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ME-402 · INSTRUMENTATION & CONTROL/Quick Revision Short Notes

INSTRUMENTATION & CONTROL (ME-402) - Unit 1 Short Notes

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:

  1. 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).

  2. 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).

  3. Signal Processing / Data Acquisition Element: Further processes the conditioned signal (e.g., analog-to-digital conversion, computation, multiplexing) for analysis or control.

  4. 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

  • 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.

  • Standards:

    • Primary Standard: Highest accuracy, defines the unit (e.g., NIST, BIPM). Rarely used directly.

    • Secondary Standard: Calibrated against a primary standard. Used in national/regional labs.

    • Working Standard: Used routinely in laboratories/industry to calibrate instruments. Calibrated against secondary standards.

  • 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.

  • Traceability: The documented unbroken chain of comparisons (calibrations) linking a measurement result to a primary standard, with stated uncertainties at each step.

  • 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

  • Definition: The difference between the measured value and the true value.

  • Sources: Imperfections in instruments, environmental changes (temp, humidity), observer bias, method limitations.

  • Types:

    1. Systematic Errors: Consistent, predictable, repeatable. Can be corrected.

      • Calibration Error: Instrument not correctly calibrated.

      • Environmental Error: Changes in ambient conditions (e.g., thermal expansion).

      • Observational Error: Parallax, zero error.

    2. Random Errors: Unpredictable, caused by noise, small fluctuations. Characterized by precision. Reduced by averaging.

    3. Gross Errors / Mistakes: Human errors (reading wrong, recording error). Should be eliminated by careful procedure.

2.2 Uncertainty Analysis

  • 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.

  • Types:

    • Absolute Uncertainty ($\Delta x$): ± value with same unit as measurement (e.g., $25.46 \pm 0.02$ g).

    • Relative/Percentage Uncertainty ($\delta$): $$\displaystyle \delta = \frac{\Delta x}{x} \times 100\% $$.

  • Estimation from Specifications:

    • % of Full Scale Deflection (FSD): $$\displaystyle \Delta x = \pm \left( \frac{\%}{100} \times \text{Full Scale Value} \right) $$. Worse at low readings.

    • % of Reading (True Value): $$\displaystyle \Delta x = \pm \left( \frac{\%}{100} \times \text{Measured Value} \right) $$. Constant relative error.

  • Propagation of Uncertainties (for function $$\displaystyle z = f(x, y) $$):

    • For sum/difference: $$\displaystyle z = x + y \Rightarrow \Delta z = \sqrt{(\Delta x)^2 + (\Delta y)^2} $$

    • For product/quotient: $$\displaystyle z = x \cdot y \Rightarrow \frac{\Delta z}{z} = \sqrt{\left(\frac{\Delta x}{x}\right)^2 + \left(\frac{\Delta y}{y}\right)^2} $$

    • For constant multiplier: $$\displaystyle z = kx \Rightarrow \Delta z = |k| \Delta x $$

  • 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

  • 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).

  • 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

  • Time Delay / Dead Time ($\theta$): Time lag between application of input and start of output response.

  • Speed of Response:

    • 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 $$\displaystyle y(t) = K(1 - e^{-at}) $$.

    • 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.

  • Fidelity: Faithfulness of output waveform to input waveform, especially for periodic inputs. High fidelity means minimal amplitude/phase distortion.

  • Settling Time ($$\displaystyle t_s $$): Time for output to stay within a certain band (e.g., ±2%) of final value after a step.

  • Rise Time ($$\displaystyle t_r $$): Time for output to go from 10% to 90% (or 0% to 100%) of final value.

  • 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)

  • Significance: Converts a time-domain signal $x(t)$ into its frequency-domain representation $X(f)$. Reveals constituent frequencies and their amplitudes/phases.

  • Definition:

$$X(f) = \int_{-\infty}^{\infty} x(t) e^{-j2\pi ft} dt$$

Inverse FT: $$\displaystyle x(t) = \int_{-\infty}^{\infty} X(f) e^{j2\pi ft} df $$
  • Key Properties:

    • Linearity: $$\displaystyle \mathcal{F}\{a x_1(t) + b x_2(t)\} = a X_1(f) + b X_2(f) $$

    • Time-Shift: $$\displaystyle \mathcal{F}\{x(t - t_0)\} = X(f) e^{-j2\pi f t_0} $$ (introduces phase shift)

    • Frequency-Shift: $$\displaystyle \mathcal{F}\{x(t) e^{j2\pi f_0 t}\} = X(f - f_0) $$

  • 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).

