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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 equivalent resistance Req seen by the source V1.
Three branches are connected between node A and ground, as shown. Use nodal analysis to find the current I1 in branch 1, flowing up into node A in the direction of the arrow.
V1 = 15 VR1 = 20 ΩV2 = 10 VR2 = 4 ΩR3 = 15 Ω
I1 = A
4.Nodal analysisHard
The diamond is a voltage-controlled current source that pushes a current of 0.05·VA (in A, with VA in V) up into node B. Use nodal analysis to find the node voltage VA (measured from ground).
The inductor carries a steady current of 2.5 A. At t = 0 the switch closes the loop through R and the source is removed, so the inductor current decays through R. Find the current i at t = 5 ms.
i(0) = 2.5 AR = 15 ΩL = 100 mHt = 5 ms
i = A
12.RC & RL transientsHard
Just before the switch closes at t = 0, the capacitor holds 2 V with the polarity shown. Find the capacitor voltage vC at t = 1000 ms.
Vs = 9 VR = 10 kΩC = 47 µFvC(0) = 2 Vt = 1000 ms
vC = V
13.AC impedance & phasorsMedium
A series RLC circuit with L = 20 mH must resonate at 200 Hz. Find the capacitance C needed.
f0 = 200 HzL = 20 mH
C = µF
14.AC impedance & phasorsHard
A series RLC circuit is connected to a 24 V (rms), 200 Hz supply. Find the resonant frequency f0 of the circuit.
V = 24 V (rms)f = 200 HzR = 40 ΩL = 100 mHC = 1 µF
f0 = Hz
15.AC power & power factorMedium
An inductive load takes 7.5 A and 630 W from a 120 V (rms) single-phase supply. Model it as a resistance R in series with a reactance X. Find R.
V = 120 VI = 7.5 AP = 630 W
R = Ω
16.AC power & power factorHard
A single-phase load takes 25 kW at a power factor of 0.6 lagging from a 400 V, 50 Hz supply. A capacitor connected in parallel raises the power factor to 0.98. Find the reactive power QC the capacitor must supply.
P = 25 kWpf1 = 0.6pf2 = 0.98V = 400 Vf = 50 Hz
QC = kvar
17.Three-phase powerMedium
A balanced three-phase load draws a line current of 15 A from a supply with a line-to-line voltage of 480 V. The power factor is 0.92 lagging. Find the total real power P drawn by the load in kW.
VL = 480 VIL = 15 Acos φ = 0.92
P = kW
18.Three-phase powerHard
A balanced three-phase load takes 80 kW at a power factor of 0.8 lagging from a 690 V (line-to-line), 50 Hz supply. A three-phase capacitor bank in parallel with the load must raise the overall power factor to 0.95 lagging. The real power stays the same. Find the total reactive power QC the capacitor bank must supply, in kvar.
P = 80 kWpf1 = 0.8pf2 = 0.95VL = 690 Vf = 50 Hz
QC = kvar
19.TransformersMedium
A single-phase 150 kVA, 480/240 V transformer operates at its rated load. Treat it as ideal. Find the current IHV in the high-voltage winding.
S = 150 kVAV1 = 480 VV2 = 240 V
IHV = A
20.TransformersHard
A single-phase 150 kVA transformer has a core loss of 900 W and a copper loss of 3600 W at rated load. At what load Sη,max, in kVA, is its efficiency highest?
S = 150 kVAPcore = 900 WPcu,fl = 3600 W
Sη,max = kVA
21.Op-amp circuitsMedium
The op-amp is ideal and runs from ±15 V supplies. Find the output voltage Vout.
Vin = −1.5 VR1 = 2 kΩRf = 2 kΩ
Vout = V
22.Op-amp circuitsHard
The summing amplifier uses an ideal op-amp with ±15 V supplies. Find the current If through the feedback resistor, flowing towards the output.
An NPN transistor with β = 80 has voltage-divider bias from VCC = 20 V: R₁ = 82 kΩ from VCC to the base and R₂ = 6.8 kΩ from the base to ground. The collector resistor is RC = 2.2 kΩ and the emitter resistor is RE = 1 kΩ. Take VBE = 0.7 V and use the Thévenin equivalent of the divider (do not neglect the base current). Find the collector–emitter voltage VCE.
