Mechatronic Systems: cram pack

Formula sheets, the key method steps for every topic and 12 practice problems, with full solutions at the back.

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1Formulas and methods

DC motors

Armature circuit
V = E + IaRa
Back-EMF and torque
E = k·ω, T = k·Ia
Speed
ω = 2π·n/60, ω = (V − IaRa)/k
No-load speed and stall torque
ω0 = V/k, Tstall = k·V/Ra
Powers
Pin = V·Ia, Pdev = E·Ia = T·ω, Pout = Pdev − Prot
Starting
Istart = V/(Ra + Rst)
Speed regulation
SR = (n0 − nFL)/nFL
Maximum developed power
Pmax = V²/(4Ra)
Chopper drive
Va = D·Vdc

Method

  1. Draw the armature circuit: supply V, resistance Ra and the back-EMF E in series.
  2. Use V = E + Ia·Ra to link voltage, current and back-EMF.
  3. Use E = k·ω for speed and T = k·Ia for torque, with ω = 2π·n/60.
  4. For power and efficiency, start from V·Ia, subtract the copper loss Ia²·Ra and then the rotational losses.

Gears & gear trains

Meshing gears
n1·N1 = n2·N2
Torque
T2 = T1·(N2/N1)·η
Power
P = T·ω, ω = 2π·n/60
Compound train
total ratio = product of the stage ratios

Data acquisition & sampling

Nyquist criterion
fs > 2·fmax, fN = fs/2
Alias frequency
fa = |f − k·fs|, k = round(f/fs)
Step size
1 LSB = VFSR/2ᴺ
Quantisation error (rounding)
±½ LSB
Truncating ADC code
D = ⌊Vin/LSB⌋
Bits for a resolution r
2ᴺ ≥ span/r
Ideal SQNR, full-scale sine
SQNR = 6.02·N + 1.76 dB
Data rate
channels × fs × N bit/s
Multiplexed ADC
fs = 1/(n·(tc + tset))
UART
Tb = 1/baud; 8N1 = 10 bits per byte; bytes/s = baud/bits per frame
Baud rate divider
baud = fclk/(16·D)

Method

  1. Write down what is given: sampling rate, signal frequencies, number of bits, input range, baud rate.
  2. For sampling questions, compare each frequency with fs/2; a higher frequency appears at fa = |f − k·fs| with the nearest multiple of fs.
  3. For resolution questions, find 1 LSB = VFSR/2ᴺ, or the smallest N with 2ᴺ ≥ span/resolution.
  4. For data rates and UART links, count everything that is sent: channels, samples per second, bits or whole bytes per sample, and the start, parity and stop bits of every frame.

Wheatstone bridge & strain gauges

Divider voltages
Va = VsR2/(R1 + R2), Vb = VsR4/(R3 + R4)
Output
Vab = Va − Vb
Balance
R1/R2 = R3/R4
Slide-wire bridge
R/Rx = l/(100 − l)
Thévenin resistance
Rth = R1∥R2 + R3∥R4
Gauge factor
ΔR/R = GF·ε
Bridge output
quarter Vs·GF·ε/4, half Vs·GF·ε/2, full Vs·GF·ε
Small change, one arm
Vab ≈ Vs·ΔR/(4R)
Stress
σ = E·ε

Method

  1. Treat the bridge as two voltage dividers across the same supply.
  2. For balance, set R₁/R₂ = R₃/R₄ and solve for the unknown resistor.
  3. For an unbalanced bridge, find Va and Vb from the dividers and subtract; use the Thévenin equivalent when a meter loads the output.
  4. For strain gauges, convert strain to ΔR/R = GF·ε and use Vs·GF·ε/4, /2 or ×1 for a quarter, half or full bridge.

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.DC motorsMedium
T (N·m)n (rpm)3 N·mn0​n = ?

A DC motor (k = 0.3 N·m/A, Ra = 1.2 Ω) runs from 120 V and drives a load torque of 3 N·m. Find its speed n in rpm.