  • Electrical Systems (LRC Circuits):

    • Resistor: $$\displaystyle v_R = iR $$

    • Capacitor: $$\displaystyle i_C = C \frac{dv_C}{dt} $$ or $$\displaystyle v_C = \frac{1}{C} \int i dt $$

    • Inductor: $$\displaystyle v_L = L \frac{di_L}{dt} $$

    • Example (Series RLC): $$\displaystyle L\frac{di}{dt} + Ri + \frac{1}{C}\int i dt = v_{in}(t) $$. Laplace: $$\displaystyle L s I(s) + R I(s) + \frac{1}{Cs} I(s) = V_{in}(s) $$.

$$G(s) = \frac{I(s)}{V_{in}(s)} = \frac{1}{Ls^2 + Rs + 1/C}$$

  • Mechanical Systems (Translational):

    • Mass ($m$): $$\displaystyle F = m \frac{d^2x}{dt^2} $$ (inertia)

    • Damper ($b$): $$\displaystyle F = b \frac{dx}{dt} $$ (viscous friction)

    • Spring ($k$): $$\displaystyle F = kx $$ (elasticity)

    • Example (Mass-Spring-Damper): $$\displaystyle m\ddot{x} + b\dot{x} + kx = F(t) $$. Laplace:

$$G(s) = \frac{X(s)}{F(s)} = \frac{1}{ms^2 + bs + k}$$

[!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

  • Bourdon Tube: Curved tube that straightens under pressure. Motion converted to pointer rotation. Robust, no power.

  • Bellows / Diaphragm: Flexible elements that expand/contract. Used for low pressure, differential pressure.

5.1.2 Manometers

  • U-tube: Simple, balances pressure head: $$\displaystyle P_1 - P_2 = \rho g h $$. Measures differential pressure.

  • Inclined Tube: Amplifies deflection ($$\displaystyle h = L \sin\theta $$), increases sensitivity for low pressures.

5.1.3 Pressure Transducers

  • Strain Gauge Type: Pressure acts on diaphragm, causing strain. Strain gauges in Wheatstone bridge measure strain → pressure.

  • Capacitive Type: Pressure changes diaphragm position → changes capacitance between plates.

  • 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.

  • Piezoresistive Type: Semiconductor strain gauge. Large gauge factor, sensitive to temperature.

5.1.4 Flow Measurement (Pressure-Based)

  • Venturi Meter: Converging-diverging tube. Pressure drop $$\displaystyle \Delta P \propto Q^2 $$. Low permanent pressure loss.

  • Orifice Meter: Thin plate with hole. Simple, but high energy loss & upstream disturbance.

  • Flow Nozzle: Compromise between venturi and orifice.

  • Pitot Tube: Measures flow velocity (stagnation pressure - static pressure $$\displaystyle \propto v^2 $$).

5.2 Temperature Measurement

5.2.1 Contact Sensors

  • 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.

  • Thermistor: Semiconductor, $$\displaystyle R = A e^{B/T} $$ (NTC: resistance ↓ with T). High sensitivity, non-linear, limited range.

  • 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).
  • Bimetallic Thermometer: Two metals with different $\alpha$ bonded. Bends with T. Mechanical, no power.

  • Liquid-in-Glass (Mercury/Alcohol): Thermal expansion of liquid in capillary. Simple, direct reading.

5.2.2 Non-Contact Sensors

  • Radiation Pyrometers:

    • Optical Pyrometer: Compares brightness of filament with object. Manual/automatic. Measures high T (>700°C).

    • Total Radiation Pyrometer: Measures total IR radiation. Output depends on emissivity.

5.3 Displacement, Position & Angular Measurement

5.3.1 Potentiometric Transducer

  • Principle: Wiper slides on resistive element. Displacement → variable resistance/voltage (voltage divider).

  • Types: Rotary, Linear.

  • Limitations: Loading effect (meter resistance draws current, causes error), wear, limited resolution.

5.3.2 Inductive Transducers

  • 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.
  • RVDT (Rotary Variable Differential Transformer): Same principle for angular displacement.

5.4 Strain, Load & Force Measurement

5.4.1 Resistance Strain Gauge

  • Principle: Piezoresistive effect. Strain $\epsilon$ changes resistance $\Delta R$.