An NPN transistor with β = 100 switches a 470 Ω load resistor connected between VCC = 24 V and its collector. The emitter is grounded. The base is driven from a 3.3 V logic output through a base resistor RB. Take VBE = 0.7 V and VCE(sat) = 0.2 V. For reliable switching, design for a base current 5 times the minimum needed for saturation. Find RB in kΩ.
Use the Karnaugh map to find the minimal sum-of-products (SOP) form of F(A, B, C, D) = Σm(0, 2, 3, 4, 7, 12, 13, 14, 15). How many literals L does it contain in total (a primed variable counts as one literal)?
F(A, B, C, D) = Σm(0, 2, 3, 4, 7, 12, 13, 14, 15)
L =
28.Digital logic: gates, K-maps & flip-flopsHard
For F(A, B, C, D) = Σm(1, 6, 7, 14) + d(3, 8, 9, 11), where d marks the don't-care conditions, find the number N of essential prime implicants.
F(A, B, C, D) = Σm(1, 6, 7, 14) + d(3, 8, 9, 11)
N =
29.Laplace transformsMedium
F(s) = (6s + 32)/(s² + 15s + 56). Its inverse transform has the form f(t) = A·e−7t + B·e−8t. Find the coefficient A by partial fractions.
F(s) = (6s + 32)/(s² + 15s + 56)
A =
30.Laplace transformsHard
Solve y″ + 6y′ + 8y = 0 with y(0) = 4 and y′(0) = −10 using the Laplace transform, and find y(0.3).
y″ + 6y′ + 8y = 0y(0) = 4y′(0) = −10t = 0.3 s
y(0.3) =
31.Block diagramsMedium
A unity negative feedback loop has G(s) = 2(s + 2)/((s + 1)(s + 5)). A step of size 5 is applied at the reference. Find the steady-state error ess.
G(s) = 2(s + 2)/((s + 1)(s + 5))R = 5
ess =
32.Block diagramsHard
The plant G(s) = K/((s + 2)(s + 4)(s + 6)) is in a unity negative feedback loop. At the largest stable gain the loop oscillates. Find the frequency of oscillation ω in rad/s.
A system has the transfer function G(s) = 144/(s² + 4s + 72) and receives a unit step input. Find the damping ratio ζ.
G(s) = 144/(s² + 4s + 72)
ζ =
34.Step responseHard
A unity negative feedback loop has G(s) = K/(s(s + 5)). Find the gain K that gives a step response with 30 % overshoot.
G(s) = K/(s(s + 5))%OS = 30 %
K =
35.Bode plots & marginsMedium
Find the exact magnitude |G(jω)| of G(s) = 126/((s + 3)(s + 7)) at ω = 1 rad/s, in dB.
G(s) = 126/((s + 3)(s + 7))ω = 1 rad/s
|G(jω)| = dB
36.Bode plots & marginsHard
A unity-feedback loop has the open-loop transfer function L(s) = 360/(s(s + 20)). Find the phase margin PM in degrees.
L(s) = 360/(s(s + 20))
PM = °
37.Stability: Routh–Hurwitz & root locusMedium
The loop in the diagram uses positive feedback, with L(s) = 50/(s(s + 6)(s + 8)). How many closed-loop poles N lie in the right half-plane?
L(s) = 50/(s(s + 6)(s + 8))
N =
38.Stability: Routh–Hurwitz & root locusHard
For L(s) = K/((s + 4)(s² + 6s + 10)), find the angle of departure θd of the root locus from the complex pole in the upper half-plane, measured from the positive real axis.
L(s) = K/((s + 4)(s² + 6s + 10))
θd = °
39.Steady-state error & PID controlMedium
The parabolic input r(t) = 2·t²/2 is applied to a unity-feedback loop with G(s) = 10(s + 4)/(s²(s + 5)). Find the steady-state error ess.
