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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
Start at the end of the network furthest from the terminals.
Combine resistors in series by adding them, and resistors in parallel with 1/R = 1/R₁ + 1/R₂ + …
Redraw the circuit after each step.
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
Choose a reference node (ground) and label the other node voltages.
Write Kirchhoff’s current law at every unknown node: currents leaving through each branch equal the currents entering.
Express every branch current as (Va − Vb)/R.
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
Draw a clockwise current in every mesh (window) of the circuit.
Apply Kirchhoff’s voltage law around each mesh: the sum of voltage drops is zero.
In a resistor shared by two meshes the current is the difference of the two mesh currents.
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
Count the independent sources. You will solve one simpler circuit per source.
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).
Solve the simpler circuit for the voltage or current you need, keeping track of its direction.
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
Remove the load and mark the two terminals a and b.
Find the open-circuit voltage between a and b: this is Vth.
Switch off all independent sources and find the resistance seen from a–b: this is Rth.
Put the load back on the equivalent circuit: Vth in series with Rth.
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
Find the initial value just after switching: a capacitor voltage and an inductor current cannot jump.
Find the final value long after switching: a capacitor acts as an open circuit, an inductor as a short circuit.
Find the time constant: τ = RC or τ = L/R, using the resistance seen by the capacitor or inductor.
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
Convert the frequency: ω = 2πf.
Find each reactance: XL = ωL and XC = 1/(ωC).
Add impedances like resistors, with Z = R + jX.
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
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.
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.
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.
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
Write the closed-loop characteristic polynomial: the denominator of 1 + K·G(s) = 0, multiplied out.
Put the coefficients alternately into the first two rows of the Routh array and build the remaining rows.
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.
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
Count the poles of the open loop C(s)·G(s) at s = 0: that is the system type.
Work out the error constant that matches the input: Kp for a step, Kv for a ramp, Ka for a parabola.
Apply ess = A/(1 + Kp), A/Kv or A/Ka, or solve it for the gain you need.
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
Find the current IR2 through R2.
V1 = 18 VR1 = 10 ΩR2 = 12 ΩR3 = 4 ΩR4 = 5 Ω
IR2 = A
2.Series & parallel resistorsHard
Find the current IR1 delivered by the source, which flows through R1.
The voltage source Vₛ between A and B has its + terminal at A, so it makes VA − VB = Vₛ. Use nodal analysis with a supernode to find the node voltage VA (measured from ground).
V1 = 6 VIs = 1 AVs = 9 VR1 = 6 ΩR2 = 30 ΩR3 = 4 Ω
VA = V
5.Mesh analysisMedium
Use mesh analysis to find the mesh current I1 (clockwise).
V1 = 9 VV2 = 15 VR1 = 10 ΩR2 = 15 ΩR3 = 2 Ω
I1 = A
6.Mesh analysisHard
Use mesh analysis to find the mesh current I3 (clockwise).
A linear resistive circuit contains three independent sources: V1, V2 and Is. The current I through a load is measured three times. With all sources at their normal values, I = 17.5 mA. With V1 doubled and the other two unchanged, I = 27 mA. With the direction of Is reversed and the other two unchanged, I = 0.5 mA. Find the load current I when V2 is switched off and V1 and Is have their normal values.
normal: I = 17.5 mA2·V1: I = 27 mA−Is: I = 0.5 mA
I = mA
9.Thévenin & NortonMedium
Find the Thévenin resistance Rth seen from terminals a–b.
V1 = 10 VR1 = 2 ΩR2 = 6 ΩR3 = 20 Ω
Rth = Ω
10.Thévenin & NortonHard
Find the Norton current IN: the current that flows from a to b if the terminals are shorted.
V1 = 5 VIs = 1.5 AR1 = 12 ΩR2 = 5 ΩR3 = 15 Ω
IN = A
11.RC & RL transientsMedium
The inductor carries no current before the switch closes at t = 0. Find the current i at t = 1 ms.
Vs = 20 VR = 33 ΩL = 33 mHt = 1 ms
i = A
12.RC & RL transientsHard
The switch has been closed for a long time, so the circuit is in steady state. At t = 0 the switch opens. Find the capacitor voltage vC at t = 500 ms.