  • 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).

  • Construction: Foil (most common), wire, semiconductor.

5.4.2 Strain Gauge Configurations (Wheatstone Bridge)

$$ \frac{\Delta R}{R} = GF \cdot \epsilon $$

  • Quarter Bridge: One active gauge. Output $$\displaystyle V_o \approx \frac{V_{ex}}{4} \cdot GF \cdot \epsilon $$. Temperature sensitive.

  • Half Bridge: Two active gauges (e.g., tension/compression). Output doubles, some temp. compensation.

  • Full Bridge: Four active gauges. Max output, excellent temp. compensation (adjacent arms opposite strain).

  • Signal Conditioning: Bridge excitation (low-noise DC/AC), amplification (instrumentation amp), filtering.

5.4.3 Load Cells

  • Principle: Strain gauges bonded to a structural element (load cell) that deforms under load.

  • Types: Compression, Tension, Bending beam, Shear beam.

  • 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

  • Principle: Relative motion between magnetic field & conductor induces EMF (Faraday's law: $$\displaystyle e = Blv $$ or $$\displaystyle e = k \omega $$).

  • DC Tachogenerator: Rotating magnet/armature → AC → commutator → DC voltage $\propto \omega$. Contact type.

  • 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

  • Centrifugal: Weights fly out with speed → pointer deflection. Bulky, inaccurate.

  • 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

  • Principle (Inverse): Apply stress → strain → electric charge (direct: stress → charge). Materials: Quartz (stable, low sensitivity), PZT (high sensitivity, but temp. sensitive).

  • Applications: Dynamic pressure, acceleration (seismic mass on crystal), force, ultrasonic generation/detection.

  • Limitation: Cannot measure static quantities (charge leaks away). Needs high-impedance amplifier.

5.6.2 Ionization Transducers

  • Principle: Ionizing radiation or gas molecule collisions create ion pairs. Current measured is proportional to pressure (in vacuum) or radiation intensity.

  • Ionization Gauge (Vacuum): Current from ionized gas molecules $\propto$ pressure (at very low pressures).

  • 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

  • Plant / Process: The physical system to be controlled (e.g., boiler, motor).

  • Controlled Variable (CV): The quantity to be maintained/regulated (e.g., temperature, level, speed).

  • Manipulated Variable (MV): The input to the plant adjusted by the controller (e.g., fuel valve opening, pump speed).

  • Input / Reference ($r(t)$): Desired value (setpoint) of the controlled variable.

  • Output ($c(t)$): Actual measured value of the controlled variable.

  • Disturbance ($d(t)$): Unwanted input affecting the plant output.

6.2 Open-Loop Control System

DiagramCANVAS: Block diagram: Input (Setpoint) → Controller → Plant → Output. No feedback path from Output to Comparator.
  • Working: Output has no effect on the control action. Controller acts based only on setpoint and maybe a fixed model.

  • Advantages: Simple, stable, easy to construct, no instability issues.

  • Limitations: Inaccurate (no correction for disturbances or model errors), no disturbance rejection, performance depends entirely on calibration.

  • 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

DiagramCANVAS: Block diagram: Summing point (Comparator) with inputs: Reference (r) and -Feedback (from sensor measuring output c). Error (e = r - c) → Controller → Plant → Output (c). Sensor measures c and feeds back. Disturbance (d) adds to plant output.
  • Working: Feedback compares output with reference. Error signal drives controller to reduce error to zero.

  • Advantages:

    • High accuracy (reduces steady-state error).

    • Disturbance rejection (compensates for $d(t)$).

    • Reduced sensitivity to parameter variations in plant.

    • Can stabilize unstable open-loop plants.

  • Limitations:

    • More complex, expensive (needs sensor).

    • Potential for instability (oscillations) if not properly designed.

    • May have slower response due to feedback loop.

  • Examples:

    • Temperature Control: Heater (MV) + Thermocouple (sensor) + Controller. Compensates for room temp changes (disturbance).

    • 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.

6.4 Control System Representation

  • Block Diagram Algebra: Rules for interconnecting blocks.

    • Series: $$\displaystyle G_{total} = G_1 G_2 $$

    • Parallel: $$\displaystyle G_{total} = G_1 + G_2 $$

    • Feedback: $$\displaystyle G_{total} = \frac{G}{1 + G H} $$ (negative feedback). $H$ is feedback transfer function.

  • 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.

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