G(s) = 10(s + 4)/(s²(s + 5))r(t) = 2·t²/2
ess =
40.Steady-state error & PID controlHard
A proportional controller K drives the plant G(s) = 1/(s(s + 10)) in a unity-feedback loop. Find the gain K that gives the closed loop a damping ratio ζ = 0.4.
G(s) = 1/(s(s + 10))ζ = 0.4
K =
3Solutions
1.Series & parallel resistors
Answer: Req = 19.62 Ω
Series and parallel resistors: in series the same current flows through each resistor and R = R₁ + R₂ + …. In parallel each resistor has the same voltage and 1/R = 1/R₁ + 1/R₂ + …. A ladder network is reduced one pair at a time until a single equivalent resistance remains.
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 = 5 + 15 = 20 Ω
R2 ∥ 20 = 6·20/(6+20) = 4.615 Ω
Req = R1 + 4.615 = 15 + 4.615 = 19.62 Ω
Answer
Req = 19.62 Ω
2.Series & parallel resistors
Answer: IR2 = 0.2514 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 = 6 + 6 = 12 Ω
R4 ∥ 12 = 8.108 Ω
R3 + 8.108 = 38.11 Ω
R2 ∥ 38.11 = 5.184 Ω
Req = R1 + 5.184 = 12 + 5.184 = 17.18 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 = 5/17.18 = 0.291 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 = 5 − 0.291·12 = 1.508 V
IR2 = VA/R2 = 1.508/6 = 0.2514 A
Answer
IR2 = 0.2514 A
3.Nodal analysis
Answer: I1 = −0.9886 A
Nodal analysis: choose a reference node, label the unknown node voltages, write Kirchhoff’s current law at each unknown node using Ohm’s law (I = ΔV/R), and solve the resulting equations.
KCL at node A
Take the bottom wire as ground. Each branch carries (VA − Vk)/Rk away from A, where Vk is the voltage of its source (zero for a plain resistor). The currents leaving A add up to zero.
(VA − (−15))/20 + (VA − 10)/4 + VA/15 = 0
Solve for VA
VA = ((−15)/20 + 10/4 + 0/15) / (1/20 + 1/4 + 1/15) = 1.75/0.3667 = 4.773 V
Branch current
The arrow points up through the branch, into node A.
A negative result means the real current flows against the arrow.
4.Nodal analysis
Answer: VA = 1.091 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.
KCL at node A
Currents leaving A through the resistors equal the current pushed into A by sources.
(VA − V1)/R1 + VA/R2 + (VA − VB)/R3 = 0
0.4·VA − 0.2·VB = 0.3
KCL at node B
The dependent source pushes g·VA into node B. Treat it like an independent source, then move the VA term to the left-hand side.
(VB − VA)/R3 + VB/R4 = 0.05·VA
−0.25·VA + 0.4·VB = 0
Solve
Δ = (0.4)(0.4) − (−0.2)(−0.25) = 0.11
VA = Δ1/Δ = 0.12/0.11 = 1.091 V
VB = Δ2/Δ = 0.075/0.11 = 0.6818 V
Answer
VA = 1.091 V
5.Mesh analysis
Answer: I1 = 0.4545 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
8·I1 + 6(I1 − I2) = 10
14·I1 − 6·I2 = 10
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
6·I2 + 6(I2 − I1) = (−10)
−6·I1 + 12·I2 = −10
Solve
Δ = (14)(12) − (−6)(−6) = 132
I1 = Δ1/Δ = 60/132 = 0.4545 A
I2 = Δ2/Δ = −80/132 = −0.6061 A
Answer
I1 = 0.4545 A
A negative mesh current flows anticlockwise.
6.Mesh analysis
Answer: I3 = −0.4913 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
30·I1 + 8(I1 − I2) = 18
38·I1 − 8·I2 = 18
KVL around mesh 2
Going clockwise, the voltage drops across resistors equal the source voltage rises (− to + in the direction of travel).
