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22-Elec-A2 Systems and Control · May 2015

Question 4 of 8: Stability range from Bode, root locus and Routh–Hurwitz

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 2015, 3 hours, closed book (approved Casio/Sharp calculator plus one signed, double-sided 8.5 × 11" formula/notes sheet; a Laplace-transform table and design plots are supplied with the paper). Questions 1 and 2 are compulsory; a complete paper is five questions, so candidates choose three of Q3–Q8. Each question is worth 20 marks. All eight are worked below so the set is a complete study resource.

Reference texts: N. S. Nise, Control Systems Engineering (7th ed., Wiley) — time response and second-order specifications (Ch. 4), block/signal-flow reduction and Mason’s rule (Ch. 5), Routh–Hurwitz stability (Ch. 6), steady-state error and static error constants (Ch. 7), root locus (Ch. 8), PID / lead–lag design (Ch. 9–11), frequency response, Bode, Nyquist, gain and phase margins (Ch. 10–11), state space, controllability/observability and pole placement (Ch. 3, 12); K. Ogata, Modern Control Engineering (5th ed., Prentice Hall) — dominant-poles modelling and Mason’s gain formula; G. F. Franklin, J. D. Powell & A. Emami-Naeini, Feedback Control of Dynamic Systems. All block diagrams, pole–zero maps, root loci, Bode plots, signal-flow graphs and the Nyquist plot below are redrawn as inline figures.

Reading the exam figures. Where a transfer function is stated exactly (Q1–Q5, Q7, Q8A) every result is confirmed analytically and the exact model governs. Q4 supplies a Bode plot ($G_m=16.1$ dB at $2.05$ rad/s, $P_m=-85.1^\circ$ at $0.589$ rad/s) and a root locus; Q5 Parts A–B and Q6 use printed frequency-response plots, and Q8B a printed Nyquist diagram — values read from those curves are flagged as reads and cross-checked against the analytics wherever a transfer function is available.

Question 4 — Stability range from Bode, root locus and Routh–Hurwitz [10 + 10]

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. The PID term simplifies: $\left(1+\tfrac{1}{2s}\right)(1+0.5s)=\dfrac{0.5s^2+1.25s+0.5}{s}=\dfrac{0.5(s+2)(s+0.5)}{s}$, so $G_{open}(s)=\dfrac{5K_p(s+2)(s+0.5)}{s^2(s+20)(s-1)}$: poles $0,0,-20,+1$ (one RHP pole), zeros $-2,-0.5$.

Find. The stable range of $K_p$, twice (graphically and by Routh).

[Figure not reproduced: Figure Q4.2 redrawn — the branch from the RHP pole at $+1$ and the double-integrator branches migrate into the left half-plane, crossing the imaginary axis at $\pm j2.05$; the loop becomes stable only above that gain. See the official exam paper.]

Part 1 — Stability range from the figures [10]

Approach. With an open-loop RHP pole the system is stable only for sufficient gain (Nyquist needs the $-1$ point encircled once); the Bode gain margin measures the distance from the plotted gain to that boundary.

  1. Read the Bode margin. The plot (drawn at $K_p=1$) shows $G_m=16.1$ dB at the phase-crossover $\omega=2.05$ rad/s. Thus the gain must be raised by $16.1$ dB, i.e. by a factor $10^{16.1/20}=6.4$, to reach marginal stability: $\boxed{K_{p,\min}\approx6.4}$.
  2. Read the root locus. The branches originating at the origin and at the RHP pole $+1$ move left as $K_p$ increases and cross the $j\omega$-axis at $\pm j2.05$; for gains above the crossing all closed-loop poles lie in the LHP.
  3. Range. Both figures agree: $\boxed{K_p\gt6.4}$ (no finite upper limit — higher gain only moves the poles deeper into the LHP).

Part 2 — Routh–Hurwitz verification [10]

Approach. Form the closed-loop characteristic polynomial $s^2(s+20)(s-1)+5K_p(s+2)(s+0.5)=0$ and require a positive first column.

  1. Characteristic polynomial. $$s^4+19s^3+(5K_p-20)s^2+12.5K_p\,s+5K_p=0.$$
  2. Routh array. $$\begin{array}{c|ccc}s^4&1&5K_p-20&5K_p\\s^3&19&12.5K_p&\\s^2&\frac{82.5K_p-380}{19}&5K_p&\\s^1&c_1&&\\s^0&5K_p&&\end{array}$$ with $c_1=12.5K_p-\dfrac{95K_p}{(82.5K_p-380)/19}$.
  3. First-column conditions. $5K_p\gt0$ (all $K_p\gt0$); the $s^2$ entry $\gt0$ needs $K_p\gt4.61$; the $s^1$ entry $c_1\gt0$ needs $12.5(82.5K_p-380)\gt1805\Rightarrow K_p\gt6.36$. The binding condition is $\boxed{K_p\gt6.36}$.
  4. Oscillation frequency. At $K_p=6.36$ the $s^2$-row auxiliary equation gives $s^2=-\dfrac{5K_p}{7.6}=-4.18$, i.e. $\omega_{osc}=\boxed{2.05\ \text{rad/s}}$ — exactly the Bode phase-crossover and the root-locus $j\omega$ crossing.
QuantityResult
Stable range (figures)$K_p\gt6.4$ (from $16.1$ dB above $K_p=1$)
Stable range (Routh)$\boxed{K_p\gt6.36}$
$\omega_{osc}$ at the boundary$2.05$ rad/s (all three methods agree)