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]
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.