UNIT 1: FUNDAMENTALS OF MEASUREMENT, INSTRUMENTATION & CONTROL SYSTEMS
1.0 MEASUREMENT SYSTEM FUNDAMENTALS
1.1 Elements of a Generalized Measurement System
A measurement system typically consists of four functional stages:
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Primary Sensing Element / Sensor: Directly interacts with the measured variable (e.g., Bourdon tube for pressure, thermocouple for temperature) and produces a primary effect (mechanical displacement, thermal EMF).
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Signal Conditioning Element: Converts the primary signal into a more suitable form (e.g., amplification, filtering, linearization). Often includes a transducer (converts one energy form to another, like strain gauge converting strain to resistance change).
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Signal Processing / Data Acquisition Element: Further processes the conditioned signal (e.g., analog-to-digital conversion, computation, multiplexing) for analysis or control.
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Display / Recording Element: Presents the measurement result to the user (e.g., analog pointer, digital readout, chart recorder, computer screen).
[!TIP] Exam Focus: Questions often ask to "explain elements" or "draw a block diagram." Remember the sequence: Variable → Sensor → Conditioning → Processing → Output.
1.2 Standards and Calibration
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Need for Calibration: To establish the relationship between the instrument's output and the known true value of the input. Ensures accuracy, traceability, and reliability of measurements. Compensates for drift, wear, and manufacturing tolerances.
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Standards:
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Primary Standard: Highest accuracy, defines the unit (e.g., NIST, BIPM). Rarely used directly.
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Secondary Standard: Calibrated against a primary standard. Used in national/regional labs.
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Working Standard: Used routinely in laboratories/industry to calibrate instruments. Calibrated against secondary standards.
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Calibration Procedure: Involves applying known inputs (from a standard) across the instrument's range and recording the output. A calibration curve (plot of true value vs. instrument output) is generated. The instrument's deviation from this curve defines its error.
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Traceability: The documented unbroken chain of comparisons (calibrations) linking a measurement result to a primary standard, with stated uncertainties at each step.
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Example - Dead Weight Tester (Pressure Calibration):
DiagramCANVAS: A piston-cylinder assembly with weights stacked on a platform. The piston area is precisely known. Pressure P = (Total Weight) / (Piston Area). This provides a known, highly accurate pressure source to compare against the gauge under test.
[!TIP] Common Pitfall: Confusing accuracy (closeness to true value) with precision (repeatability). Calibration improves accuracy.
1.3 Classification of Instruments
| Basis | Types | Examples |
|---|---|---|
| Function | Indicating (e.g., analog gauge) | Recording (e.g., chart recorder) |
| Integrating (e.g., energy meter) | ||
| Application | Industrial (robust) | Laboratory (high precision) |
| Biomedical (specialized) | ||
| Signal Type | Analogue (continuous output, e.g., 0-10V, 4-20mA) | Digital (discrete numeric output, e.g., RS-232) |
2.0 ERRORS, UNCERTAINTIES & STATIC PERFORMANCE CHARACTERISTICS
2.1 Measurement Errors
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Definition: The difference between the measured value and the true value.
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Sources: Imperfections in instruments, environmental changes (temp, humidity), observer bias, method limitations.
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Types:
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Systematic Errors: Consistent, predictable, repeatable. Can be corrected.
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Calibration Error: Instrument not correctly calibrated.
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Environmental Error: Changes in ambient conditions (e.g., thermal expansion).
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Observational Error: Parallax, zero error.
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Random Errors: Unpredictable, caused by noise, small fluctuations. Characterized by precision. Reduced by averaging.
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Gross Errors / Mistakes: Human errors (reading wrong, recording error). Should be eliminated by careful procedure.
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2.2 Uncertainty Analysis
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Definition: A parameter, associated with the result of a measurement, that characterizes the dispersion of the values that could reasonably be attributed to the measurand. It quantifies our lack of complete knowledge.
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Types:
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Absolute Uncertainty ($\Delta x$): ± value with same unit as measurement (e.g., $25.46 \pm 0.02$ g).
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Relative/Percentage Uncertainty ($\delta$): $$\displaystyle \delta = \frac{\Delta x}{x} \times 100\% $$.
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Estimation from Specifications:
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% of Full Scale Deflection (FSD): $$\displaystyle \Delta x = \pm \left( \frac{\%}{100} \times \text{Full Scale Value} \right) $$. Worse at low readings.
