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Semester 4• Course: EEE2005 Paired Lab: EEE2055• technical track5 min read

Control Systems Engineering

Transfer functions, mathematical modeling of physical systems, block diagram reduction, signal flow graphs, time response, Routh-Hurwitz, Root Locus, and Bode/Nyquist stability.

Study Progress0 of 4 completed (0%)

Syllabus Units (4)

  1. Unit 1

    Mathematical Modeling, Block Diagrams & Signal Flow Graphs

    Differential equations of physical systems, mechanical translational and rotational systems, Force-Voltage (F-V) and Force-Current (F-I) analogies, transfer function derivations, block diagram algebra and reduction rules, and Mason’s Gain Formula for Signal Flow Graphs (SFG).

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  2. Unit 2

    Time Response Analysis & Transient Specifications

    Standard test signals, first-order step and impulse responses, prototype second-order system dynamics across undamped, underdamped, critically damped, and overdamped regimes, transient response specifications (delay, rise, peak time, %Mp, and settling time), steady-state error analysis, static error constants (Kp, Kv, Ka), and system types.

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  3. Unit 3

    Stability Analysis & Root Locus Techniques

    Concept of BIBO and asymptotic stability, characteristic equation and s-plane pole locations, Routh-Hurwitz stability criterion with special cases (first column zero and all-zero row / auxiliary polynomial), marginal stability, Evans Root Locus fundamentals, angle and magnitude criteria, construction rules (real-axis segments, asymptotes, centroid, breakaway points, departure angles, jω crossings), and s-plane transient design bounds.

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  4. Unit 4

    Frequency Response & State Variable Analysis

    Frequency domain specifications (resonant peak Mr, resonant frequency ωr, bandwidth ωBW), Bode magnitude and phase plots, gain and phase margins, polar plots, Nyquist stability criterion (encirclement formula N = P - Z), state variable concepts, canonical state-space forms (controllable, observable), Resolvent matrix (sI - A)⁻¹, State Transition Matrix (STM) Φ(t) = e^(At), and Kalman controllability and observability rank tests.

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