Vs = 12 VR1 = 10 kΩR2 = 6.8 kΩC = 33 µFt = 500 ms
vC = V
13.AC impedance & phasorsMedium
A series RLC circuit is connected to a 230 V (rms), 60 Hz supply. Find the phase angle φ of the impedance, in degrees (positive when the current lags the voltage).
V = 230 V (rms)f = 60 HzR = 40 ΩL = 200 mHC = 47 µF
φ = °
14.AC impedance & phasorsHard
A series RLC circuit has R = 5 Ω, L = 10 mH and C = 0.022 µF. Find its bandwidth B (the width of the band between the half-power frequencies), in Hz.
R = 5 ΩL = 10 mHC = 0.022 µF
B = Hz
15.AC power & power factorMedium
An inductive load takes 9.5 A and 1938 W from a 240 V (rms) single-phase supply. Model it as a resistance R in series with a reactance X. Find R.
V = 240 VI = 9.5 AP = 1938 W
R = Ω
16.AC power & power factorHard
A single-phase load takes 10 kW at a power factor of 0.8 lagging from a 230 V, 60 Hz supply. A capacitor connected in parallel raises the power factor to 0.9. Find the new line current Inew.
P = 10 kWpf1 = 0.8pf2 = 0.9V = 230 Vf = 60 Hz
Inew = A
17.Three-phase powerMedium
A balanced three-phase load draws a line current of 40 A from a supply with a line-to-line voltage of 208 V. The power factor is 0.88 lagging. Find the total real power P drawn by the load in kW.
VL = 208 VIL = 40 Acos φ = 0.88
P = kW
18.Three-phase powerHard
A balanced three-phase load takes 250 kW at a power factor of 0.72 lagging from a 690 V (line-to-line), 60 Hz supply. A three-phase capacitor bank in parallel with the load must raise the overall power factor to 0.98 lagging. The real power stays the same. The capacitors are connected in Δ. Find the capacitance Cph of each capacitor in µF.
P = 250 kWpf1 = 0.72pf2 = 0.98VL = 690 Vf = 60 Hz
Cph = µF
19.TransformersMedium
A single-phase 25 kVA, 4800/240 V transformer operates at its rated load. Treat it as ideal. Find the current IHV in the high-voltage winding.
S = 25 kVAV1 = 4800 VV2 = 240 V
IHV = A
20.TransformersHard
A single-phase 150 kVA transformer has a core loss of 900 W. At rated load and a power factor of 0.9 lagging its efficiency is 99%. Find the full-load copper loss Pcu,fl in watts.
S = 150 kVAPcore = 900 Wpf = 0.9η = 99%
Pcu,fl = W
21.Op-amp circuitsMedium
The op-amp is ideal and runs from ±15 V supplies. Find the output voltage Vout.
Vin = −0.3 VR1 = 4.7 kΩRf = 100 kΩ
Vout = V
22.Op-amp circuitsHard
The op-amp is ideal and runs from ±15 V supplies. The resistor ratios are not matched. Find the output voltage Vout.
An NPN transistor with β = 80 has voltage-divider bias from VCC = 18 V: R₁ = 22 kΩ from VCC to the base and R₂ = 15 kΩ from the base to ground. The collector resistor is RC = 1 kΩ and the emitter resistor is RE = 1.2 kΩ. Take VBE = 0.7 V and use the Thévenin equivalent of the divider (do not neglect the base current). Find the collector current IC in mA.
An NPN transistor with β = 100 switches a 330 Ω load resistor connected between VCC = 24 V and its collector. The emitter is grounded. The base is driven from a 5 V logic output through a base resistor RB = 33 kΩ. Take VBE = 0.7 V and VCE(sat) = 0.2 V. Find the collector current IC in mA when the input is high. Decide first whether the transistor is saturated.
