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22-Elec-A2 Systems and Control · May 2015

Question 3 of 8: Top-down controller design by pole matching

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 3 — Top-down controller design by pole matching [7 + 5 + 8]

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. $G(s)=\dfrac{10}{s(s+2)}$ (one free integrator $\Rightarrow$ Type 1, so a step error of 0 is automatic); $G_c(s)=\dfrac{a_1s+a_0}{b_1s+1}$.

Find. $G_{cl}(s)$ and $Q(s)$; the desired cubic; and $a_1,a_0,b_1$.

Part 1 — Closed-loop transfer function [7]

  1. Forward path. $G_cG=\dfrac{10(a_1s+a_0)}{(b_1s+1)\,s(s+2)}$.
  2. Close the unity loop. $G_{cl}=\dfrac{G_cG}{1+G_cG}=\dfrac{10(a_1s+a_0)}{(b_1s+1)s(s+2)+10(a_1s+a_0)}$.
  3. Characteristic equation. Expanding the denominator,$$Q(s)=b_1s^3+(2b_1+1)s^2+(2+10a_1)s+10a_0=0.$$

Part 2 — Desired characteristic equation [5]

  1. Dominant damping. $PO=5\%\Rightarrow\zeta=0.690$.
  2. Dominant natural frequency. $T_{settle}=\dfrac{4}{\zeta\omega_n}=4$ s $\Rightarrow\zeta\omega_n=1$, so $\omega_n=\dfrac{1}{0.690}=1.449$ rad/s ($\omega_n^2=2.10$). Dominant pair: $-1\pm j1.05$.
  3. Third pole. Ten times farther left than the dominant real part ($-1$): $s=-10$.
  4. Desired cubic. $(s^2+2s+2.10)(s+10)$:$$Q_{des}(s)=s^3+12s^2+22.1s+21=0.$$ (The Type-1 plant already gives $e_{ss}(\text{step})=0$.)

Part 3 — Matching and controller identification [8]

Approach. Divide $Q(s)$ by $b_1$ to make it monic, then equate coefficients with $Q_{des}$.

  1. $s^2$ coefficient. $\dfrac{2b_1+1}{b_1}=12\Rightarrow2+\dfrac1{b_1}=12\Rightarrow\boxed{b_1=0.1}$.
  2. $s^0$ coefficient. $\dfrac{10a_0}{b_1}=21\Rightarrow10a_0=2.1\Rightarrow\boxed{a_0=0.21}$.
  3. $s^1$ coefficient. $\dfrac{2+10a_1}{b_1}=22.1\Rightarrow2+10a_1=2.21\Rightarrow\boxed{a_1=0.021}$.
  4. Controller nature. The zero is at $-a_0/a_1=-10$ and the pole at $-1/b_1=-10$ — they coincide. Hence $G_c(s)=\dfrac{0.021(s+10)}{0.1(s+10)}=0.21$: the compensator collapses to a $\boxed{\text{pure Proportional controller, }K_p=0.21}$. Structurally it is the degenerate limit of a lead/lag network (pole/zero ratio = 1); the controller pole supplies the desired third pole at $-10$ while its zero cancels it, leaving a clean second-order dominant response.
Check: the third pole never appears. Because the compensator zero cancels its pole at $-10$, the realised closed loop is exactly $G_{cl}(s)=\dfrac{2.1}{s^2+2s+2.1}$ — second order, DC gain 1, poles $-1\pm j1.05$. This is the ideal outcome (no lingering third pole), which is why a plain proportional gain meets all three specifications here.
QuantityResult
$Q(s)$$b_1s^3+(2b_1+1)s^2+(2+10a_1)s+10a_0$
Desired cubic$s^3+12s^2+22.1s+21$
$b_1$ / $a_0$ / $a_1$$0.1$ / $0.21$ / $0.021$
Controller$G_c=0.21$ (pure P; pole–zero cancel at $-10$)