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% of Reading (True Value): $$\displaystyle \Delta x = \pm \left( \frac{\%}{100} \times \text{Measured Value} \right) $$. Constant relative error.
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Propagation of Uncertainties (for function $$\displaystyle z = f(x, y) $$):
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For sum/difference: $$\displaystyle z = x + y \Rightarrow \Delta z = \sqrt{(\Delta x)^2 + (\Delta y)^2} $$
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For product/quotient: $$\displaystyle z = x \cdot y \Rightarrow \frac{\Delta z}{z} = \sqrt{\left(\frac{\Delta x}{x}\right)^2 + \left(\frac{\Delta y}{y}\right)^2} $$
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For constant multiplier: $$\displaystyle z = kx \Rightarrow \Delta z = |k| \Delta x $$
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Mitigation: Use higher-grade instruments, calibrate, control environment, take multiple readings, use appropriate measurement technique.
[!EXAMPLE] From Past Paper (JUN 2025):
Scale accuracy = ±0.02 g.
Reading = 25.46 g.
Absolute Uncertainty = $\boxed{\pm 0.02 \text{ g}}$.
% Uncertainty = $$\displaystyle \frac{0.02}{25.46} \times 100\% \approx 0.078\% $$.
Mitigation: Weigh multiple samples and average; use a scale with higher resolution/accuracy; ensure stable, vibration-free environment; tare the container properly.
2.3 Static Performance Characteristics
Characteristics assessed with steady (constant) inputs.
| Characteristic | Definition | Significance |
|---|---|---|
| Accuracy | Closeness of agreement between measured value & true value. | Overall quality of measurement. Often expressed as % of reading or FSD. |
| Precision | Closeness of agreement between independent measurements (repeatability). | Indicates random error. High precision ≠ high accuracy. |
| Repeatability | Precision under same conditions (same operator, instrument, short time). | Part of precision. |
| Reproducibility | Precision under changed conditions (different operator, time, lab). | Measures robustness. |
| Sensitivity | Ratio of change in output to change in input ($$\displaystyle S = \frac{\Delta \text{out}}{\Delta \text{in}} $$). | "Gain" of the system. Slope of calibration curve. |
| Resolution | Smallest detectable change in input. | Limited by display/readout (e.g., 0.1 mm on a ruler). |
| Threshold | Minimum input that produces a detectable output change. | Related to resolution & noise floor. |
| Drift | Gradual change in output over time for a constant input. | Caused by component aging, temperature. |
| Hysteresis | Difference in output for same input depending on direction (up/down sweep). | Caused by friction, magnetic effects. Plotted as a hysteresis loop. |
| Linearity | Deviation of actual calibration curve from a straight line. | Often expressed as % of FSD. Ideal for simple scaling. |
| Span / Range | Difference between upper & lower limits of measurable input. | Instrument's operating window. |
| Deadband | Range of input values for which there is no change in output. | Similar to threshold/hysteresis. Instrument is "insensitive" in this region. |
Representation: All are derived from the calibration curve (input vs. output). Hysteresis is shown by two curves (increasing/decreasing input).
[!TIP] Exam Key: Be able to define each term and explain its impact (e.g., "High hysteresis reduces accuracy for cyclic measurements"). Know how to read specifications from a datasheet (e.g., "Accuracy: ±0.5% of FSD, Linearity: ±0.2%").
3.0 DYNAMIC PERFORMANCE CHARACTERISTICS & SIGNAL ANALYSIS
3.1 Dynamic Response Fundamentals
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Static vs. Dynamic: Static characteristics assume steady-state conditions. Dynamic characteristics describe how the system responds to time-varying inputs. Crucial for measuring fast-changing processes (vibration, pressure spikes).
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Need: A system with good static specs may distort or lag behind a fast-changing input, leading to erroneous readings.
3.2 Dynamic Response Parameters
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Time Delay / Dead Time ($\theta$): Time lag between application of input and start of output response.
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Speed of Response:
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Time Constant ($\tau$): For a 1st order system, time to reach ~63.2% of final value after a step input. $$\displaystyle \tau = \frac{1}{a} $$ in $$\displaystyle y(t) = K(1 - e^{-at}) $$.