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(1, 2, 3, 5, 14)
1AB = 00, CD = 00
2AB = 00, CD = 01
3AB = 00, CD = 11
4AB = 00, CD = 10
5AB = 01, CD = 00
6AB = 01, CD = 01
7AB = 01, CD = 11
8AB = 01, CD = 10
9AB = 11, CD = 00
10AB = 11, CD = 01
11AB = 11, CD = 11
12AB = 11, CD = 10
13AB = 10, CD = 00
14AB = 10, CD = 01
15AB = 10, CD = 11
16AB = 10, CD = 10
28.Digital logic: gates, K-maps & flip-flopsHard
Find the minimal SOP form of F(A, B, C, D) = Σm(0, 1, 7, 14) + d(2, 11, 13, 15), where d marks the don't-care conditions. How many literals L does it contain?
Find f(t) for F(s) = (6s + 19)/(s² + 6s + 9) and evaluate f(0.4).
F(s) = (6s + 19)/(s² + 6s + 9)t = 0.4 s
f(0.4) =
30.Laplace transformsHard
A system obeys y″ + 8y′ + 15y = 45·u(t). It starts at rest (y(0) = 0, y′(0) = 0) and the input is a step u(t) = 2 for t ≥ 0. Use the Laplace transform to find the output y(0.1).
The plant G(s) = 7/(s + 1) has an inner (minor) negative feedback loop with gain H₁ = 0.5. A controller gain K = 13 and an outer unity negative feedback loop close the system. Find the closed-loop pole p.
G(s) = 7/(s + 1)H₁ = 0.5K = 13
p =
32.Block diagramsHard
A proportional controller K drives the plant G(s) = 5/(s + 9) in a unity negative feedback loop. A disturbance step of size 2 enters at the plant input while R = 0. Find the smallest gain K that keeps the steady-state output at or below 0.1111.
G(s) = 5/(s + 9)D = 2css ≤ 0.1111
K =
33.Step responseMedium
A system has the transfer function G(s) = 7/(s² + 2s + 7) and receives a unit step input. Find the 2 % settling time ts of the step response, using ts ≈ 4/(ζωₙ).
G(s) = 7/(s² + 2s + 7)
ts = s
34.Step responseHard
A second-order system without zeros must have a step response with 30 % overshoot. Find the damping ratio ζ.
%OS = 30 %
ζ =
35.Bode plots & marginsMedium
The RL high-pass filter shown has R = 470 Ω, L = 2.2 mH. A sinusoidal input of 100 kHz is applied. Find the gain |H| = |vout/vin| in dB.
R = 470 ΩL = 2.2 mHf = 100 kHz
|H| = dB
36.Bode plots & marginsHard
A unity-feedback loop has the open-loop transfer function L(s) = 60/(s(s + 5)). Find the phase margin PM in degrees.
L(s) = 60/(s(s + 5))
PM = °
37.Stability: Routh–Hurwitz & root locusMedium
The loop in the diagram has negative feedback and L(s) = 1120/(s(s + 4)(s + 10)). How many closed-loop poles N lie in the right half-plane?
L(s) = 1120/(s(s + 4)(s + 10))
N =
38.Stability: Routh–Hurwitz & root locusHard
The root locus of L(s) = K(s + 5)/(s(s + 1)) leaves the real axis between s = 0 and s = −1, circles round and joins the real axis again to the left of the zero. Find the break-away point sb.
L(s) = K(s + 5)/(s(s + 1))
sb =
39.Steady-state error & PID controlMedium
A process G(s) = 2/(0.5s + 1) is controlled by a proportional gain K = 2 in a unity-feedback loop. Find the steady-state error ess for a step, as a percentage of the step size.
G(s) = 2/(0.5s + 1)K = 2
ess = %
40.Steady-state error & PID controlHard
A PD controller C(s) = 8 + Kd·s drives the plant G(s) = 5/(s(s + 3)) in a unity-feedback loop. Find the derivative gain Kd that gives the closed loop a damping ratio ζ = 0.8.
G(s) = 5/(s(s + 3))Kp = 8ζ = 0.8
Kd = s
3Solutions
1.Series & parallel resistors
Answer: IR2 = 0.5094 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.
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 = 4 + 5 = 9 Ω
R2 ∥ 9 = 12·9/(12+9) = 5.143 Ω
Req = R1 + 5.143 = 10 + 5.143 = 15.14 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 = 18/15.14 = 1.189 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 = 18 − 1.189·10 = 6.113 V
IR2 = VA/R2 = 6.113/12 = 0.5094 A
Answer
IR2 = 0.5094 A
2.Series & parallel resistors
Answer: IR1 = 1.301 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.
