Question 8 of 8: Root Locus Analysis, Gain Selection and Response Estimation
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, 16-Elec-A2 Systems & Control, December 2018 — 3 hours, CLOSED BOOK (approved calculator plus one double-sided handwritten aid sheet). Eight questions of 20 marks each; Questions 1 and 2 are compulsory and the candidate chooses three of the remaining six, so five answers make a complete paper (100 marks). All eight questions are solved here, because the set is intended as a study resource. A short Laplace-transform table and the standard second-order design charts are supplied with the paper.
Reference texts. N. S. Nise, Control Systems Engineering, 8th ed. (root locus, frequency-domain design, steady-state error); K. Ogata, Modern Control Engineering, 5th ed. (Routh–Hurwitz, state-space methods); R. C. Dorf and R. H. Bishop, Modern Control Systems, 13th ed. (dominant-pole modelling, lag/lead compensator design); G. F. Franklin, J. D. Powell and A. Emami-Naeini, Feedback Control of Dynamic Systems, 8th ed.
Question 8: Root Locus Analysis, Gain Selection and Response Estimation (20 marks)
Find. The complete root-locus geometry (asymptote angles and centroid, break points, imaginary-axis crossing and critical gain); the gain meeting the 5% overshoot target with the associated settling time, rise time and steady-state error; and a critique of the dominant-pole prediction.
Approach. Apply the standard construction rules, then solve $dK/ds = 0$ for the break points and test the Routh array for imaginary-axis crossings; select the gain where the locus meets the required damping ray; and finally check the third pole and the zero before trusting the estimates.
Count branches and locate real-axis segments. With $n = 3$ poles and $m = 1$ zero there are three branches; one terminates on the finite zero at $-3$ and the other two run to infinity. A point on the real axis belongs to the locus when the number of real poles and zeros strictly to its right is odd. That gives the segments $$[-3,\,-2] \quad\text{and}\quad [-10,\,-5].$$ The interval $[-5,-3]$ has two singularities to its right and so is excluded.
Asymptote angles and centroid. The two branches heading to infinity follow asymptotes at $$\theta_a = \frac{(2q+1)180^\circ}{n - m} = \frac{180^\circ}{2},\ \frac{540^\circ}{2} = \pm 90^\circ,$$ radiating from the centroid $$\sigma_a = \frac{\sum p_i - \sum z_j}{n - m} = \frac{(-2 - 5 - 10) - (-3)}{2} = \frac{-14}{2} = -7.$$ So the pair leaves the real axis and climbs vertically near $\mathrm{Re}\,s = -7$.
Break points. On the locus $K_p = -1/G(s)$, i.e. $$K_p(s) = -\frac{(s+2)(s+5)(s+10)}{5(s+3)}.$$ Setting $dK_p/ds = 0$ and solving gives a single real root inside a locus segment, $$\boxed{s_b = -7.367 \text{ (break-away)}, \qquad K_p(s_b) = 1.53.}$$ It lies in $[-10,-5]$, so the two branches from the poles at $-5$ and $-10$ meet there at gain 1.53 and depart perpendicular to the real axis. The segment $[-3,-2]$ carries no break point: that branch simply travels from the pole at $-2$ to the zero at $-3$ as the gain rises.
Test for an imaginary-axis crossing. The closed-loop characteristic polynomial is $$1 + K_p G(s) = 0 \;\Rightarrow\; s^3 + 17 s^2 + (80 + 5K_p)s + (100 + 15K_p) = 0.$$ Its Routh array has first column $1$, $17$, $\dfrac{17(80+5K_p) - (100+15K_p)}{17} = \dfrac{1260 + 70K_p}{17}$, and $100 + 15K_p$. Every one of these is strictly positive for all $K_p \gt 0$; the $s^1$ entry never vanishes.
State the stability conclusion. Because no Routh entry changes sign, $$\boxed{\text{the locus never crosses the imaginary axis: the loop is stable for every } K_p \gt 0.}$$ There is therefore no finite $K_{crit}$ and no $\omega_{osc}$ — formally $K_{crit} \to \infty$. The geometry says the same thing: the two infinite branches follow vertical asymptotes anchored at $\sigma_a = -7$, deep in the left half-plane, so they can never reach the axis. This is a legitimate and complete answer to the part of the question that asks for the crossover coordinates.
Part 2 — convert the overshoot target into a damping ratio. With $PO = 5\%$ and $L = \ln 0.05 = -2.9957$, $$\zeta = \frac{2.9957}{\sqrt{9.8696 + 8.9744}} = \frac{2.9957}{4.3410} = 0.690.$$ The design point is where the locus crosses the ray at $\theta = \cos^{-1} 0.690 = 46.4^\circ$ from the negative real axis.
Find the gain at that point. Sweeping $K_p$ and factoring the cubic, the complex pair reaches $\zeta = 0.690$ at $$\boxed{K_{op} = 13.12,}$$ where the closed-loop roots are $s_{1,2} = -7.097 \pm j\,7.443$ and $s_3 = -2.806$. The dominant pair therefore has $\omega_n = |s_1| = 10.28$ rad/s and $\sigma = \zeta\omega_n = 7.097$ s$^{-1}$.
Settling time and rise time. Using the five-percent criterion requested, $$T_{s(\pm 5\%)} = \frac{3}{\zeta\omega_n} = \frac{3}{7.097} = 0.423\ \text{s},$$ and with $\omega_d = 7.443$ rad/s the rise time is $$T_{r(0-100\%)} = \frac{\pi - \cos^{-1}\zeta}{\omega_d} = \frac{3.1416 - 0.8097}{7.443} = 0.313\ \text{s}.$$
Steady-state error. The loop is Type 0, so $$K_{pos} = K_{op}\,G(0) = 13.12 \times \frac{5 \times 3}{2 \times 5 \times 10} = 13.12 \times 0.15 = 1.968,$$ and $$e_{ss(step)\%} = \frac{100}{1 + K_{pos}} = \frac{100}{2.968} = 33.7\%.$$ That is a very large error — the inevitable consequence of choosing the gain purely for damping on a Type-0 plant.
Part 3 — where the model and reality part company. Three effects will make the measured response differ from the second-order prediction. First, the third closed-loop pole at $-2.806$ is actually closer to the imaginary axis than the complex pair at $-7.097$, so the usual dominance argument is inverted; the only thing that rescues the model is the open-loop zero at $-3$, which sits just $0.194$ away from that pole and very nearly cancels it. Second, that near-cancellation is not exact, so a small slow exponential tail rides on the fast oscillation and stretches the effective settling time beyond the predicted 0.42 s. Third, the closed-loop zero itself adds derivative action, which tends to increase overshoot slightly above the nominal 5% while quickening the initial rise. In short, the predicted specifications are sound as engineering estimates but should be treated as approximate, and the large 33.7% steady-state error — which the model reports correctly — is the real limitation of proportional-only control here.
Root locus for Kp > 0 with the break-away point, the vertical asymptotes at σa = −7, and the design point at Kop = 13.12 marked. The branches never reach the imaginary axis.
Unit step response at Kop = 13.12: the exact third-order closed loop against the dominant second-order model. The offset from unity is the 33.7% steady-state error of the Type-0 loop.
Check: the question asks for ωosc and Kcrit, which presupposes an imaginary-axis crossing. For this plant there is none — both the Routh test and the asymptote geometry confirm unconditional stability for Kp > 0 — so the honest answer is that no finite critical gain exists. A crossing would appear only for negative gain, which is outside the stated proportional-control configuration.