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Natural Frequency ($$\displaystyle \omega_n $$) & Damping Ratio ($\zeta$): For a 2nd order system. $$\displaystyle \omega_n $$ = undamped oscillation frequency. $\zeta$ = ratio of actual damping to critical damping.
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Fidelity: Faithfulness of output waveform to input waveform, especially for periodic inputs. High fidelity means minimal amplitude/phase distortion.
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Settling Time ($$\displaystyle t_s $$): Time for output to stay within a certain band (e.g., ±2%) of final value after a step.
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Rise Time ($$\displaystyle t_r $$): Time for output to go from 10% to 90% (or 0% to 100%) of final value.
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Overshoot ($$\displaystyle M_p $$): Maximum peak value above the final steady-state value, expressed as a percentage. Occurs in underdamped 2nd order systems.
3.3 System Order and Response
System Order: Highest power of 's' in the denominator of the transfer function.
- First-Order System (e.g., thermometer, RC circuit):
$$G(s) = \frac{K}{\tau s + 1}$$
* **Step Response:** $$\displaystyle y(t) = K(1 - e^{-t/\tau}) $$. No overshoot.
* **Ramp Response:** Output lags input by $\tau$. **Tracking error** = $\tau \cdot \text{slope}$.
* **Harmonic Response:** Magnitude decreases, phase lags as frequency increases.
- Second-Order System (e.g., seismometer, RLC circuit):
$$G(s) = \frac{K \omega_n^2}{s^2 + 2\zeta\omega_n s + \omega_n^2}$$
* **Response Types:**
* **Underdamped ($$\displaystyle \zeta < 1 $$):** Oscillatory, overshoot.
* **Critically Damped ($$\displaystyle \zeta = 1 $$):** Fastest response without overshoot.
* **Overdamped ($$\displaystyle \zeta > 1 $$):** Slower, no overshoot.
* **Step Response:** Shape depends critically on $\zeta$.
3.4 Input Signal Types
| Signal Type | Examples | Characteristics & Effect on Response |
|---|---|---|
| Periodic | Harmonic (Sine) | Used for frequency response (Bode plots). Tests fidelity & phase. |
| Non-Harmonic (Square, Triangle) | Contains harmonics. Tests system's ability to handle multiple freq. | |
| Aperiodic | Transient: Step, Ramp, Impulse | Tests speed, overshoot, settling time. Step is most common. |
| Random (Noise, speech) | Characterized statistically (PSD). Tests noise rejection & averaging. |
[!TIP] Exam Trap: "Harmonic" is a subset of "periodic." All harmonics are periodic, but not all periodic signals are harmonic (e.g., square wave).
4.0 MATHEMATICAL TOOLS FOR SIGNAL & SYSTEM ANALYSIS
4.1 Fourier Transform (FT)
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Significance: Converts a time-domain signal $x(t)$ into its frequency-domain representation $X(f)$. Reveals constituent frequencies and their amplitudes/phases.
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Definition:
$$X(f) = \int_{-\infty}^{\infty} x(t) e^{-j2\pi ft} dt$$
Inverse FT: $$\displaystyle x(t) = \int_{-\infty}^{\infty} X(f) e^{j2\pi ft} df $$
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Key Properties:
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Linearity: $$\displaystyle \mathcal{F}\{a x_1(t) + b x_2(t)\} = a X_1(f) + b X_2(f) $$
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Time-Shift: $$\displaystyle \mathcal{F}\{x(t - t_0)\} = X(f) e^{-j2\pi f t_0} $$ (introduces phase shift)
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Frequency-Shift: $$\displaystyle \mathcal{F}\{x(t) e^{j2\pi f_0 t}\} = X(f - f_0) $$
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Application: Analyzing system frequency response, filtering, signal spectrum analysis.
4.2 Mathematical Modelling of Systems
Goal: Derive differential equations from physical laws, then obtain Transfer Function $$\displaystyle G(s) = \frac{Y(s)}{X(s)} $$ (Laplace transform of impulse response, assuming zero initial conditions).
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Electrical Systems (LRC Circuits):
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Resistor: $$\displaystyle v_R = iR $$
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Capacitor: $$\displaystyle i_C = C \frac{dv_C}{dt} $$ or $$\displaystyle v_C = \frac{1}{C} \int i dt $$
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Inductor: $$\displaystyle v_L = L \frac{di_L}{dt} $$
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Example (Series RLC): $$\displaystyle L\frac{di}{dt} + Ri + \frac{1}{C}\int i dt = v_{in}(t) $$. Laplace: $$\displaystyle L s I(s) + R I(s) + \frac{1}{Cs} I(s) = V_{in}(s) $$.