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 + 6 = 31 Ω
R4 ∥ 31 = 3.543 Ω
R3 + 3.543 = 28.54 Ω
R2 ∥ 28.54 = 8.448 Ω
Req = R1 + 8.448 = 10 + 8.448 = 18.45 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 = 24/18.45 = 1.301 A
Answer
IR1 = 1.301 A
3.Nodal analysis
Answer: PIs = 101.3 W
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
Currents leaving A through the resistors equal the current pushed into A by sources.
VA/R2 + (VA − V1)/R1 + (VA − VB)/R3 = 0
VA/10 + (VA − 9)/15 + (VA − VB)/20 = 0
0.2167·VA − 0.05·VB = 0.6
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/8 + (VB − VA)/20 = 4
−0.05·VA + 0.175·VB = 4
Solve
Δ = (0.2167)(0.175) − (−0.05)(−0.05) = 0.03542
VA = Δ1/Δ = 0.305/0.03542 = 8.612 V
VB = Δ2/Δ = 0.8967/0.03542 = 25.32 V
Power delivered by the current source
The source pushes Iₛ up into node B, from ground (0 V) to VB. A source whose current leaves its + end delivers P = V·I.
PIs = VB·Is = 25.32·4 = 101.3 W
Answer
PIs = 101.3 W
4.Nodal analysis
Answer: VA = 9.444 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.
Form a supernode
The voltage source between A and B carries an unknown current, so KCL cannot be written at A or B separately. Enclose A, B and the source in one supernode: the current entering it equals the current leaving it.
VB = VA − 9
(VA − V1)/R1 + VA/R2 + VB/R3 = Is
Solve
(VA − 6)/6 + VA/30 + (VA − 9)/4 = 1
VA·(1/6 + 1/30 + 1/4) = 1 + 6/6 + 9/4 = 4.25
VA = 4.25/0.45 = 9.444 V
VB = 0.4444 V
Answer
VA = 9.444 V
5.Mesh analysis
Answer: I1 = 0.615 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.
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 + 2(I1 − I2) = 9
12·I1 − 2·I2 = 9
KVL around mesh 2
Going clockwise, the voltage drops across resistors equal the source voltage rises (− to + in the direction of travel).
R2·I2 + R3(I2 − I1) = −V2
15·I2 + 2(I2 − I1) = (−15)
−2·I1 + 17·I2 = −15
Solve
Δ = (12)(17) − (−2)(−2) = 200
I1 = Δ1/Δ = 123/200 = 0.615 A
I2 = Δ2/Δ = −162/200 = −0.81 A
Answer
I1 = 0.615 A
A negative mesh current flows anticlockwise.
6.Mesh analysis
Answer: I3 = −2.828 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.
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
12·I1 + 6(I1 − I2) = 12
18·I1 − 6·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 + R4(I2 − I1) + R5(I2 − I3) = 0
6·I2 + 6(I2 − I1) + 20(I2 − I3) = 0
−6·I1 + 32·I2 − 20·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
3·I3 + 20(I3 − I2) = (−30)
−20·I2 + 23·I3 = −30
Solve
Δ = det of the coefficient matrix = 5220
I1 = Δ1/Δ = 432/5220 = 0.08276 A
I2 = Δ2/Δ = −9144/5220 = −1.752 A
I3 = Δ3/Δ = −14760/5220 = −2.828 A
Answer
I3 = −2.828 A
A negative mesh current flows anticlockwise.
7.Superposition
Answer: IR1 = −4.118 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.
Case 1 · V1 acting alone
Iₛ becomes an open circuit, so R₃ and R₄ form one series branch from A to ground, in parallel with R₂.
