Question 4 of 8: Second-order dominant-pole models
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 2016, 3 hours, closed book (approved Casio/Sharp calculator plus one signed, double-sided 8.5 × 11" formula sheet; a Laplace-transform table and the standard ζ–overshoot and ζ–resonant-peak design plots are supplied). Questions 1 and 2 are compulsory; a complete paper is five questions, so a candidate chooses 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) — Routh–Hurwitz (Ch. 6), root locus (Ch. 8), steady-state error and static error constants (Ch. 7), frequency response, Bode, Nyquist, gain/phase margins (Ch. 10), lead–lag and PID design (Ch. 9–11), state space and Mason’s rule (Ch. 3, 5); K. Ogata, Modern Control Engineering (5th ed., Prentice Hall) — dominant-poles modelling and second-order correlations. All block diagrams, root loci, pole–zero maps, Bode sketches, Nyquist plots and the realization diagrams below are redrawn as inline figures.
Reading the supplied design charts. The percent-overshoot chart uses $PO=100\,e^{-\zeta\pi/\sqrt{1-\zeta^2}}$ and the second-order model is $G_m(s)=K_{dc}\,\dfrac{\omega_n^2}{s^2+2\zeta\omega_n s+\omega_n^2}$. Questions 4, 6 and 7 are read from printed Bode/response plots, so those values carry normal chart-reading tolerance; the s-domain results (Q1, Q2, Q3, Q5, Q8) are exact.
Figure Q4.1 — unity-feedback loop, process $150/[s(s^3+15s^2+62s+72)]$.
Item (1) — dominant-pole model $G_{m1}$
Given. factored closed-loop poles $-8.35,\,-6.07$ and the pair $-0.29\pm j1.70$. Find. the appropriate second-order model.
$G_{cl}$ pole map: the pair $-0.29\pm j1.70$ lies $\sim21\times$ closer to the jw-axis than the real poles $-6.07,-8.35$, so it dominates the response.
Identify the dominant pair. Real part of the pair is $-0.29$; the real poles at $-6.07,-8.35$ are more than $20\times$ further left, so they decay far faster and are negligible. Keep the pair $s^2+0.58s+2.96$.
Match DC gain. $G_{cl}(0)=150/150=1$, so scale the numerator to keep unity DC gain: $$\boxed{G_{m1}(s)=\frac{2.96}{s^2+0.58s+2.96}}.$$
Items (2)–(3) — models from the frequency responses
[Figure not reproduced: Figure Q4.2 redrawn. Closed loop (dashed) is flat at $0$ dB with a resonant peak $\approx9$ dB near $\omega_r\approx1.67$; open loop (solid) rises at low $\omega$ (integrator) and crosses $0$ dB at $\omega_{cp}\approx1.53$. See the official exam paper.]
$G_{m2}$ from the open-loop response. Read gain crossover $\omega_{cp}\approx1.53$ rad/s and phase margin $\Phi_m\approx22^\circ$. Using $\zeta\approx\Phi_m/100=0.22$ and $\omega_n=\omega_{cp}/\sqrt{\sqrt{1+4\zeta^4}-2\zeta^2}\approx1.60$: $$G_{m2}(s)=\frac{2.57}{s^2+0.71s+2.57},\quad \zeta_2=0.22,\ \omega_{n2}=1.60.$$
$G_{m3}$ from the closed-loop response. Read resonant peak $M_r\approx9.1$ dB $=2.85$ at $\omega_r\approx1.67$. From $M_r=\dfrac{1}{2\zeta\sqrt{1-\zeta^2}}$ get $\zeta_3\approx0.178$, and $\omega_{n3}=\dfrac{\omega_r}{\sqrt{1-2\zeta^2}}\approx1.72$: $$G_{m3}(s)=\frac{2.96}{s^2+0.61s+2.96},\quad \zeta_3=0.178,\ \omega_{n3}=1.72.$$
Contrast. $G_{m1}$ and $G_{m3}$ nearly coincide ($\omega_n=1.72$, $\zeta\approx0.17$) because the closed-loop resonance is set by the same dominant pair. $G_{m2}$ (from the open-loop margin) gives a slightly higher damping ($\zeta=0.22$) and lower $\omega_n$, because the phase-margin correlation is only approximate and the two neglected real poles still bleed a little phase near crossover. All three predict a lightly-damped, oscillatory step response of comparable speed.
Model
$\omega_n$
$\zeta$
Source
$G_{m1}$
1.72
0.169
s-domain dominant pair
$G_{m2}$
1.60
0.22
open-loop $\Phi_m,\omega_{cp}$
$G_{m3}$
1.72
0.178
closed-loop $M_r,\omega_r$
Check: $G_{m2}$ and $G_{m3}$ rest on graphical reads ($\omega_{cp},\Phi_m,M_r,\omega_r$) from Figure Q4.2; the numbers above are the exact model values the printed curves correspond to, quoted to chart-reading tolerance.