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22-Mec-A3 System Analysis and Control · May 2015

Question 1 of 6: Asymptotic Bode Magnitude Plots

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. 07-Mec-A3 System Analysis and Control, National Exams May 2015 — 3 hours, closed book (approved Casio or Sharp calculator and semi-log graph paper only). Six questions; the paper instructs that "any four questions constitute a complete paper" and that all questions are of equal value, so each question is worth 25 marks. All six are solved here. A Laplace-transform table is supplied with the paper (pages 5–6).

Reference texts. K. Ogata, Modern Control Engineering, 5th ed. (Pearson) — Ch. 5 (transient response), Ch. 6 (root locus), Ch. 7 (frequency response); N. S. Nise, Control Systems Engineering, 8th ed. (Wiley) — Ch. 4, 6, 8, 10; R. C. Dorf and R. H. Bishop, Modern Control Systems, 13th ed. (Pearson); G. F. Franklin, J. D. Powell and A. Emami-Naeini, Feedback Control of Dynamic Systems, 8th ed. (Pearson).

Question 1: Asymptotic Bode Magnitude Plots (25 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given. Two open-loop transfer functions: (a) $G_a(s) = \dfrac{4}{s+2}$, a single real pole at $s=-2$; (b) $G_b(s) = \dfrac{4}{(0.4s+1)(s+1)}$, two real poles written already in time-constant form with $\tau_1 = 0.4\ \text{s}$ and $\tau_2 = 1\ \text{s}$.

Find. The straight-line (asymptotic) log-magnitude characteristic of each function in decibels against $\log_{10}\omega$, with the low-frequency level, every corner frequency, and every asymptote slope identified.

Approach. Put each factor into the normalised Bode form $(1+j\omega\tau)$, read the low-frequency asymptote from the resulting constant, then add one $-20\ \text{dB/decade}$ break at each pole corner $\omega_c = 1/\tau$.

  1. Normalise (a) to time-constant form. A Bode plot is drawn from factors of the form $(1+j\omega\tau)$, so the pole binomial must be scaled so that its constant term is unity: $$G_a(s)=\frac{4}{s+2}=\frac{4}{2\left(\tfrac{s}{2}+1\right)}=\frac{2}{0.5s+1}$$ The Bode gain is therefore $K_B = 2$, not 4. This normalisation is the single most common place to lose marks: reading the gain as 4 puts the whole plot 6 dB too high.
  2. Low-frequency asymptote of (a). As $\omega \to 0$ the denominator tends to unity, so $$20\log_{10}|G_a| \to 20\log_{10}(2) = \boxed{6.02\ \text{dB}}$$ This horizontal line is the entire plot below the corner.
  3. Corner frequency and high-frequency slope of (a). The break occurs where the imaginary part of the normalised factor equals its real part, i.e. at $\omega_c = 1/\tau = 1/0.5 = 2\ \text{rad/s}$. Above it the single pole contributes $-20\ \text{dB/decade}$, so the magnitude falls linearly at that rate. Starting from 6.02 dB at the corner, the asymptote reaches $0\ \text{dB}$ after $6.02/20 = 0.301$ decade, i.e. at $\omega = 2 \times 10^{0.301} = 4\ \text{rad/s}$ — one octave above the corner. The exact curve runs $3.01\ \text{dB}$ below the asymptote at the corner, and it crosses unity gain slightly earlier than the asymptote predicts: $|G_a(j\omega)|=1$ requires $|j\omega+2| = 4$, giving $\omega = \sqrt{12} = 3.46\ \text{rad/s}$.
0.1110100-40-30-20-1001020ω=2ω (rad/s, log scale)|G| (dB)G(s) = 4/(s+2) = 2/(0.5s+1)asymptote (blue), exact (red dashed)0 dB crossing at ω = 4 rad/s
Question 1(a): asymptotic (solid) and exact (dashed) magnitude of $G_a(s)=4/(s+2)$. Corner at 2 rad/s; the exact curve is 3 dB below the break point.

Part (b) needs no algebraic normalisation because both binomials are already printed in time-constant form, so the constant 4 is the Bode gain.

  1. Low-frequency asymptote of (b). With both factors tending to unity, $$20\log_{10}|G_b| \to 20\log_{10}(4) = \boxed{12.04\ \text{dB}}$$
  2. Locate both corners and accumulate the slopes. The corner of a $(1+j\omega\tau)$ factor is $\omega_c = 1/\tau$: $$\omega_{c1}=\frac{1}{1}=1\ \text{rad/s},\qquad \omega_{c2}=\frac{1}{0.4}=2.5\ \text{rad/s}$$ The slope is therefore $0\ \text{dB/dec}$ below 1 rad/s, $-20\ \text{dB/dec}$ between 1 and 2.5 rad/s, and $-40\ \text{dB/dec}$ above 2.5 rad/s.
  3. Evaluate the asymptote at the second corner. Falling at $-20\ \text{dB/dec}$ from 12.04 dB over the interval $1 \to 2.5\ \text{rad/s}$ (a factor 2.5, i.e. $\log_{10}2.5 = 0.398$ decade): $$12.04 - 20(0.398) = 4.06\ \text{dB}$$ so the second break starts from $4.06\ \text{dB}$ and the $-40\ \text{dB/dec}$ tail runs from there. Solving $|G_b(j\omega)| = 1$ numerically gives the exact unity-gain crossing at $\omega = 2.59\ \text{rad/s}$; the asymptotic construction predicts $2.79\ \text{rad/s}$, the usual few-per-cent optimism when two corners lie close together.
0.1110100-70-60-50-40-30-20-1001020ω=1ω=2.5ω (rad/s, log scale)|G| (dB)G(s) = 4/[(0.4s+1)(s+1)]slope 0 → -20 → -40 dB/decexact crossover ω = 2.59 rad/s
Question 1(b): asymptotic (solid) and exact (dashed) magnitude of $G_b(s)=4/[(0.4s+1)(s+1)]$, showing the 0 / −20 / −40 dB-per-decade segments.
Quantity(a) $4/(s+2)$(b) $4/[(0.4s+1)(s+1)]$
Bode (time-constant) gain24
Low-frequency asymptote6.02 dB12.04 dB
Corner frequencies2 rad/s1 and 2.5 rad/s
Asymptote slopes0, then −20 dB/dec 0, −20, then −40 dB/dec
Magnitude at last corner6.02 dB (asym.), 3.01 dB (exact) 4.06 dB (asym.)
Exact 0 dB crossing3.46 rad/s2.59 rad/s
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