R3+R4 = 2+10 = 12 Ω
R2 ∥ (R3+R4) = 8·12/(8+12) = 4.8 Ω
VA = 12·4.8/(2+4.8) = 8.471 V
VB = VA·R4/(R3+R4) = 8.471·10/12 = 7.059 V
IR1′ = (VA − V1)/R1 = (8.471 − 12)/2 = −1.765 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 = 2·8/(2+8) = 1.6 Ω
Req = R4 ∥ (R3+R1∥R2) = 10 ∥ 3.6 = 2.647 Ω
VB = Is·Req = (−4)·2.647 = −10.59 V
VA = VB·(R1∥R2)/(R3+R1∥R2) = −10.59·1.6/3.6 = −4.706 V
IR1″ = (VA − V1)/R1 = (−4.706 − 0)/2 = −2.353 A
Add the contributions
IR1 = IR1′ + IR1″
IR1 = (−1.765) + (−2.353) = −4.118 A
A negative result means the real current flows against the arrow.
8.Superposition
Answer: I = 18 mA
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.
Write the measurements with contributions
Each contribution is proportional to its own source.
I₁ + I₂ + I₃ = 17.5
2·I₁ + I₂ + I₃ = 27
I₁ + I₂ − I₃ = 0.5
Solve for the contributions
I₁ = 27 − 17.5 = 9.5 mA
I₃ = (17.5 − 0.5)/2 = 8.5 mA
I₂ = 17.5 − 9.5 − 8.5 = −0.5 mA
Switch V₂ off
I = I₁ + I₃ = 9.5 + 8.5 = 18 mA
Answer
I = 18 mA
9.Thévenin & Norton
Answer: Rth = 21.5 Ω
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.
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 = 2·6/(2+6) = 1.5 Ω
Rth = (R1 ∥ R2) + R3 = 1.5 + 20 = 21.5 Ω
10.Thévenin & Norton
Answer: IN = 1.579 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.
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 = 12·5/(12+5) = 3.529 Ω
Rth = (R1 ∥ R2) + R3 = 3.529 + 15 = 18.53 Ω
Find Vth, the open-circuit voltage
With a–b open, the only path for Iₛ is through R₃ into node A. Find V_A by superposition of V₁ and Iₛ, then add the drop across R₃.
VA = V1·R2/(R1+R2) + Is·(R1∥R2) = 1.471 + 1.5·3.529 = 6.765 V
Vth = VB = VA + Is·R3 = 6.765 + 1.5·15 = 29.26 V
Norton equivalent
A Norton source is the same circuit seen as a current source in parallel with R_th. Its current is the short-circuit current at a–b.
IN = Vth/Rth = 29.26/18.53 = 1.579 A
11.RC & RL transients
Answer: i = 0.3831 A
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.
First-order transients: in a circuit with one capacitor or one inductor, every voltage and current moves exponentially from its initial value to its final value: x(t) = x(∞) + [x(0) − x(∞)]·e−t/τ, with τ = RC or τ = L/R. After about 5τ the circuit has settled.
Initial capacitor voltage
In steady state the capacitor is an open circuit, so R₁ and R₂ form a voltage divider. The capacitor voltage cannot jump when the switch opens.
vC(0) = 12·6.8/(10 + 6.8) = 4.857 V
Time constant after the switch opens
τ = R2·C = 6.8·33 = 224.4 ms
Discharge
vC(t) = 4.857·e−500/224.4 = 0.5232 V
Answer
vC = 0.5232 V
13.AC impedance & phasors
Answer: φ = 25.36 °
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·60 = 377 rad/s
XL = ωL = 377·0.2 = 75.4 Ω
XC = 1/(ωC) = 1/(377·47·10⁻⁶) = 56.44 Ω
Impedance
In series the impedances add as complex numbers: Z = R + j(XL − XC).
AC circuits with phasors: resistors, inductors and capacitors have impedances R, jωL and 1/(jωC), with ω = 2πf. In series, impedances add like resistances, but as complex numbers. Rms current and voltage follow Ohm’s law with |Z|.
Resonant frequency
f0 = 1/(2π·√(0.01·0.022·10⁻⁶)) = 10730 Hz
Quality factor
Q compares the reactance at resonance with the resistance: Q = ω₀L/R.
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.
Resistance from the real power
R = P/I² = 1938/9.5² = 21.47 Ω
Answer
R = 21.47 Ω
16.AC power & power factor
Answer: Inew = 48.31 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 = P·tan φ1 = 10·tan(36.87°) = 7.5 kvar
Q2 = P·tan φ2 = 10·tan(25.84°) = 4.843 kvar
QC = Q1 − Q2 = 2.657 kvar
New line current
Inew = P/(V·cos φ2) = 10000/(230·0.9) = 48.31 A
Answer
Inew = 48.31 A
17.Three-phase power
Answer: P = 12.68 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.