R2·I2 + R4(I2 − I1) + R5(I2 − I3) = 0
20·I2 + 8(I2 − I1) + 15(I2 − I3) = 0
−8·I1 + 43·I2 − 15·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
8·I3 + 15(I3 − I2) = (−10)
−15·I2 + 23·I3 = −10
Solve
Δ = det of the coefficient matrix = 27560
I1 = Δ1/Δ = 12552/27560 = 0.4554 A
I2 = Δ2/Δ = −2388/27560 = −0.08665 A
I3 = Δ3/Δ = −13540/27560 = −0.4913 A
Answer
I3 = −0.4913 A
A negative mesh current flows anticlockwise.
7.Superposition
Answer: VR4 = 17.42 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.
Case 1 · V1 acting alone
Iₛ becomes an open circuit, so R₃ and R₄ form one series branch from A to ground, in parallel with R₂.
R3+R4 = 20+10 = 30 Ω
R2 ∥ (R3+R4) = 2·30/(2+30) = 1.875 Ω
VA = 18·1.875/(2+1.875) = 8.71 V
VB = VA·R4/(R3+R4) = 8.71·10/30 = 2.903 V
VR4′ = 0 − VB = 0 − 2.903 = −2.903 V
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 = 2·2/(2+2) = 1 Ω
Req = R4 ∥ (R3+R1∥R2) = 10 ∥ 21 = 6.774 Ω
VB = Is·Req = (−3)·6.774 = −20.32 V
VA = VB·(R1∥R2)/(R3+R1∥R2) = −20.32·1/21 = −0.9677 V
VR4″ = 0 − VB = 0 − −20.32 = 20.32 V
Add the contributions
VR4 = VR4′ + VR4″
VR4 = (−2.903) + 20.32 = 17.42 V
A negative result means the real polarity is opposite to the one marked.
8.Superposition
Answer: IR2 = 1.876 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
V₂ becomes a short and Iₛ an open circuit. Seen from A, R₃ is in parallel with the series pair R₂+R₄.
A negative result means the real current flows against the arrow.
9.Thévenin & Norton
Answer: Rth = 16.71 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 = 4·3/(4+3) = 1.714 Ω
Rth = (R1 ∥ R2) + R3 = 1.714 + 15 = 16.71 Ω
10.Thévenin & Norton
Answer: PL = 21.14 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.
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 = 15·15/(15+15) = 7.5 Ω
Rth = (R1 ∥ R2) + R3 = 7.5 + 30 = 37.5 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) = 5 + (−3)·7.5 = −17.5 V
Vth = VB = VA + Is·R3 = −17.5 + (−3)·30 = −107.5 V
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) = −107.5/(37.5 + 3) = −2.654 A
PL = IL²·RL = −2.654²·3 = 21.14 W
11.RC & RL transients
Answer: i = 1.181 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
τ = L/R = 100 mH / 15 Ω = 6.667 ms
Decay of the current
i(t) = 2.5·e−5/6.667 = 1.181 A
Answer
i = 1.181 A
12.RC & RL transients
Answer: vC = 8.166 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.
Initial value, final value, time constant
The capacitor voltage cannot jump, so it starts at its stored value and heads for the source voltage.
vC(0) = 2 V, vC(∞) = Vs = 9 V
τ = R·C = 10 kΩ · 47 µF = 470 ms
vC(t) = 9 + (2 − 9)·e−t/τ
Voltage at the given time
vC(1000) = 9 + (−7)·e−1000/470 = 8.166 V
Answer
vC = 8.166 V
13.AC impedance & phasors
Answer: C = 31.66 µF
AC circuits with phasors: resistors, inductors and capacitors have impedances R, jωL and 1/(jωC), with ω = 2πf. In series, impedances add like resistances, but as complex numbers. Rms current and voltage follow Ohm’s law with |Z|.
Resonance condition
At resonance the inductive and capacitive reactances cancel: ωL = 1/(ωC).
ω₀ = 2π·200 = 1257 rad/s
C = 1/(ω₀²·L) = 1/(1257²·0.02) = 31.66 µF
Answer
C = 31.66 µF
14.AC impedance & phasors
Answer: f0 = 503.3 Hz
AC circuits with phasors: resistors, inductors and capacitors have impedances R, jωL and 1/(jωC), with ω = 2πf. In series, impedances add like resistances, but as complex numbers. Rms current and voltage follow Ohm’s law with |Z|.
