Question 3 of 8: Second-order dominant-pole models three ways
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, 07-Elec-A2 Systems & Control, December 2014, 3 hours, closed book (approved Casio/Sharp calculator plus one signed, double-sided 8.5 × 11" formula sheet). 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 specs (Ch. 4), Routh–Hurwitz stability (Ch. 6), steady-state error and error constants (Ch. 7), root locus (Ch. 8), PID and 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 rule; G. F. Franklin, J. D. Powell & A. Emami-Naeini, Feedback Control of Dynamic Systems. All block diagrams, pole–zero maps, root loci, Bode plots and signal-flow graphs below are redrawn as inline figures.
Reading the exam figures. Q1 supplies open- and closed-loop Bode plots and Q6 supplies uncompensated/compensated open-loop Bode plots. Where a transfer function is stated exactly in the text, every graphical reading is also confirmed analytically and the exact model governs; where only a plot is given (Q6), the values are read from the printed curves and flagged as such.
Given. Closed-loop $T(s)=\dfrac{100}{s^3+10s^2+25s+100}$, $T(0)=1$; the factored poles above; from Q1 the open-loop margins ($\text{PM}=28.7^\circ$, $\omega_{cp}=2.96$ rad/s); from Figure Q1.3 a resonant peak $M_r\approx2.15$ at $\omega_r\approx4$ rad/s.
Find. $G_{m1},G_{m2},G_{m3}$ and the step-response specs from the most accurate model.
Closed-loop poles: the complex pair at $-0.78\pm j3.35$ sits $10.8\times$ nearer the axis than the real pole at $-8.44$ — strong dominance.
Part 1 — $G_{m1}$ from pole locations [5]
Dominance test. $|\mathrm{Re}\,p_3|/|\mathrm{Re}\,p_{1,2}| =8.44/0.779=10.8\gt5$, so the complex pair dominates and a 2nd-order model is valid.
Model parameters. $\omega_n=|p_{1,2}|=\sqrt{0.779^2+3.352^2}=\boxed{3.442\ \text{rad/s}}$; $\zeta=\dfrac{0.779}{3.442}=\boxed{0.226}$. Preserving $T(0)=1$, $$G_{m1}(s)=\frac{11.85}{s^2+1.558s+11.85}.$$
Part 2 — $G_{m2}$ from the open-loop Bode plot [5]
Damping from PM. Inverting $\text{PM}=\arctan\dfrac{2\zeta}{\sqrt{\sqrt{1+4\zeta^4}-2\zeta^2}}$ at $\text{PM}=28.7^\circ$ gives $\boxed{\zeta\approx0.257}$.
Natural frequency from $\omega_{cp}$. $\omega_{cp}=\omega_n\sqrt{\sqrt{1+4\zeta^4}-2\zeta^2}$ with $\omega_{cp}=2.96$ gives $\omega_n\approx3.16$ rad/s, so $$G_{m2}(s)=\frac{9.99}{s^2+1.62s+9.99}.$$
Part 3 — $G_{m3}$ from the closed-loop Bode plot [5]
Damping from the resonant peak. $M_r=\dfrac{1}{2\zeta\sqrt{1-\zeta^2}}=2.15\Rightarrow\boxed{\zeta\approx0.240}$.
Natural frequency from $\omega_r$. $\omega_r=\omega_n\sqrt{1-2\zeta^2}=4$ gives $\omega_n\approx4.25$ rad/s, so $$G_{m3}(s)=\frac{18.1}{s^2+2.04s+18.1}.$$
Part 4 — Comparison & step specifications [5]
Approach. $G_{m1}$ is built from the exact poles, so it is the reference; $G_{m2}$ and $G_{m3}$ agree on $\zeta\approx0.24$–$0.26$ and $\omega_n\approx3.2$–$4.3$ — the graphical reads bracket the exact model. Use $G_{m1}$.
Step error. Type 1 loop with $T(0)=1\Rightarrow e_{ss(step\%)}=\boxed{0}$.
Rise time (0–100%). $T_r=\dfrac{\pi-\theta}{\omega_d}$ with $\theta=\arccos\zeta=76.9^\circ$ and $\omega_d=\omega_n\sqrt{1-\zeta^2}=3.35$ rad/s: $T_r=\dfrac{\pi-1.342}{3.35}=\boxed{0.537\ \text{s}}$.
Overshoot. $PO=100\,e^{-\zeta\pi/\sqrt{1-\zeta^2}}=100\,e^{-0.729}=\boxed{48\%}$ (large, because $\zeta$ is small).