Apparent power
S = √3·VL·IL = √3·208·40 = 14.41 kVA
Real power
P = S·cos φ = 14.41·0.88 = 12.68 kW
Answer
P = 12.68 kW
18.Three-phase power
Answer: Cph = 353.2 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 = 250·tan(acos 0.72) = 250·0.9639 = 241 kvar
Q2 = 250·tan(acos 0.98) = 250·0.2031 = 50.76 kvar
Reactive power from the capacitors
QC = Q1 − Q2 = 190.2 kvar
Capacitance per phase
In a Δ bank each capacitor is connected between two lines.
V = 690 V, ω = 2π·60 = 377 rad/s
Cph = (QC/3)/(ω·V²) = 63400/(377·690²) = 353.2 µF
Answer
Cph = 353.2 µF
19.Transformers
Answer: IHV = 5.208 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.
IHV = S/V = 25000/4800 = 5.208 A
Answer
IHV = 5.208 A
20.Transformers
Answer: Pcu,fl = 463.6 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 = 150·0.9 = 135 kW
Pin = 135000/0.99 = 136364 W
Total and copper losses
Ploss = 136364 − 135000 = 1364 W
Pcu,fl = 1364 − 900 = 463.6 W
Answer
Pcu,fl = 463.6 W
21.Op-amp circuits
Answer: Vout = −6.683 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.
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₊ = V2·R4/(R3 + R4) = 0.3·2/(2 + 2) = 0.15 V
Superpose the two inputs
With V₂ = 0, V₁ sees an inverting amplifier. With V₁ = 0, V₊ is amplified by the non-inverting gain 1 + R₂/R₁.
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.
Thévenin equivalent of the divider
VTH = 18·15/(22 + 15) = 7.297 V
RTH = 22·15/(22 + 15) = 8.919 kΩ
Base current
KVL around the base loop; the emitter current is (β + 1)·IB.
IB = (7.297 − 0.7)/(8.919 + 81·1.2) = 62.17 µA
Collector current
IC = 80·62.17 µA = 4.974 mA
IE = 81·62.17 µA = 5.036 mA
Answer
IC = 4.974 mA
24.Diodes & transistors
Answer: IC = 13.03 mA
BJT as a switch: to switch a load fully on, the transistor is driven into saturation, where VCE = VCE(sat) and the collector current is set by the load: IC(sat) = (VCC − VCE(sat))/RC. Saturation needs at least IB = IC(sat)/β. If the base current is smaller, the transistor stays active and IC = β·IB.
Base current
IB = (5 − 0.7)/33 kΩ = 130.3 µA
Saturated or active?
β·IB is smaller than IC(sat), so the transistor stays active.
β·IB = 13.03 mA
IC(sat) = (24 − 0.2)/330 = 72.12 mA
Collector current
IC = β·IB = 13.03 mA
Answer
IC = 13.03 mA
The transistor is active, so the load is not fully switched on.
25.Number systems
Answer: U = 226
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
30 = 0001 1110
inverted: 1110 0001
+1 → 1110 0010
Read it as unsigned
1110 0010₂ = 256 − 30 = 226
Answer
U = 226
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 < 4907
213 = 8192 ≥ 4907
Answer
b = 13
27.Digital logic: gates, K-maps & flip-flops
Answer: AB = 11, CD = 10
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.
m14: m15, m12, m10, m6 → 0
The isolated 1
m14 = ABCD′ → AB = 11, CD = 10
Answer
AB = 11, CD = 10
28.Digital logic: gates, K-maps & flip-flops
Answer: L = 9
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.
