Question 3 of 8: Root Locus Analysis and Proportional Gain Selection
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, December 2019 —
16-Elec-A2, Systems & Control. Three hours, closed book
(approved Casio or Sharp calculator plus one double-sided handwritten 8.5×11″ formula
sheet). Eight questions of 20 marks each. Questions 1 and 2 are compulsory;
candidates then choose three of the remaining six, so five questions constitute a complete
paper (100 marks). A short table of Laplace transforms and a page of standard second-order
plots and formulae are supplied with the paper. Every one of the eight questions is
solved below, because the full set is the more useful study resource.
Reference texts.
Nise, Control Systems Engineering, 8th ed. — root locus (Ch. 8), frequency
response and Nyquist (Ch. 10), design via frequency response (Ch. 11), state space (Ch. 12).
Ogata, Modern Control Engineering, 5th ed. — Routh–Hurwitz (§5.6),
lead/lag design (Ch. 6), state-space controllability and observability (Ch. 9).
Dorf & Bishop, Modern Control Systems, 13th ed. — performance of
second-order systems (Ch. 5), stability (Ch. 6).
Franklin, Powell & Emami-Naeini, Feedback Control of Dynamic Systems, 8th ed.
— dominant-pole approximation and pole placement (Ch. 7).
Check: figure reads. Questions 2, 3, 5 and 8 depend on
plotted data. Every value quoted below was read from the printed figures. Chart reads carry a
tolerance of roughly the last quoted digit; where a graphical read drives a design, the exact
analytical value is given alongside it.
Question 3: Root Locus Analysis and Proportional Gain Selection (20 marks)
Given. Unit-feedback loop with proportional gain $K_p$ acting on
$G(s) = (s+4)(s+8)/[s^2(s+6)]$: open-loop poles at $s = 0$ (double) and $s = -6$, open-loop zeros
at $s = -4$ and $s = -8$, so $n = 3$ and $m = 2$. Target overshoot 5%.
Find. The full root-locus geometry (asymptote angles, centroid, real-axis
segments, break points, and any imaginary-axis crossing with its critical gain); the gain
$K_{op}$ giving 5% overshoot together with the resulting settling time, rise time and steady-state
error; and a comment on how the true third-order response departs from the dominant-pair
estimate.
Approach. Apply the standard root-locus construction rules, then use the
Routh array to settle the question of an imaginary-axis crossing, search the locus for the gain
whose complex pair carries $\zeta = 0.69$, and finally weigh the third pole and the two finite
zeros against that pair to judge dominance.
Count branches and asymptotes. With $n = 3$ poles and $m = 2$ finite zeros
there are three branches; two terminate on the finite zeros at $-4$ and $-8$ and the remaining
$n-m = 1$ branch escapes to infinity. A single asymptote means the asymptote angle is
$$\theta = \frac{(2q+1)180^\circ}{n-m} = 180^\circ$$
i.e. the escaping branch runs out along the negative real axis. The centroid formula still
evaluates, to
$$\sigma_a = \frac{\sum p_i - \sum z_j}{n-m} = \frac{(0+0-6)-(-4-8)}{1} = +6$$
though with only one asymptote this value simply anchors a horizontal line rather than a fan.
Identify the real-axis segments. A point on the real axis belongs to the locus
when the count of real poles and zeros strictly to its right is odd. Counting rightwards from each
interval gives: to the right of the origin, zero items (even, not on the locus); between $-4$ and
$0$, the double pole at the origin counts twice (even, not on the locus); between $-6$ and $-4$,
two poles plus the zero at $-4$ is three (odd, on the locus); between $-8$ and
$-6$, four items (even, not on the locus); left of $-8$, five items (odd,
on the locus). So the real-axis locus is the segment $[-6,\,-4]$ together with the
ray $(-\infty,\,-8]$.
Departure from the double pole at the origin. Two branches leave the repeated
pole at $s = 0$. For a pole of multiplicity two the departure angles are separated by
$360^\circ/2 = 180^\circ$ and, by the angle criterion applied just off the origin, they leave
vertically at $\pm 90^\circ$. These two branches swing into the left half plane as a complex pair.
