = Δ2/Δ = −20/315 = −0.06349 A

Answer

IR2 = I2 = −0.06349 A

A negative mesh current flows anticlockwise.

6.Mesh analysis

Answer: VR2 = 1.614 V

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​ = 2 ΩR3​ = 12 Ω+−V1​24 VR4​4 ΩAR5​5 ΩB+−V2​15 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
5·I1 + 4(I1 − I2) = 24
9·I1 − 4·I2 = 24

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 + 4(I2 − I1) + 5(I2 − I3) = 0
−4·I1 + 11·I2 − 5·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
12·I3 + 5(I3 − I2) = (−15)
−5·I2 + 17·I3 = −15

Solve

Δ = det of the coefficient matrix = 1186
I1 = Δ1/Δ = 3588/1186 = 3.025 A
I2 = Δ2/Δ = 957/1186 = 0.8069 A
I3 = Δ3/Δ = −765/1186 = −0.645 A

Answer

IR2 = I2 = 0.8069 A
VR2 = IR2·R2 = 0.8069·2 = 1.614 V

A negative mesh current flows anticlockwise.

7.Superposition

Answer: IR1 = −0.05085 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​ = 6 ΩR3​ = 3 Ω+−V1​12 VR2​10 ΩAR4​8 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 = 3+8 = 11 Ω
R2 ∥ (R3+R4) = 10·11/(10+11) = 5.238 Ω
VA = 12·5.238/(6+5.238) = 5.593 V
VB = VA·R4/(R3+R4) = 5.593·8/11 = 4.068 V
IR1′ = (VA − V1)/R1 = (5.593 − 12)/6 = −1.068 A
R1​ = 6 ΩR3​ = 3 ΩSHORTR2​10 ΩAR4​8 ΩBIs​3 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 = 6·10/(6+10) = 3.75 Ω
Req = R4 ∥ (R3+R1∥R2) = 8 ∥ 6.75 = 3.661 Ω
VB = Is·Req = 3·3.661 = 10.98 V
VA = VB·(R1∥R2)/(R3+R1∥R2) = 10.98·3.75/6.75 = 6.102 V
IR1″ = (VA − V1)/R1 = (6.102 − 0)/6 = 1.017 A

Add the contributions

IR1 = IR1′ + IR1″
IR1 = (−1.068) + 1.017 = −0.05085 A

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

8.Superposition

Answer: V2 = 14.75 V

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​ = 12 ΩR2​ = 3 ΩR4​ = 4 Ω+−V1​9 VR3​10 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) = 10 ∥ 7 = 4.118 Ω
VA = 9·4.118/(12+4.118) = 2.299 V
VB = VA·R4/(R2+R4) = 2.299·4/7 = 1.314 V
R1​ = 12 ΩR2​ = 3 ΩR4​ = 4 ΩSHORTR3​10 ΩAIs​5 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. The arrow of Iₛ points down, away from its node, so Iₛ draws current out of that node: its term enters with a minus sign.

R1 ∥ R3 = 5.455 Ω, so the left path is R2+5.455 = 8.455 Ω
Req = R4 ∥ 8.455 = 2.715 Ω
VB = −Is·Req = −5·2.715 = −13.58 V
VA = VB·5.455/8.455 = −8.759 V

Case 3 · V2 acting alone, per volt

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

R1 ∥ R3 = 5.455 Ω
VA‴ = V2·5.455/(4 + 3 + 5.455) = 0.438·V2

Set VA to zero

With VA = 0 there is no voltage across R₃, so its current is zero.