V = 120 Vk = 0.3 N·m/ARa = 1.2 ΩT = 3 N·m
n = rpm
2.DC motorsHard
+−48 VRs​ = ?Ra​ = 0.5 ΩM+−En = 400 rpmT = 3.2 N·m

A DC motor (k = 0.4 V·s/rad, Ra = 0.5 Ω) on a fixed 48 V supply drives a load of 3.2 N·m. Find the series resistance Rs that slows it down to 400 rpm.

V = 48 Vk = 0.4 V·s/radRa = 0.5 ΩT = 3.2 N·mn = 400 rpm
Rs = Ω
3.Gears & gear trainsMedium
Nw​ = 36z = 3, 1440 rpm

A worm with 3 start(s) turns at 1440 rpm and drives a worm wheel with 36 teeth. Find the speed nw of the wheel.

z = 3Nw = 36n = 1440 rpm
nw = rpm
4.Gears & gear trainsHard
A = 12B = 48C = 15D = 32

In a compound gear train, gear A (12 teeth) on the input shaft turning at 1450 rpm drives gear B (48 teeth). Gear C (15 teeth) is fixed to the same shaft as B and drives gear D (32 teeth) on the output shaft. Find the output speed nout.

nin = 1450 rpmA = 12B = 48C = 15D = 32
nout = rpm
5.Data acquisition & samplingMedium
SD0​D1​D2​D3​D4​D5​D6​D7​Tb​10·Tb​115200 Bd, 8N1

A UART sends bytes at 115200 baud in the format 8N1: 8 data bits, no parity and 1 stop bit(s), plus the start bit. Find the largest number of data bytes per second it can transfer.

baud = 115200 Bd8N1
RB = B/s
6.Data acquisition & samplingHard
f0fs​/2fs​2fs​3fs​3.2 kHz7f₁?

A 3.2 kHz square wave is sampled at 8 kHz with no anti-aliasing filter. A square wave contains the odd harmonics 3f₁, 5f₁, 7f₁, … At which frequency fa does its harmonic 7f₁ appear in the sampled data? Give it in Hz.

f₁ = 3.2 kHzfs = 8 kHzharmonic: 7f₁
fa = Hz
7.Wheatstone bridge & strain gaugesMedium
+−15 VR1​ = 800 ΩR2​ = 40 ΩR3​ = 250 ΩR4​ = 20 ΩabGRg​ = 20 Ω

A galvanometer with a resistance of 20 Ω is connected between a and b of the bridge shown (Vs = 15 V). Find the galvanometer current Ig from a to b, in µA.

Vs = 15 VR1 = 800 ΩR2 = 40 ΩR3 = 250 ΩR4 = 20 ΩRg = 20 Ω
Ig = µA
8.Wheatstone bridge & strain gaugesHard
+−10 V120 Ω − ΔR120 Ω + ΔR120 Ω120 Ωab+−Vo​ = ?

A bridge with 120 Ω arms is excited with 10 V and has two active gauges in adjacent arms, one in tension and one in compression (half bridge). The gauge factor is 2.1 and the strain is 1200 µε. Find the bridge output Vo in mV.

Vs = 10 VGF = 2.1ε = 1200 µε
Vo = mV
9.Steady-state error & PID controlMedium
R(s)+K(s + 1)(s + 2)C(s)−

A unity-feedback loop has G(s) = K/((s + 1)(s + 2)). Find the gain K that gives a steady-state error of 25 % for a step input.

G(s) = K/((s + 1)(s + 2))ess = 25 %
K =
10.Steady-state error & PID controlHard
R(s)+K = 15s(s + 2)C(s)−

A proportional controller K = 1 drives the plant G(s) = 5/(s(s + 2)) in a unity-feedback loop. Find the 2 % settling time ts of the step response, using ts ≈ 4/(ζωₙ).

G(s) = 5/(s(s + 2))K = 1
ts = s
11.Step responseMedium
t (s)y(t)1?

A system has the transfer function G(s) = 49/(s² + 2s + 49) and receives a unit step input. Find the percent overshoot %OS of the step response.

