Question 6 of 8: Lag-controller design in the frequency domain
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 6 — Lag-controller design in the frequency domain [15 + 5]
Given. Uncompensated Type 0, $K_{pos}=G(0)=10$; targets $e_{ss}=2\%\Rightarrow K_{pos,c}=49$, $\Phi_m=45^\circ$ at $\omega_{cp}=4$ rad/s. At $\omega=4$: $|G(j4)|=3.43$, $\angle G(j4)=-111.1^\circ$.
Find. $a_0,a_1,b_1$, $G_c(s)$, and the compensated step specs.
Part 1 — Lag-controller calculation [15]
Approach. The DC gain sets the error constant; the values at the target crossover ($|G_cG|=1$, $\angle G_cG=-135^\circ$) then fix the two time constants.
DC gain for the error spec. $K_{pos,c}=G_c(0)\,G(0)=a_0(10)=49\Rightarrow\boxed{a_0=4.9}$.
Requirements at $\omega_{cp}=4$. For $|G_cG(j4)|=1$ with $|G(j4)|=3.43$: $|G_c(j4)|=\dfrac{1}{3.43}=0.292$. For $\angle G_cG(j4)=-135^\circ$ (i.e. $PM=45^\circ$) with $\angle G(j4)=-111.1^\circ$: $\angle G_c(j4)=-23.9^\circ$ — a genuine lag contribution.
Solve for $a_1,b_1$. With $G_c(j4)=\dfrac{a_0+j4a_1}{1+j4b_1}$, imposing the magnitude and phase above gives $$\boxed{a_1=2.59,\qquad b_1=9.80.}$$
Controller. $$\boxed{G_c(s)=\frac{2.59\,s+4.9}{9.80\,s+1}}$$ — zero at $-a_0/a_1=-1.89$, pole at $-1/b_1=-0.102$. The pole is nearer the imaginary axis than the zero, confirming a lag network. DC gain $4.9$ (raises $K_{pos}$ to 49); high-frequency gain $a_1/b_1=0.264$ (the mid-band attenuation that pulls the crossover down to 4 rad/s).
Uncompensated (blue) vs lag-compensated (red) open loop: the lag lifts the low-frequency gain for the $2\%$ error while attenuating near crossover, moving $\omega_{cp}$ to $4$ rad/s with $45^\circ$ phase margin.
Lag pole–zero: pole $-0.10$ inside, zero $-1.89$ outside.