Locate the break point. Break points satisfy $dK/ds = 0$ where
$K(s) = -1/G(s) = -s^2(s+6)/[(s+4)(s+8)]$. Differentiating and clearing denominators leaves a
quartic whose only admissible real root is
$$s_b = -13.90$$
which does lie on the locus ray $(-\infty,-8]$. The associated gain is
$$K_b = -\frac{s_b^2(s_b+6)}{(s_b+4)(s_b+8)} = 26.13$$
This is a break-in point: the complex pair that left the origin returns to the
real axis there, after which one branch heads left to infinity and the other moves right to
terminate on the zero at $-8$.
Test for an imaginary-axis crossing. The closed-loop characteristic equation is
$$s^2(s+6) + K(s+4)(s+8) = s^3 + (6+K)s^2 + 12K\,s + 32K = 0$$
Building the Routh array, the $s^1$ element is
$$\frac{(6+K)(12K) - 32K}{6+K} = \frac{K\,(12K + 40)}{6+K}$$
Every coefficient and this element are strictly positive for all $K \gt 0$, so no
sign change ever occurs. Therefore
$$\boxed{\text{there is no imaginary-axis crossing: } \omega_{osc} \text{ and } K_{crit}
\text{ do not exist, and the loop is stable for every } K \gt 0}$$
This is consistent with the geometry: with a single asymptote at 180° and both finite zeros in
the left half plane, no branch can ever reach the $j\omega$ axis.
Figure 3.1 — Root locus of G(s) = (s+4)(s+8)/[s^2(s+6)]. Crosses mark open-loop poles, circles the zeros. The branches leave the double pole at the origin vertically, break in at -13.90, and no branch ever reaches the imaginary axis, so the loop is stable for every positive gain.
Find the gain giving 5% overshoot. Inverting the overshoot relation,
$$\zeta = \frac{-\ln(0.05)}{\sqrt{\pi^2+\ln^2(0.05)}} = 0.690$$
Searching the locus for the gain whose complex pair sits on the $\zeta = 0.690$ ray gives
$$\boxed{K_{op} = 10.14}$$
at which the three closed-loop roots are
$$s_{1,2} = -5.646 \pm j5.921, \qquad s_3 = -4.847$$
so the dominant pair has $\omega_n = |s_{1,2}| = 8.182$ rad/s and
$\zeta = 5.646/8.182 = 0.690$ as required.
Estimate the transient specifications. Using the dominant pair,
$$T_{s(\pm5\%)} = \frac{3}{\zeta\omega_n} = \frac{3}{5.646} = \boxed{0.531\ \text{s}}$$
$$T_{r(0-100\%)} = \frac{\pi - \cos^{-1}\zeta}{\omega_d}
= \frac{\pi - 0.808}{5.921} = \boxed{0.394\ \text{s}}$$
Note the question asks for the $\pm5\%$ settling band, hence the numerator 3 rather than 4.
Steady-state error. The open loop carries $s^2$ in its denominator, so the
system is Type 2. The position constant is infinite and
$$e_{ss(step)} = \frac{1}{1+K_{pos}} = \boxed{0\%}$$
independently of the gain — the double integrator tracks a step (and indeed a ramp) with no
residual error.
Compare the dominant model with the true response (part 3). Three effects make
the actual response differ from the clean second-order estimate. First, the third pole at $-4.847$
lies closer to the imaginary axis than the real part of the "dominant" pair at $-5.646$,
so on a naive separation test the pair is not dominant at all and the estimates above should be
suspect. What rescues them is the open-loop zero at $-4$: it sits only 0.85 units from that third
pole and very nearly cancels it, so the residue attached to the slow real mode is small and its
contribution to the step response is correspondingly weak. Second, the surviving zeros at $-4$ and
$-8$ differentiate the response, which typically raises the overshoot above the nominal 5% and
shortens the rise time relative to the pole-only formula. Third, because the near-cancellation is
imperfect, a small slowly decaying tail persists that the second-order model does not predict, so
the true settling time tends to be slightly longer than 0.531 s. The estimates remain useful
engineering approximations, but the dominance claim here rests on the pole–zero
near-cancellation, not on pole separation, and that should be stated explicitly.