G(s) = 49/(s² + 2s + 49)
%OS = %
12.Step responseHard
R(s)+245s(s + 5)G(s)C(s)−

A unity negative feedback loop has G(s) = 245/(s(s + 5)). Find the 2 % settling time ts of the closed-loop step response, using ts ≈ 4/(ζωₙ).

G(s) = 245/(s(s + 5))
ts = s

3Solutions

1.DC motors

Answer: n = 3438 rpm

DC motor: the armature is a resistance Ra in series with the back-EMF E, so V = E + Ia·Ra. The back-EMF grows with speed, E = k·ω, and the torque with current, T = k·Ia, with the same motor constant k (V·s/rad = N·m/A) in SI units. Convert speeds with ω = 2π·n/60. The developed power is E·Ia = T·ω; the input power is V·Ia, and the copper loss Ia²Ra and the rotational loss make the difference. The speed falls in a straight line with torque, ω = V/k − Ra·T/k², from the no-load speed V/k to zero at the stall torque k·V/Ra. At standstill E = 0, so the starting current V/Ra is large unless a resistor limits it.

Armature current

Ia = T/k = 3/0.3 = 10 A

Back-EMF and speed

E = 120 − 10·1.2 = 108 V
ω = E/k = 360 rad/s → n = 3438 rpm

Answer

n = 3438 rpm
2.DC motors

Answer: Rs = 3.406 Ω

DC motor: the armature is a resistance Ra in series with the back-EMF E, so V = E + Ia·Ra. The back-EMF grows with speed, E = k·ω, and the torque with current, T = k·Ia, with the same motor constant k (V·s/rad = N·m/A) in SI units. Convert speeds with ω = 2π·n/60. The developed power is E·Ia = T·ω; the input power is V·Ia, and the copper loss Ia²Ra and the rotational loss make the difference. The speed falls in a straight line with torque, ω = V/k − Ra·T/k², from the no-load speed V/k to zero at the stall torque k·V/Ra. At standstill E = 0, so the starting current V/Ra is large unless a resistor limits it.

Current and back-EMF

Ia = 3.2/0.4 = 8 A
E = 0.4·41.89 = 16.76 V

Series resistance

Ra + Rs = (48 − 16.76)/8 = 3.906 Ω
Rs = 3.406 Ω

Answer

Rs = 3.406 Ω

The resistor wastes 218 W; a chopper controls the speed with far less loss.

3.Gears & gear trains

Answer: nw = 120 rpm

Gear trains: meshing gears have the same speed at the teeth, so n₁·N₁ = n₂·N₂: the gear with fewer teeth turns faster. Gears on one shaft turn at the same speed. Power is passed on (minus losses), so torque goes up when speed goes down: T₂ = T₁·(N₂/N₁)·η, and P = T·ω with ω = 2π·n/60.

Wheel speed

nw = n·z/Nw = 1440·3/36 = 120 rpm

Answer

nw = 120 rpm
4.Gears & gear trains

Answer: nout = 169.9 rpm

Gear trains: meshing gears have the same speed at the teeth, so n₁·N₁ = n₂·N₂: the gear with fewer teeth turns faster. Gears on one shaft turn at the same speed. Power is passed on (minus losses), so torque goes up when speed goes down: T₂ = T₁·(N₂/N₁)·η, and P = T·ω with ω = 2π·n/60.

First stage

nB = 1450·12/48 = 362.5 rpm = nC

Second stage

nout = 362.5·15/32 = 169.9 rpm

Answer

nout = 169.9 rpm

total ratio = 8.533 : 1

5.Data acquisition & sampling

Answer: RB = 11520 B/s

UART: an asynchronous serial link sends each byte as a frame: one start bit (low), the data bits, an optional parity bit and one or two stop bits (high). The baud rate is the number of bits per second, so one bit lasts Tb = 1/baud and a frame of n bits lasts n/baud. The common 8N1 format has 10 bits per byte. The baud generator divides the clock: baud = fclk/(16·D) with a whole number D, so the real baud rate differs slightly from the target; an error below about 2 % is usually acceptable.