Resonance
At resonance the inductive and capacitive reactances cancel: ωL = 1/(ωC). The supply frequency does not matter.
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 = 630/7.5² = 11.2 Ω
Answer
R = 11.2 Ω
16.AC power & power factor
Answer: QC = 28.26 kvar
AC power: apparent power S = V·I (VA) splits into real power P = S·cos φ (W), which does useful work, and reactive power Q = S·sin φ (var), which moves back and forth between source and load. The power factor is cos φ. A capacitor in parallel supplies reactive power locally, so the line current drops for the same real power.
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 = 25·tan(53.13°) = 33.33 kvar
Q2 = P·tan φ2 = 25·tan(11.48°) = 5.076 kvar
QC = Q1 − Q2 = 28.26 kvar
Answer
QC = 28.26 kvar
17.Three-phase power
Answer: P = 11.47 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 = √3·480·15 = 12.47 kVA
Real power
P = S·cos φ = 12.47·0.92 = 11.47 kW
Answer
P = 11.47 kW
18.Three-phase power
Answer: QC = 33.71 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 = 80·tan(acos 0.8) = 80·0.75 = 60 kvar
Q2 = 80·tan(acos 0.95) = 80·0.3287 = 26.29 kvar
Reactive power from the capacitors
QC = Q1 − Q2 = 33.71 kvar
Answer
QC = 33.71 kvar
19.Transformers
Answer: IHV = 312.5 A
Ideal transformer: the voltages are in the ratio of the turns and the currents in the inverse ratio: V₁/V₂ = N₁/N₂ = a and I₁/I₂ = N₂/N₁ = 1/a, so the power in equals the power out, V₁·I₁ = V₂·I₂. A load impedance Z on the secondary looks like a²·Z from the primary.
Rated current
Both windings carry the same apparent power.
IHV = S/V = 150000/480 = 312.5 A
Answer
IHV = 312.5 A
20.Transformers
Answer: Sη,max = 75 kVA
Transformer losses: the core loss (hysteresis and eddy currents) depends on the voltage and is the same at any load. The copper loss in the windings goes with the current squared, so at a fraction x of rated load it is x²·Pcu,fl. Efficiency η = Pout/(Pout + Pcore + Pcu), with Pout = x·S·pf. The efficiency is highest at the load where the copper loss equals the core loss.
Copper loss equals core loss
x²·3600 = 900 → x = √(900/3600) = 0.5
Load at maximum efficiency
Sη,max = x·S = 0.5·150 = 75 kVA
Answer
Sη,max = 75 kVA
21.Op-amp circuits
Answer: Vout = −3 V
Ideal op-amp rules: with negative feedback, the op-amp drives its output so that its two inputs sit at the same voltage (V₋ = V₊), and no current flows into either input. Writing KCL at the inverting input with these two facts gives the output.
Inverting input follows the input
V₋ = V₊ = −1.5 V
I = V₋/R1 = −1.5/2 = −0.75 mA
Output voltage
The current through R₁ also flows through Rf.
Vout = V₋ + I·Rf = −1.5 + (−0.75)·2 = −3 V
Answer
Vout = −3 V
22.Op-amp circuits
Answer: If = −0.4095 mA
Ideal op-amp rules: with negative feedback, the op-amp drives its output so that its two inputs sit at the same voltage (V₋ = V₊), and no current flows into either input. Writing KCL at the inverting input with these two facts gives the output.
Input currents
V₋ = 0, so each input resistor has its full input voltage across it.
I1 = V1/R1 = −2/4.7 = −0.4255 mA
I2 = V2/R2 = 1.6/100 = 0.016 mA
If = I1 + I2 = −0.4095 mA
Answer
If = −0.4095 mA
23.Diodes & transistors
Answer: VCE = 17.55 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.