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$$G(s) = \frac{I(s)}{V_{in}(s)} = \frac{1}{Ls^2 + Rs + 1/C}$$
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Mechanical Systems (Translational):
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Mass ($m$): $$\displaystyle F = m \frac{d^2x}{dt^2} $$ (inertia)
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Damper ($b$): $$\displaystyle F = b \frac{dx}{dt} $$ (viscous friction)
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Spring ($k$): $$\displaystyle F = kx $$ (elasticity)
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Example (Mass-Spring-Damper): $$\displaystyle m\ddot{x} + b\dot{x} + kx = F(t) $$. Laplace:
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$$G(s) = \frac{X(s)}{F(s)} = \frac{1}{ms^2 + bs + k}$$
[!TIP] Analogy: Electrical (L, R, 1/C) ↔ Mechanical (m, b, 1/k). This helps model one system using the other's analogy.
5.0 TRANSDUCERS & SENSORS FOR PHYSICAL QUANTITIES
5.1 Pressure Measurement
5.1.1 Mechanical Gauges
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Bourdon Tube: Curved tube that straightens under pressure. Motion converted to pointer rotation. Robust, no power.
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Bellows / Diaphragm: Flexible elements that expand/contract. Used for low pressure, differential pressure.
5.1.2 Manometers
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U-tube: Simple, balances pressure head: $$\displaystyle P_1 - P_2 = \rho g h $$. Measures differential pressure.
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Inclined Tube: Amplifies deflection ($$\displaystyle h = L \sin\theta $$), increases sensitivity for low pressures.
5.1.3 Pressure Transducers
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Strain Gauge Type: Pressure acts on diaphragm, causing strain. Strain gauges in Wheatstone bridge measure strain → pressure.
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Capacitive Type: Pressure changes diaphragm position → changes capacitance between plates.
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Piezoelectric Type (Quartz, PZT): Dynamic pressure only. Stress generates surface charge: $$\displaystyle Q = d \cdot F $$ (charge sensitivity), $$\displaystyle V = g \cdot \sigma $$ (voltage sensitivity). No DC response.
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Piezoresistive Type: Semiconductor strain gauge. Large gauge factor, sensitive to temperature.
5.1.4 Flow Measurement (Pressure-Based)
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Venturi Meter: Converging-diverging tube. Pressure drop $$\displaystyle \Delta P \propto Q^2 $$. Low permanent pressure loss.
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Orifice Meter: Thin plate with hole. Simple, but high energy loss & upstream disturbance.
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Flow Nozzle: Compromise between venturi and orifice.
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Pitot Tube: Measures flow velocity (stagnation pressure - static pressure $$\displaystyle \propto v^2 $$).
5.2 Temperature Measurement
5.2.1 Contact Sensors
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RTD (Resistance Temperature Detector): $$\displaystyle R_T = R_0 [1 + \alpha T + \beta T^2 + ...] $$. Pt100 ($$\displaystyle R_0=100\Omega $$ at 0°C) is standard. Stable, accurate, linear (approx). 3-wire/4-wire configs for lead compensation.
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Thermistor: Semiconductor, $$\displaystyle R = A e^{B/T} $$ (NTC: resistance ↓ with T). High sensitivity, non-linear, limited range.
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Thermocouple (Seebeck Effect): Two dissimilar metals joined → voltage $$\displaystyle E = f(T_1, T_2) $$. Measures temperature difference. Needs cold junction compensation (reference junction at known T, usually 0°C or electronic compensation).
- Types: J (Fe-CuNi), K (NiCr-NiAl - most common), T (Cu-CuNi), E (NiCr-CuNi), S (PtRh-Pt - high temp).
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Bimetallic Thermometer: Two metals with different $\alpha$ bonded. Bends with T. Mechanical, no power.
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Liquid-in-Glass (Mercury/Alcohol): Thermal expansion of liquid in capillary. Simple, direct reading.
5.2.2 Non-Contact Sensors
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Radiation Pyrometers:
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Optical Pyrometer: Compares brightness of filament with object. Manual/automatic. Measures high T (>700°C).
