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17-Phys-B5 Systems and Control · May 2017

Question 7 of 8: Root Locus, Critical Gain, and a 5% Overshoot Design

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

Notes on this paper

Paper format. 98-Phys-B5 Control, National Examination May 2017 — a three-hour closed-book examination with one double-sided handwritten formula/notes sheet permitted and an approved calculator. Questions 1 and 2 are compulsory; candidates choose three of the remaining six (3–8). Every question is nonetheless answered in full below so the paper remains a complete study resource. All eight questions carry equal value (20 marks each).

Reference texts. N. S. Nise, Control Systems Engineering, 7th ed. (transient-response specifications, root locus, Routh–Hurwitz, frequency-response and Nyquist stability, state-space representation, steady-state errors); K. Ogata, Modern Control Engineering, 5th ed. (root-locus and PID compensator design, controllability/ observability, Mason's Gain Formula on signal-flow graphs).

Question 7: Root Locus, Critical Gain, and a 5% Overshoot Design (20 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.

Re −18 Im (jω) centroid −4.33 −2 −4 −7 breakaway −2.88 j7.07 (ωosc, Kcrit=59.4) Kop≈3.82 dominant pole 3rd pole −8.37 (at Kop)
Figure Q7.2 — root locus for $G(s)=10/[(s+2)(s+4)(s+7)]$: real-axis branches (poles $-2,-4$ merging at the breakaway point $-2.88$; pole $-7$ moving left), the complex branches through the $j\omega$-axis crossing at $K_{crit}=59.4$, and the design pole at $K_{op}\approx3.82$.

Given. $G(s)=10/[(s+2)(s+4)(s+7)]$, unity feedback, proportional gain $K_p$.

Find. 1) Asymptote angles, breakaway point, centroid, $j\omega$-crossing ($\omega_{osc}$, $K_{crit}$). 2) $K_{op}$ for $PO\approx5\%$ and the resulting $T_{settle(\pm5\%)}$, $T_{rise(0-100\%)}$, $e_{ss(step\%)}$. 3) Commentary on the dominant-pole model's accuracy.

Approach. Apply the standard root-locus rules (real-axis segments, asymptote angles/centroid, breakaway via $dK_p/ds=0$) to the open-loop poles $-2,-4,-7$; find the $j\omega$-crossing via Routh–Hurwitz on the characteristic polynomial. For the design, invert the overshoot formula for $\zeta$, find where the $\zeta$-line intersects the locus by the angle condition, then read $K_{op}$ and the transient specs off the standard 2nd-order formulas.

  1. Part 1) — asymptotes, centroid, breakaway. Three poles, no zeros $\Rightarrow$ 3 asymptotes at $\theta=\dfrac{(2k{+}1)180^\circ}{3}=\boxed{60^\circ,180^\circ,300^\circ}$, centroid $\sigma_a=\dfrac{-2-4-7}{3}=\boxed{-4.33}$. Real-axis locus exists on $(-4,-2)$ and $(-\infty,-7)$ (odd pole/zero count to the right). Breakaway: with $f(s)=(s+2)(s+4)(s+7)=s^3+13s^2+50s+56$, solve $f'(s)=3s^2+26s+50=0\Rightarrow s=-2.88\ \text{or}\ -5.79$; only $s=-2.88$ lies ON the locus segment $(-4,-2)$ (the other root, $-5.79$, falls in $(-7,-4)$ where the locus does NOT exist — an even pole count to the right — so it is rejected): $\boxed{\text{breakaway}=-2.88}$.
  2. Part 1) — $j\omega$-crossing via Routh–Hurwitz. Char. eq. $s^3+13s^2+50s+56+10K_p=0$. Routh's $s^1$ row vanishes at $K_p=\tfrac{13(50)-(56+10K_p)}{13}=0\Rightarrow\boxed{K_{crit}=59.4}$; the auxiliary equation from the $s^2$ row, $13s^2+(56+594)=0$, gives $s^2=-50\Rightarrow \boxed{\omega_{osc}=\sqrt{50}\approx7.07\ \text{rad/s}}$ (matching the orange markers in the sketch, where the third, real closed-loop pole sits at exactly $s=-13$).
  3. Part 2) — damping ratio and dominant pole for $PO\approx5\%$. Inverting $PO=100e^{-\zeta\pi/\sqrt{1-\zeta^2}}=5$ gives $\boxed{\zeta\approx0.690}$ ($\theta=\cos^{-1}\zeta\approx46.4^\circ$ off the negative real axis). Solving the angle condition (sum of angles from the three poles $=180^\circ\pmod{360^\circ}$) numerically along this $\zeta$-line locates the dominant closed-loop pole at $$s_{dom}\approx-2.315\pm j2.427\quad(\omega_n=|s_{dom}|\approx3.354\ \text{rad/s}).$$ Evaluating $K_p=-f(s_{dom})/10$ at that point gives $\boxed{K_{op}\approx3.82}$ (the third closed-loop pole from the resulting cubic lands at $s\approx-8.37$, real, as marked in green above).
  4. Part 2) — step-response estimates. Using $\sigma=\zeta\omega_n=2.315$ and $\omega_d=2.427$: $T_{settle(\pm5\%)}\approx3/\sigma\approx\boxed{1.30\ \text{s}}$; $T_{rise(0-100\%)}=(\pi-\cos^{-1}\zeta)/\omega_d\approx\boxed{0.96\ \text{s}}$ (exact closed form for a pure 2nd-order, zero-free response); and with $G(0)=10/(2\cdot4\cdot7)=0.1786$, $$e_{ss(step)\%}=\frac{100}{1+K_{op}G(0)}=\frac{100}{1+3.82(0.1786)}\approx\boxed{59.5\%}$$ (a large residual error, since this is Type 0 proportional-only control — no integrator to drive it to zero).
  5. Part 3) — dominant-pole model vs. the actual response. The third closed-loop pole ($-8.37$) is only $8.37/2.315\approx3.6\times$ farther from the imaginary axis than the dominant pair's real part — short of the usual $\ge5\times$–$10\times$ separation needed for the 2nd-order estimate to be accurate. A direct time-domain simulation of the actual (3rd-order) closed loop at $K_{op}$ confirms this: the true peak overshoot is only $\approx4.7\%$ (slightly under the nominal 5%) and the response re-enters the $\pm5\%$ band by $t\approx0.85$ s — noticeably FASTER than the $1.30$ s dominant-pole estimate. $\boxed{\text{The third pole's own decay measurably speeds up settling and slightly trims the overshoot versus the pure 2nd-order prediction.}}$
Final results — Question 7
PartResult
1) locus geometryasymptotes $60^\circ,180^\circ,300^\circ$; centroid $-4.33$; breakaway $-2.88$
1) $j\omega$ crossing$\omega_{osc}\approx7.07$ rad/s, $K_{crit}=59.4$
2) design$\zeta\approx0.690$, $K_{op}\approx3.82$
2) step specs$T_{settle(5\%)}\approx1.30$ s, $T_{rise}\approx0.96$ s, $e_{ss}\approx59.5\%$
3) model accuracy3rd pole only $\sim3.6\times$ separated → actual response settles faster, overshoots slightly less