Thévenin equivalent of the divider
VTH = 20·6.8/(82 + 6.8) = 1.532 V
RTH = 82·6.8/(82 + 6.8) = 6.279 kΩ
Base current
KVL around the base loop; the emitter current is (β + 1)·IB.
IB = (1.532 − 0.7)/(6.279 + 81·1) = 9.527 µA
Collector current
IC = 80·9.527 µA = 0.7622 mA
IE = 81·9.527 µA = 0.7717 mA
Collector–emitter voltage
VCE = 20 − 0.7622·2.2 − 0.7717·1 = 17.55 V
Answer
VCE = 17.55 V
24.Diodes & transistors
Answer: RB = 1.027 kΩ
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.
Collector current in saturation
IC(sat) = (24 − 0.2)/470 = 50.64 mA
Minimum base current
IB(min) = IC(sat)/β = 50.64/100 = 506.4 µA
Design base current
IB = 5·506.4 µA = 2532 µA
Base resistor
RB = (3.3 − 0.7)/IB = 2.6 V/2.532 mA = 1.027 kΩ
Answer
RB = 1.027 kΩ
25.Number systems
Answer: N = 60
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.
32 + 16 + 8 + 4 = 60
Answer
N = 60
26.Number systems
Answer: R = 191
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.
Bit by bit
XOR gives 1 where the two bits differ.
0101 0100
XOR 1110 1011
= 1011 1111
Value of the result
1011 1111₂ = 191
Answer
R = 191
27.Digital logic: gates, K-maps & flip-flops
Answer: L = 11
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.
Group the 1s
Every group is a rectangle of 2ᵏ cells; edge cells are neighbours of the cells on the opposite edge.
BC′D′
A′CD
AB
A′B′D′
Minimal SOP form
F = BC′D′ + A′CD + AB + A′B′D′
L = 11
Answer
L = 11
Another grouping of the same size exists; it has the same number of terms and literals.
28.Digital logic: gates, K-maps & flip-flops
Answer: N = 2
Karnaugh maps: the cells are ordered in Gray code (00, 01, 11, 10), so neighbouring cells, including the ones across the edges, differ in exactly one variable. Group the 1s in rectangles of 1, 2, 4, 8 or 16 cells, as large as possible and as few as possible, until every 1 is covered. Each group is one product term: the variables that stay constant inside it. A group of 2ᵏ cells loses k variables. Don't-cares (X) may be used to make groups bigger but never have to be covered. Grouping the 0s instead gives the minimal POS form.
Prime implicants
The largest groups that can be formed from 1s and Xs.
B′D, BCD′, A′CD, A′BC
Essential prime implicants
B′D, BCD′
N = 2
Answer
N = 2
29.Laplace transforms
Answer: A = −10
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 + 15s + 56 = (s + 7)(s + 8)
F(s) = A/(s + 7) + B/(s + 8)
Cover-up rule
Multiply by (s + 7) and set s = −7: the B-term vanishes.
A = (6s + 32)/(s + 8) |s = −7 = −10/1 = −10
Answer
A = −10
(B = 16, so f(t) = −10·e−7t + 16·e−8t)
30.Laplace transforms
Answer: y(0.3) = 1.948
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 − 4s − (−10) + 6(sY − 4) + 8Y = 0
Y(s) = (4s + 14)/((s + 2)(s + 4))
Partial fractions
A = 6/2 = 3
B = −2/(−2) = 1
Result
y(t) = 3·e−2t + e−4t
y(0.3) = 1.948
Answer
y(0.3) = 1.948
Check: y(0) = A + B = 4.
31.Block diagrams
Answer: ess = 2.778
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).
Position error constant
Kₚ = G(0) = 2·2/(1·5) = 0.8
Steady-state error
ess = A/(1 + Kₚ) = 5/(1 + 0.8) = 2.778
Answer
ess = 2.778
32.Block diagrams
Answer: ω = 6.633 rad/s
Block-diagram algebra: blocks in series multiply (G₁·G₂), blocks in parallel add (G₁ + G₂), and a loop with forward path G and feedback path H reduces to T = G/(1 + G·H) for negative feedback and G/(1 − G·H) for positive feedback. Reduce inner loops first, then work outwards. The closed-loop poles are the roots of the characteristic equation 1 + G(s)H(s) = 0. For a stable loop, a step input of size A gives the steady-state output A·T(0); with unity feedback the steady-state error to a step is A/(1 + Kp) with Kp = G(0).