VA′ + VA″ + VA‴ = 2.299 + (−8.759) + 0.438·V2 = 0
V2 = 6.46/0.438 = 14.75 V

Answer

V2 = 14.75 V
9.Thévenin & Norton

Answer: Vth = 2.5 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​ = 20 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 = 10·2/(10+2) = 1.667 Ω
Rth = (R1 ∥ R2) + R3 = 1.667 + 20 = 21.67 Ω
R1​ = 10 ΩR3​ = 20 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/(10+2) = 2.5 V
10.Thévenin & Norton

Answer: PL = 15.3 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​ = 3 ΩR3​ = 5 ΩSHORTR2​30 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 = 3·30/(3+30) = 2.727 Ω
Rth = (R1 ∥ R2) + R3 = 2.727 + 5 = 7.727 Ω
R1​ = 3 ΩR3​ = 5 Ω+−V1​18 VR2​30 ΩAIs​5 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) = 16.36 + (−5)·2.727 = 2.727 V
Vth = VB = VA + Is·R3 = 2.727 + (−5)·5 = −22.27 V
Rth​ = 7.727 Ω−+Vth​22.27 VRL​12 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) = −22.27/(7.727 + 12) = −1.129 A
PL = IL²·RL = −1.129²·12 = 15.3 W
11.RC & RL transients

Answer: vC = 1.01 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.

Thévenin equivalent seen by the capacitor

Short the source to find Rth; open the capacitor to find the voltage it will settle at.

Rth = R1 ∥ R2 = 6.8·1/(6.8 + 1) = 0.8718 kΩ
vC(∞) = 9·1/(6.8 + 1) = 1.154 V

Time constant

τ = Rth·C = 0.8718·22 = 19.18 ms

Charging curve

vC(t) = 1.154·(1 − e−40/19.18) = 1.01 V

Answer

vC = 1.01 V
12.RC & RL transients

Answer: C = 0.8686 µF

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.

Required time constant

8.1 = 9·(1 − e−200/τ) → τ = 200/ln(9/(9 − 8.1))
τ = 200/2.303 = 86.86 ms

Capacitance

kΩ times µF gives milliseconds.

C = τ/R = 86.86/100 = 0.8686 µF

Answer

C = 0.8686 µF
13.AC impedance & phasors

Answer: φ = −50.09 °

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·100 = 628.3 rad/s
XL = ωL = 628.3·0.02 = 12.57 Ω
XC = 1/(ωC) = 1/(628.3·22·10⁻⁶) = 72.34 Ω

Impedance

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

|Z| = √(R² + (XL − XC)²) = √(50² + (−59.78)²) = 77.93 Ω

Phase angle

φ = arctan((XL − XC)/R) = arctan(−59.78/50) = −50.09°

Answer

φ = −50.09°
14.AC impedance & phasors

Answer: I = 4.954 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|.

Reactance

XC = 1/(2π·500·4.7·10⁻⁶) = 67.73 Ω

Parallel combination

Multiply top and bottom by the complex conjugate to split Zp into real and imaginary parts.

Zp = R₂·(−jXC)/(R₂ − jXC) = (R₂·XC² − jR₂²·XC)/(R₂² + XC²)
Zp = 25.08 − j11.11 Ω

Total impedance

Z = 20 + 25.08 − j11.11 = 45.08 − j11.11 Ω
|Z| = √(45.08² + 11.11²) = 46.43 Ω

Current

I = V/|Z| = 230/46.43 = 4.954 A

Answer

I = 4.954 A
15.AC power & power factor

Answer: I = 130 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) = 39000/(400·0.75) = 130 A

Answer

I = 130 A
16.AC power & power factor

Answer: I = 123.8 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.

Reactive power before and after

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

Q1 = 25·tan(arccos 0.8) = 18.75 kvar
QC = V²·2πf·C = 240²·2π·50·150·10⁻⁶ = 2714 var = 2.714 kvar
Q2 = 18.75 − 2.714 = 16.04 kvar

New apparent power

S2 = √(25² + 16.04²) = 29.7 kVA

New line current

I = S2/V = 29701/240 = 123.8 A

Answer

I = 123.8 A
17.Three-phase power

Answer: P = 16.36 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 = 480/√3 = 277.1 V

Phase current

|Z| = √(12² + 5²) = 13 Ω
Iph = 277.1/13 = 21.32 A

Total real power

Only the resistive part of each impedance absorbs real power.

P = 3·Iph²·R = 3·21.32²·12 = 16.36 kW

Answer

P = 16.36 kW

Check: cos φ = R/|Z| = 0.9231, and √3·VL·IL·cos φ gives the same power.