Bits per frame

1 + 8 + 0 + 1 = 10

Byte rate

115200/10 = 11520 B/s

Answer

RB = 11520 B/s
6.Data acquisition & sampling

Answer: fa = 1600 Hz

Sampling: an ADC measures the signal fs times per second. By the Nyquist–Shannon theorem a frequency f is captured correctly only while f < fs/2, the Nyquist (folding) frequency, so the sampling rate must exceed twice the highest signal frequency. A higher frequency is not lost: it shows up as an alias at fa = |f − k·fs|, with the whole number k that brings the result between 0 and fs/2. The samples cannot tell the two apart, so an analogue anti-aliasing filter must remove everything above fs/2 before the ADC.

Harmonic frequency

7f₁ = 7·3.2 kHz = 22.4 kHz

Nearest multiple of the sampling rate

m = round(2.8) = 3

Alias frequency

fa = |22400 − 3·8000| = 1600 Hz

Answer

fa = 1600 Hz

The alias lands inside the signal band, where no digital filter can remove it. Only an analogue filter before the ADC helps.

7.Wheatstone bridge & strain gauges

Answer: Ig = −5180 µA

Wheatstone bridge: two voltage dividers share one supply Vs. The left divider R1–R2 gives Va = Vs·R2/(R1 + R2) and the right divider R3–R4 gives Vb = Vs·R4/(R3 + R4); the output is Vab = Va − Vb. The bridge is balanced (Vab = 0, no current in the meter) when R1/R2 = R3/R4, that is R1·R4 = R2·R3. Seen from the output, the bridge is a Thévenin source with Rth = R1∥R2 + R3∥R4.

Thévenin voltage

Vth = 15·(40/840 − 20/270) = −0.3968 V

Thévenin resistance

Rth = R₁∥R₂ + R₃∥R₄ = 56.61 Ω

Galvanometer current

Ig = −0.3968/(56.61 + 20) = −5180 µA

Answer

Ig = −5180 µA
8.Wheatstone bridge & strain gauges

Answer: Vo = 12.6 mV

Strain gauges: a gauge changes its resistance with strain: ΔR/R = GF·ε, where the gauge factor GF is about 2 for metal foil. In a bridge with all arms equal to R, one active gauge (quarter bridge) gives Vo ≈ Vs·GF·ε/4. Two active gauges with opposite strains in adjacent arms (half bridge) give Vs·GF·ε/2, and four (full bridge) give Vs·GF·ε. Stress follows from Hooke’s law, σ = E·ε. Load cells state their sensitivity in mV/V: the output at full load per volt of excitation.

Relative resistance change

ΔR/R = 2.1·1200·10⁻⁶ = 0.00252

Bridge output

Vo = Vs·GF·ε/2 = 10·0.00252/2 = 12.6 mV

Answer

Vo = 12.6 mV
9.Steady-state error & PID control

Answer: K = 6

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.

Required error constant

1/(1 + Kp) = 0.25 → Kp = 3

Gain

K/2 = 3 → K = 6

Answer

K = 6

Check the closed-loop stability as well: for this second-order loop any K > 0 is stable.

10.Steady-state error & PID control

Answer: ts = 4 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 + 2) + 1·5 = s² + 2s + 5

ωₙ and ζ

ωₙ = √5 = 2.236 rad/s
ζ = 2/(2·2.236) = 0.4472

Settling time

ζωₙ = 2/2 = 1
ts ≈ 4/1 = 4 s

Answer

ts = 4 s

The settling time does not depend on K here: raising K only makes the response oscillate faster.

11.Step response

Answer: %OS = 63.54 %

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 = 49 → ωₙ = 7 rad/s
2ζωₙ = 2 → ζ = 2/(2·7) = 0.1429

Result

%OS = 100·e−ζπ/√(1−ζ²) = 100·e−0.4534 = 63.54 %

Answer

%OS = 63.54 %
12.Step response

Answer: ts = 1.6 s

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

Closed-loop transfer function

T(s) = 245/(s² + 5s + 245): ωₙ = 15.65 rad/s, ζ = 0.1597

Settling time

ζωₙ = 5/2 = 2.5
ts ≈ 4/(ζωₙ) = 1.6 s

Answer

ts = 1.6 s

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

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