BCD, A′B′D′, A′B′C′, ABC
Minimal cover
F = BCD + A′B′C′ + ABC
L = 9
Answer
L = 9
29.Laplace transforms
Answer: f(0.4) = 1.928
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 + 6s + 9 = (s + 3)²
Partial fractions
6s + 19 = 6(s + 3) + 1
F(s) = 6/(s + 3) + 1/(s + 3)²
Inverse transform
f(t) = 6·e−3t + t·e−3t
f(0.4) = (6 + 1·0.4)·e−3·0.4 = 1.928
Answer
f(0.4) = 1.928
30.Laplace transforms
Answer: y(0.1) = 0.3465
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
Y(s) = 90/(s(s + 3)(s + 5))
Partial fractions
A = 90/(3·5) = 6
B = 90/((−3)·2) = −15
C = 90/((−5)·(−2)) = 9
Output
y(t) = 6 − 15·e−3t + 9·e−5t
y(0.1) = 0.3465
Answer
y(0.1) = 0.3465
31.Block diagrams
Answer: p = −95.5
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).
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).
Disturbance response
css = D·G(0)/(1 + K·G(0)) = 2·5/(9 + 5K)
Solve for K
9 + 5K = 2·5/0.1111 = 90
K = (90 − 9)/5 = 16.2
Answer
K = 16.2
33.Step response
Answer: ts = 4 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).
Compare with the standard form
The denominator must match s² + 2ζωₙs + ωₙ².
ωₙ² = 7 → ωₙ = 2.646 rad/s
2ζωₙ = 2 → ζ = 2/(2·2.646) = 0.378
Result
ζωₙ = 1 → ts ≈ 4/1 = 4 s
Answer
ts = 4 s
34.Step response
Answer: ζ = 0.3579
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).
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 = R/L = 470/0.0022 = 213636 rad/s
fc = 34001 Hz → f/fc = 100000/34001 = 2.941
Gain
|H| = 2.941/√(1 + 2.941²) = 0.9468
20·log₁₀(0.9468) = −0.4751 dB
Answer
|H| = −0.4751 dB
36.Bode plots & margins
Answer: PM = 35.6 °
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 + 25ω² − 3600 = 0
ω² = (−25 + √(625 + 4·3600))/2 = 48.79
ωc = 6.985 rad/s
Phase margin
∠L(jωc) = −90° − atan(6.985/5) = −144.4°
PM = 180° + ∠L = 35.6°
Answer
PM = 35.6°
37.Stability: Routh–Hurwitz & root locus
Answer: N = 2
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 + 14s² + 40s + 1120 = 0
Routh array
s³: 1, 40
s²: 14, 1120
s¹: −40
s⁰: 1120
Sign changes in the first column
1 → 14 → −40 → 1120
N = 2
Answer
N = 2
The gain is above the limit K = 560, so a complex pair has crossed into the right half-plane.
38.Stability: Routh–Hurwitz & root locus
Answer: sb = −0.5279
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 + 1s)/(s + 5)
Stationary points
Differentiate with the quotient rule and set the numerator to zero.
(2s + 1)(s + 5) − (s² + 1s) = s² + 10s + 5 = 0
s = −5 ± √20 = −0.5279, −9.472
Break-away point
sb = −0.5279
Answer
sb = −0.5279
Between the two break points the locus is a circle centred on the zero, with radius √20 = 4.472.
39.Steady-state error & PID control
Answer: ess = 20 %
Steady-state error: in a unity-feedback loop with open-loop transfer function G(s) the error is E(s) = R(s)/(1 + G(s)), and by the final value theorem ess = lims→0 s·E(s). The system type is the number of poles of G(s) at s = 0. The error constants are Kp = lim G(s), Kv = lim s·G(s) and Ka = lim s²·G(s), all for s → 0. A step of size A gives ess = A/(1 + Kp), a ramp A·t gives A/Kv and a parabola A·t²/2 gives A/Ka. A type-0 loop follows a step with a finite error, a type-1 loop follows it exactly and a ramp with a finite error.
Position constant
Kp = 2·2 = 4
Step error
ess = 100/(1 + 4) = 20 %
Answer
ess = 20 %
40.Steady-state error & PID control
Answer: Kd = 1.424 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 + 3) + 5(8 + Kds) = s² + (3 + 5Kd)s + 40
Natural frequency
ωₙ = √40 = 6.325 rad/s
Derivative gain
3 + 5Kd = 2·0.8·6.325 = 10.12
Kd = 1.424 s
Answer
Kd = 1.424 s
The derivative term adds damping without changing ωₙ.
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