Question 4 of 8: Second-order dominant model, system type, transient specs, effect of a zero
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 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 the standard ζ–overshoot / ζ–resonant-peak design plots are supplied). 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 canonical forms (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, the Nyquist plot, the network schematic and the signal-flow graph below are redrawn as inline figures.
Reading the exam figures. Every transfer function in this paper is stated exactly, so every boxed result is confirmed analytically and the exact model governs. Q2 supplies a Bode plot ($G_m=32.2$ dB at $3.9$ rad/s, $P_m=-145^\circ$ at $0.324$ rad/s) and a root locus, and Q7 supplies the uncompensated Bode plot; values read from those curves are flagged as reads and cross-checked against the Routh/analytic results.
Question 4 — Second-order dominant model, system type, transient specs, effect of a zero [5 + 5 + 5 + 5]
Given. The pole closest to the imaginary axis dominates.
Poles
Zero
$K$
Dominant pair
$-1\pm j4,\ -15,\ -20\pm j2$
$-20$
$5000$
$-1\pm j4$
Find. $(\zeta,\omega_n,K_{dc})$; system type and errors; step specs; and the effect of moving the zero to $-2$.
Pole–zero map: only $-1\pm j4$ sits near the imaginary axis; $-15$ and $-20\pm j2$ are $\ge15\times$ farther out and the zero at $-20$ is remote, so the pair dominates.
Part 1 — Dominant second-order model [5]
Dominant pair. $-1\pm j4$ gives $\omega_n=\sqrt{1^2+4^2}=\sqrt{17}=\boxed{4.123\ \text{rad/s}}$ and $\zeta=\dfrac{1}{\omega_n}=\dfrac{1}{4.123}=\boxed{0.2425}$ (the quadratic factor is $s^2+2s+17$).
DC gain. $K_{dc}=G(0)=\dfrac{5000(20)}{(17)(15)(404)}=\dfrac{100000}{103020}=\boxed{0.9707}$, where $|{-1\pm j4}|^2=17$, $|{-20\pm j2}|^2=404$.
Model. Preserving the DC gain, $$G_m(s)=0.9707\cdot\frac{17}{s^2+2s+17}=\boxed{\frac{16.5}{s^2+2s+17}}.$$
Part 2 — System type and steady-state errors [5]
System Type. $G(s)$ has no pole at the origin, so it is $\boxed{\text{Type 0}}$.
Step error. $K_{pos}=G(0)=0.9707$, so $e_{ss(step)}=\dfrac{1}{1+K_{pos}}=\dfrac{1}{1.9707}=\boxed{50.7\%}$.
Ramp error. $K_v=\lim_{s\to0}sG(s)=0$ for a Type-0 system, so $e_{ss(ramp)}=\dfrac{1}{K_v}=\boxed{\infty}$ (the output cannot track a ramp).
Settling time. The dominant real part is $\zeta\omega_n=1$, so $T_{settle}(\pm2\%)=\dfrac{4}{\zeta\omega_n}=\dfrac{4}{1}=\boxed{4.0\ \text{s}}$.
Part 4 — Effect of moving the zero to $-2$ [5]
The original zero at $-20$ is remote ($20\gg5\zeta\omega_n=5$), so it barely alters the dominant response — that is why the pure second-order model is valid. Moving it to $-2$ places it close to the dominant poles (its magnitude $2$ is only twice the dominant real part $1$, well inside the “$\ge5\times$” negligibility rule), so it strongly reshapes the response:
Overshoot rises sharply. A left-half-plane zero adds a derivative-like term to the response; near the poles it injects a large early transient. A numerical step simulation of the second-order model with the zero gives $PO\approx132\%$, up from $\approx46\%$ — roughly a threefold increase.
Faster rise, similar settling. The zero speeds up the initial rise (shorter rise/peak time), but the decay envelope is still set by the unchanged pole real part ($e^{-t}$), so $T_{settle}$ stays near $4$ s (marginally longer because the larger overshoot must decay).
DC gain and error worsen. The DC gain drops by the factor $\tfrac{2}{20}=\tfrac{1}{10}$ to $K_{dc}=0.0971$, so $K_{pos}=0.0971$ and $e_{ss(step)}=\dfrac{1}{1.0971}=91.2\%$ — far worse steady-state accuracy.
Quantity
Zero at $-20$
Zero at $-2$
$K_{dc}$ / $e_{ss(step)}$
$0.971$ / $50.7\%$
$0.097$ / $91.2\%$
$PO$ (step)
$\approx46\%$
$\approx132\%$
$T_{settle}(\pm2\%)$
$4.0$ s
$\approx4$ s (slightly longer)
$\zeta,\omega_n$
unchanged ($0.243$, $4.12$ rad/s) — poles do not move