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Total Radiation Pyrometer: Measures total IR radiation. Output depends on emissivity.
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5.3 Displacement, Position & Angular Measurement
5.3.1 Potentiometric Transducer
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Principle: Wiper slides on resistive element. Displacement → variable resistance/voltage (voltage divider).
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Types: Rotary, Linear.
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Limitations: Loading effect (meter resistance draws current, causes error), wear, limited resolution.
5.3.2 Inductive Transducers
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LVDT (Linear Variable Differential Transformer):
DiagramCANVAS: A cylindrical core (ferromagnetic) moves inside a primary coil (center) and two secondary coils (top/bottom) connected in series opposition. AC excitation on primary. Core position determines voltage induced in secondaries. Output = $$\displaystyle V_{sec1} - V_{sec2} $$. At null position, output = 0. Displacement from null gives phase & amplitude info. Infinite resolution, no electrical contact, robust.- Output: $$\displaystyle V_{out} \propto $$ displacement $x$. Phase indicates direction.
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RVDT (Rotary Variable Differential Transformer): Same principle for angular displacement.
5.4 Strain, Load & Force Measurement
5.4.1 Resistance Strain Gauge
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Principle: Piezoresistive effect. Strain $\epsilon$ changes resistance $\Delta R$.
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Gauge Factor (GF): $$\displaystyle GF = \frac{\Delta R / R}{\epsilon} = 1 + 2\nu + \frac{\Delta \rho / \rho}{\epsilon} $$ (for metals, $\nu$=Poisson's ratio, last term small → GF ≈ 1+2ν ≈ 2).
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Construction: Foil (most common), wire, semiconductor.
5.4.2 Strain Gauge Configurations (Wheatstone Bridge)
$$ \frac{\Delta R}{R} = GF \cdot \epsilon $$
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Quarter Bridge: One active gauge. Output $$\displaystyle V_o \approx \frac{V_{ex}}{4} \cdot GF \cdot \epsilon $$. Temperature sensitive.
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Half Bridge: Two active gauges (e.g., tension/compression). Output doubles, some temp. compensation.
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Full Bridge: Four active gauges. Max output, excellent temp. compensation (adjacent arms opposite strain).
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Signal Conditioning: Bridge excitation (low-noise DC/AC), amplification (instrumentation amp), filtering.
5.4.3 Load Cells
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Principle: Strain gauges bonded to a structural element (load cell) that deforms under load.
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Types: Compression, Tension, Bending beam, Shear beam.
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Output: mV/V (e.g., 2 mV/V at full load with 10V excitation → 20 mV output).
[!EXAMPLE] From Past Paper (JUN 2023, 2022):
Given: $$\displaystyle R=150\Omega $$, $$\displaystyle A=0.5\times10^{-4} m^2 $$, $$\displaystyle E=200 \times 10^9 N/m^2 $$, $$\displaystyle F=60 kN=60,000 N $$, $$\displaystyle \Delta R=1.5\Omega $$.
Stress $$\displaystyle \sigma = F/A = 60,000 / (0.5\times10^{-4}) = 1.2 \times 10^9 N/m^2 $$.
Strain $$\displaystyle \epsilon = \sigma / E = (1.2 \times 10^9) / (200 \times 10^9) = 0.006 $$.
$$\displaystyle GF = \frac{\Delta R / R}{\epsilon} = \frac{1.5 / 150}{0.006} = \frac{0.01}{0.006} \approx \boxed{1.67} $$.
5.5 Velocity & Speed Measurement
5.5.1 Stroboscope
- Principle: Produces high-frequency light flashes. If flash rate $$\displaystyle f_s $$ equals object's rotational speed $$\displaystyle f_o $$, object appears stationary. $$\displaystyle f_o = f_s $$ or $$\displaystyle f_o = f_s / n $$ (n=integer). Used for non-contact speed measurement and vibration analysis.
5.5.2 Electromagnetic Tachometers
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Principle: Relative motion between magnetic field & conductor induces EMF (Faraday's law: $$\displaystyle e = Blv $$ or $$\displaystyle e = k \omega $$).
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DC Tachogenerator: Rotating magnet/armature → AC → commutator → DC voltage $\propto \omega$. Contact type.
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AC (Induction) Tachogenerator: Two-pole rotor with salient teeth, stator with two windings (excitation & output). Output frequency = rotation speed. Non-contact (proximity).