18.Three-phase power

Answer: QC = 34.19 kvar

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 = 75·tan(acos 0.75) = 75·0.8819 = 66.14 kvar
Q2 = 75·tan(acos 0.92) = 75·0.426 = 31.95 kvar

Reactive power from the capacitors

QC = Q1 − Q2 = 34.19 kvar

Answer

QC = 34.19 kvar
19.Transformers

Answer: ILV = 520.8 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.

Rated current

Both windings carry the same apparent power.

ILV = S/V = 250000/480 = 520.8 A

Answer

ILV = 520.8 A
20.Transformers

Answer: Pcu,fl = 2473 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 = 200·0.9 = 180 kW
Pin = 180000/0.98 = 183673 W

Total and copper losses

Ploss = 183673 − 180000 = 3673 W
Pcu,fl = 3673 − 1200 = 2473 W

Answer

Pcu,fl = 2473 W
21.Op-amp circuits

Answer: Vout = 0.8246 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.

Voltage at the + input

V₊ = Vin·Rb/(Ra + Rb) = 0.5·47/(10 + 47) = 0.4123 V

Non-inverting gain

V₋ = V₊, and the current through R₁ also flows through Rf.

Vout = V₊·(1 + Rf/R1) = 0.4123·(1 + 10/10) = 0.8246 V

Answer

Vout = 0.8246 V
22.Op-amp circuits

Answer: Vout = −9 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 current and ramp rate

kΩ times µF gives milliseconds.

RC = 10 kΩ · 1 µF = 10 ms
ramp rate = −Vin/(RC) = −1.8/10 = −0.18 V/ms

Output at the given time

The ideal value lies inside ±Vsat, so the integrator has not clipped yet.

Vout = −Vin·t/(RC) = −1.8·50/10 = −9 V

Answer

Vout = −9 V
23.Diodes & transistors

Answer: VCE = 11.94 V

BJT bias point: in the active region VBE = 0.7 V, IC = β·IB and IE = (β + 1)·IB. Find IB from the base loop with KVL, then IC, then VCE from the collector–emitter loop. A voltage divider at the base is replaced by its Thévenin equivalent VTH = VCC·R₂/(R₁ + R₂), RTH = R₁∥R₂; an emitter resistor appears (β + 1) times larger in the base loop.

Base current

IB = (VCC − VBE)/RB = (15 − 0.7)/560 kΩ = 25.54 µA

Collector current

IC = β·IB = 80·25.54 µA = 2.043 mA

Collector–emitter voltage

VCE = 15 − 2.043 mA·1.5 kΩ = 11.94 V

Answer

VCE = 11.94 V
24.Diodes & transistors

Answer: PZ,max = 237.6 mW

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.

Worst-case Zener current

IZ = 21.9/470 = 46.6 mA

Zener power

PZ = 5.1·46.6 = 237.6 mW

Answer

PZ,max = 237.6 mW
25.Number systems

Answer: N = −50

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.

Add the place values

The other bits keep their normal positive values.

−128 + 64 + 8 + 4 + 2 = −50

Answer

N = −50
26.Number systems

Answer: b = 13 bit

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.

Powers of two

212 = 4096 < 4775
213 = 8192 ≥ 4775

Answer

b = 13
27.Digital logic: gates, K-maps & flip-flops

Answer: AB = 10, CD = 00

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.

Neighbours of each 1

A 1 with a neighbouring 1 can join a group of two or more.

m8: m9, m10, m12, m0 → 0
ABCD0001111000011110111111

The isolated 1

m8 = AB′C′D′ → AB = 10, CD = 00

Answer

AB = 10, CD = 00
28.Digital logic: gates, K-maps & flip-flops

Answer: L = 8

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.

C′D′, A′B′D′, ABD′, A′BC′
ABCD0001111000011110X0010312X4150706112013015X141809011010

Minimal cover

F = C′D′ + A′B′D′ + A′BC′
L = 8

Answer

L = 8
29.Laplace transforms

Answer: A = 17

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).

Factor the denominator

s² + 9s + 20 = (s + 4)(s + 5)
F(s) = A/(s + 4) + B/(s + 5)

Cover-up rule

Multiply by (s + 4) and set s = −4: the B-term vanishes.

