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22-Elec-A2 Systems and Control · May 2013

Question 3 of 8: Root locus and series-PID settling-time design

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

Notes on this paper

Paper format. National Exams, 07-Elec-A2 Systems & Control, May 2013, 3 hours, closed book (approved calculator + one handwritten formula sheet, and a printed short table of Laplace transforms). Eight questions of 20 marks each; Questions 1 and 2 are compulsory and the candidate chooses three of the remaining six (100 marks total). Every question is worked in full below, since the whole set is a study resource.

Reference texts: N. S. Nise, Control Systems Engineering (7th ed., Wiley) — root locus (Ch. 8), frequency-response / Bode and Nyquist (Ch. 10), stability and Routh–Hurwitz (Ch. 6), PID and cascade compensation (Ch. 9), steady-state error (Ch. 7), state space and pole placement (Ch. 11–12); K. Ogata, Modern Control Engineering (5th ed., Prentice Hall) — companion treatment of the s-domain, dominant-poles modelling and controllability/observability; G. F. Franklin, J. D. Powell & A. Emami-Naeini, Feedback Control of Dynamic Systems. All block diagrams, root loci, Bode/Nyquist plots and pole–zero maps below are redrawn as inline figures.

Reading the exam figures. Two questions (Q2 and Q6) require reading a second-order model off a printed step-response curve; the values read from those curves are stated explicitly in the Given block so a reader can reproduce every subsequent number.

Question 3 — Root locus and series-PID settling-time design [7 + 8 + 5]

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.

R(s)+−ControllerC(s)series PIDProcessG(s)Y(s)
Figure Q3.1 — Series PID $C(s)=K_p(1+\tfrac{1}{0.1s})(1+0.125s)$ and process $G(s)=1/(s^2+17s+30)$, $\;s^2+17s+30=(s+2)(s+15)$.

Part A — Detailed root locus [7]

Approach. Reduce the series PID to a single open-loop transfer function, then apply the standard rules (real-axis segments, asymptotes, break-away/break-in, jω crossings).

  1. Open-loop transfer function. $C(s)=K_p\dfrac{(0.1s+1)(0.125s+1)}{0.1s}=0.125K_p\dfrac{(s+10)(s+8)}{s}$, so $$L(s)=C(s)G(s)=K'\,\frac{(s+8)(s+10)}{s(s+2)(s+15)},\qquad K'=0.125K_p.$$ Open-loop poles $0,-2,-15$; open-loop zeros $-8,-10$.
  2. Real-axis segments. Left of an odd count of real singularities: $[-2,0]$, $[-10,-8]$, and $(-\infty,-15]$.
  3. Asymptotes and centroid. $n-m=3-2=1$, so a single asymptote at $180^\circ$ (the negative-real axis); the centroid $\sigma_a=\dfrac{(0-2-15)-(-8-10)}{1}=+1$ is not meaningful for a single asymptote.
  4. Break-away / break-in. Solving $\dfrac{d}{ds}\!\left[\dfrac{s(s+2)(s+15)}{(s+8)(s+10)}\right]=0$ gives a break-away at $s\approx-1.09$ (on $[-2,0]$) and a break-in at $s\approx-8.96$ (on $[-10,-8]$).
  5. Imaginary-axis crossings. The characteristic polynomial $s^3+(17+K')s^2+(30+18K')s+80K'=0$ has Routh $s^1$ entry $\dfrac{18K'^2+256K'+510}{17+K'}\gt 0$ for all $K'\gt 0$, so no branch ever crosses the $j\omega$-axis. The loop is stable for every $K_p\gt 0$; there is no finite critical gain ($K_{crit}\to\infty$, $\omega_{osc}$ not applicable).
ReIm-16-14-12-10-8-6-4-22Root locus — poles 0, −2, −15; zeros −8, −10; single asymptote at 180°
Figure Q3.2 — Root locus. The origin/$-2$ poles break away at $-1.09$, arc into the left half-plane, and break in at $-8.96$ before ending on the zeros $-8,-10$; the third branch runs from $-15$ to $-\infty$. No $j\omega$ crossing — stable for all $K_p\gt 0$.

Part B — Gain for 0.5 s settling and equivalent damping [8]

Approach. $T_{settle(\pm2\%)}=4/(\zeta\omega_n)=0.5\ \text{s}$ fixes the dominant real part at $\sigma=\zeta\omega_n=8$; find the point on the complex arc with $\mathrm{Re}(s)=-8$ and the gain that puts a closed-loop pole there.

  1. Required real part. $\sigma=4/T_{settle}=4/0.5=8$, so the dominant closed-loop poles must sit on the vertical line $\mathrm{Re}(s)=-8$.
  2. Gain from the magnitude criterion. Enforcing a root at $s=-8+j\omega_d$ on the locus gives $K'=0.125K_p=31.8$, i.e. $$\boxed{K_p\approx254}.$$ The three closed-loop poles are then $-8\pm j3.68$ and $-32.8$.
  3. Equivalent damping ratio. For the dominant pair, $\omega_n=\sqrt{8^2+3.68^2}=8.81\ \text{rad/s}$ and $$\zeta=\frac{\sigma}{\omega_n}=\frac{8}{8.81}=\boxed{0.91}.$$

Part C — Accuracy of the dominant-poles model [5]

Discussion. The assumed second-order dominant-poles model is only partially accurate here. Two effects distort it: (i) the third closed-loop pole at $-32.8$ is about four times deeper than the dominant real part $-8$, so it is genuinely fast and contributes little — this part of the model assumption is sound; but (ii) the closed-loop zeros inherited from the PID sit at $-8$ and $-10$, right on top of the dominant poles. The zero at $-8$ nearly coincides with the dominant real part, so it strongly reshapes the transient. Compared with the ideal $\zeta=0.91$ (essentially no-overshoot) model, the real response will show a noticeably faster rise time and a larger percent overshoot than the model predicts (a nearby zero always adds overshoot and speeds the rise), while the settling time stays close to the 0.5 s target because it is governed by the dominant real part $-8$, which the zeros do not move. The dominant-poles model therefore predicts settling time well but underestimates overshoot and rise speed.

QuantityResult
Centroid / asymptotesingle asymptote at $180^\circ$
Break-away / break-in$s_b=-1.09$ / $s_b=-8.96$
Critical gain, $\omega_{osc}$none — stable for all $K_p\gt 0$
Proportional gain for $T_s=0.5$ s$K_p\approx254$ (closed-loop poles $-8\pm j3.68$, $-32.8$)
Equivalent damping ratio$\boxed{\zeta\approx0.91}$