5.5.3 Mechanical Tachometers
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Centrifugal: Weights fly out with speed → pointer deflection. Bulky, inaccurate.
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Vibrating Reed: Reed resonates at its natural frequency when driven by vibrating shaft. Used for frequency monitoring.
5.6 Other Transducers
5.6.1 Piezoelectric Transducers
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Principle (Inverse): Apply stress → strain → electric charge (direct: stress → charge). Materials: Quartz (stable, low sensitivity), PZT (high sensitivity, but temp. sensitive).
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Applications: Dynamic pressure, acceleration (seismic mass on crystal), force, ultrasonic generation/detection.
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Limitation: Cannot measure static quantities (charge leaks away). Needs high-impedance amplifier.
5.6.2 Ionization Transducers
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Principle: Ionizing radiation or gas molecule collisions create ion pairs. Current measured is proportional to pressure (in vacuum) or radiation intensity.
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Ionization Gauge (Vacuum): Current from ionized gas molecules $\propto$ pressure (at very low pressures).
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Geiger-Muller Tube: Radiation detection. Each ionizing event causes large pulse.
5.6.3 Humidity Measurement (Brief)
- Sling Psychrometer: Two thermometers (dry & wet bulb). Whirled to evaporate water from wet bulb. Dry-bulb temp ($$\displaystyle T_d $$) and wet-bulb depression ($$\displaystyle T_d - T_w $$) determine relative humidity from psychrometric charts.
6.0 CONTROL SYSTEMS - FUNDAMENTALS & CLASSIFICATION
6.1 Basic Control System Concepts
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Plant / Process: The physical system to be controlled (e.g., boiler, motor).
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Controlled Variable (CV): The quantity to be maintained/regulated (e.g., temperature, level, speed).
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Manipulated Variable (MV): The input to the plant adjusted by the controller (e.g., fuel valve opening, pump speed).
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Input / Reference ($r(t)$): Desired value (setpoint) of the controlled variable.
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Output ($c(t)$): Actual measured value of the controlled variable.
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Disturbance ($d(t)$): Unwanted input affecting the plant output.
6.2 Open-Loop Control System
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Working: Output has no effect on the control action. Controller acts based only on setpoint and maybe a fixed model.
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Advantages: Simple, stable, easy to construct, no instability issues.
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Limitations: Inaccurate (no correction for disturbances or model errors), no disturbance rejection, performance depends entirely on calibration.
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Examples: Washing machine timer (runs for fixed time regardless of cleanliness), traffic light controller (fixed timing), toaster (time-based).
6.3 Closed-Loop (Feedback) Control System
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Working: Feedback compares output with reference. Error signal drives controller to reduce error to zero.
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Advantages:
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High accuracy (reduces steady-state error).
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Disturbance rejection (compensates for $d(t)$).
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Reduced sensitivity to parameter variations in plant.
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Can stabilize unstable open-loop plants.
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Limitations:
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More complex, expensive (needs sensor).
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Potential for instability (oscillations) if not properly designed.
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May have slower response due to feedback loop.
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Examples:
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Temperature Control: Heater (MV) + Thermocouple (sensor) + Controller. Compensates for room temp changes (disturbance).
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Boiler Water Level Control (Classic Example):
DiagramCANVAS: Block diagram for boiler level: Level Transmitter (sensor) measures water level (c). Signal compared with Level Setpoint (r) in controller (e.g., PID). Controller output adjusts Feed Water Valve (MV) to maintain level. Disturbance: Steam demand changes (d). -
Position Control (Servomechanism): Motor + Position Encoder + Controller to move load to desired position.
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6.4 Control System Representation
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Block Diagram Algebra: Rules for interconnecting blocks.
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Series: $$\displaystyle G_{total} = G_1 G_2 $$
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Parallel: $$\displaystyle G_{total} = G_1 + G_2 $$
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Feedback: $$\displaystyle G_{total} = \frac{G}{1 + G H} $$ (negative feedback). $H$ is feedback transfer function.
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Signal Flow Graph: Alternative representation using nodes & branches. Mason's Gain Formula for overall transfer function.
[!TIP] Exam Essential: Be able to draw block diagrams for open-loop and closed-loop systems, label all components (controller, plant, sensor, comparator, disturbance), and explain the signal flow. For boiler level control, explicitly show the feedback path from level transmitter to comparator.