A = 17/(s + 5) |s = −4 = 17/1 = 17

Answer

A = 17
(B = −17, so f(t) = 17·e−4t − 17·e−5t)
30.Laplace transforms

Answer: y(0.3) = 1.991

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).

Transform the equation

s²Y − 3s − 4 + 10(sY − 3) + 24Y = 0
Y(s) = (3s + 34)/((s + 4)(s + 6))

Partial fractions

A = 22/2 = 11
B = 16/(−2) = −8

Result

y(t) = 11·e−4t − 8·e−6t
y(0.3) = 1.991

Answer

y(0.3) = 1.991

Check: y(0) = A + B = 3.

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 + 10)(s + 12)) = 0 → s² + 22s + 120 + K = 0

Repeated root

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

22² = 4(120 + K) → K = 484/4 − 120 = 1

Answer

K = 1
Both closed-loop poles are then at s = −11.
32.Block diagrams

Answer: css = 7.625

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) = 10/(s + 10 + 30)
C/R = K·G/(1 + K·G) = 30/(s + 10 + 30)

Steady state

css = 10·30/40 + 0.5·10/40 = 7.625

Answer

css = 7.625

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

33.Step response

Answer: %OS = 5.497 %

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 = 44 → ωₙ = 6.633 rad/s
2ζωₙ = 9 → ζ = 9/(2·6.633) = 0.6784

Result

%OS = 100·e−ζπ/√(1−ζ²) = 100·e−2.901 = 5.497 %

Answer

%OS = 5.497 %
34.Step response

Answer: tp = 0.1421 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).

Natural frequency and damping ratio

ωₙ = √(k/m) = √(2000/4) = 22.36 rad/s
ζ = c/(2√(km)) = 27/(2·√(2000·4)) = 0.1509

Result

ωd = 22.1 rad/s
tp = π/ωd = 0.1421 s

Answer

tp = 0.1421 s
35.Bode plots & margins

Answer: |H| = −7.038 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.

Corner frequency

ωc = 1/(RC) = 1/(2200·4.7 × 10⁻⁹) = 96712 rad/s
fc = 15392 Hz → f/fc = 31000/15392 = 2.014

Gain

|H| = 1/√(1 + 2.014²) = 0.4447
20·log₁₀(0.4447) = −7.038 dB

Answer

|H| = −7.038 dB
36.Bode plots & margins

Answer: ω180 = 6.928 rad/s

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/6)·(ω/8) = 1 → ω180 = √(6·8) = 6.928 rad/s

Answer

ω180 = 6.928 rad/s
37.Stability: Routh–Hurwitz & root locus

Answer: Kmax = 378

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 polynomial

s³ + 11s² + 38s + 40 + K = 0

Routh array

s³: 1, 38
s²: 11, 40 + K
s¹: (11·38 − 40 − K)/11
s⁰: 40 + K

Condition

The s¹ entry must stay positive.

K < 11·38 − 40 = 378

Answer

Kmax = 378

At the limit the loop oscillates at ω = √38 = 6.164 rad/s.

38.Stability: Routh–Hurwitz & root locus

Answer: K = 9

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.

Break-away point

dK/ds = 0 for K = −(s + 4)(s + 10) gives 2s + 14 = 0.

sb = −7

Magnitude condition

K = |−7 + 4|·|−7 + 10| = 3·3 = 9

Answer

K = 9

For this gain the closed loop is critically damped (ζ = 1).

39.Steady-state error & PID control

Answer: ess = 0.125

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.

Acceleration constant

Ka = 2·2/1 = 4

Parabola error

ess = 0.5/4 = 0.125

Answer

ess = 0.125
40.Steady-state error & PID control

Answer: Kd = 0.8814 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 + 1) + 4(2 + Kds) = s² + (1 + 4Kd)s + 8

Natural frequency

ωₙ = √8 = 2.828 rad/s

Derivative gain

1 + 4Kd = 2·0.8·2.828 = 4.525
Kd = 0.8814 s

Answer

Kd = 0.8814 s

The derivative term adds damping without changing ωₙ.

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