Characteristic equation
s³ + 12s² + 44s + 48 + K = 0
Routh array
s³ | 1 44
s² | 12 48 + K
s¹ | (12·44 − 48 − K)/12
s⁰ | 48 + K
Stability limit
All entries of the first column must be positive.
Kmax = 12·44 − 48 = 480
Frequency of oscillation
12·(jω)² + 48 + 480 = 0 → ω² = 528/12 = 44
ω = 6.633 rad/s
Answer
ω = 6.633 rad/s
33.Step response
Answer: ζ = 0.2357
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 = 72 → ωₙ = 8.485 rad/s
2ζωₙ = 4 → ζ = 4/(2·8.485) = 0.2357
Result
ζ = 0.2357
Answer
ζ = 0.2357
34.Step response
Answer: K = 48.8
Step response: a first-order system G(s) = K/(τs + 1) answers a step of size U with y(t) = K·U·(1 − e−t/τ): it reaches 63.2 % of the final value K·U after one time constant τ and 98 % after 4τ. A second-order system G(s) = K·ωₙ²/(s² + 2ζωₙs + ωₙ²) has the poles s = −ζωₙ ± jωd with ωd = ωₙ√(1 − ζ²). For 0 < ζ < 1 the step response overshoots: percent overshoot %OS = 100·e−ζπ/√(1−ζ²), peak time tp = π/ωd, and the 2 % settling time ts ≈ 4/(ζωₙ). Compare the denominator with s² + 2ζωₙs + ωₙ² to read off ωₙ and ζ. For a mass–spring–damper ωₙ = √(k/m) and ζ = c/(2√(km)); for a series RLC circuit ωₙ = 1/√(LC) and ζ = (R/2)·√(C/L).
Closed-loop transfer function
T(s) = K/(s² + 5s + K)
Damping ratio from the overshoot
ζ = −ln(0.3)/√(π² + ln²(0.3)) = 0.3579
Gain
ωₙ = 5/(2ζ) = 6.986 rad/s
K = ωₙ² = 48.8
Answer
K = 48.8
35.Bode plots & margins
Answer: |G(jω)| = 15.02 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.
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 + 400ω² − 129600 = 0
ω² = (−400 + √(160000 + 4·129600))/2 = 211.8
ωc = 14.55 rad/s
Phase margin
∠L(jωc) = −90° − atan(14.55/20) = −126°
PM = 180° + ∠L = 53.96°
Answer
PM = 53.96°
37.Stability: Routh–Hurwitz & root locus
Answer: N = 1
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 + 48s − 50 = 0
Routh array
s³: 1, 48
s²: 14, −50
s¹: 51.57
s⁰: −50
Sign changes in the first column
1 → 14 → 51.57 → −50
N = 1
Answer
N = 1
Positive feedback makes the constant coefficient negative: one real pole always moves into the right half-plane.
38.Stability: Routh–Hurwitz & root locus
Answer: θd = 45 °
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.
Pole locations
s² + 6s + 10 = 0 → s = −3 ± j1
s = −4
Angles from the other poles
∠(−3 + j1 + 4) = atan2(1, 1) = 45°
∠(−3 + j1 − (−3 − j1)) = ∠(j2) = 90°
Angle of departure
θd = 180° − 45° − 90° = 45°
Answer
θd = 45°
39.Steady-state error & PID control
Answer: ess = 0.25
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 = 10·4/5 = 8
Parabola error
ess = 2/8 = 0.25
Answer
ess = 0.25
40.Steady-state error & PID control
Answer: K = 156.2
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 + 10) + 1K = s² + 10s + 1K
Natural frequency
2·0.4·ωₙ = 10 → ωₙ = 12.5 rad/s
Gain
1K = ωₙ² = 156.2 → K = 156.2
Answer
K = 156.2
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