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22-Elec-A2 Systems and Control · May 2015

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]

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

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.

  1. DC gain for the error spec. $K_{pos,c}=G_c(0)\,G(0)=a_0(10)=49\Rightarrow\boxed{a_0=4.9}$.
  2. 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.
  3. 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 $$\boxed{a_1=2.59,\qquad b_1=9.80.}$$
  4. 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).
Open loop: uncompensated (blue) vs lag-compensated (red)-100-80-60-40-20020Magnitude (dB)-225-180-135-90-45010^-210^-110^010^110^210^3Phase (deg)Frequency (rad/s)ω_pc=4.00
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 compensator: pole -0.10, zero -1.890ReIm
Lag pole–zero: pole $-0.10$ inside, zero $-1.89$ outside.

Part 2 — Compensated step estimates [5]

  1. Damping. $\zeta\approx\dfrac{\Phi_m}{100}=0.45$ (or exactly $0.456$).
  2. Overshoot. $PO=100\,e^{-\zeta\pi/\sqrt{1-\zeta^2}}\approx\boxed{20\%}$.
  3. Settling time. Taking $\omega_n\approx\omega_{cp}=4$ rad/s, $T_{settle}(\pm2\%)=\dfrac{4}{\zeta\omega_n}\approx\dfrac{4}{0.45(4)}=\boxed{2.2\ \text{s}}$.
  4. Steady-state error. By construction $e_{ss}=\dfrac{1}{1+K_{pos,c}}=\dfrac{1}{50}=\boxed{2\%}$.
QuantityUncompensatedCompensated
$K_{pos}$ / $e_{ss}$$10$ / $9.1\%$$49$ / $2\%$
$\Phi_m$ / $\omega_{cp}$$23.5^\circ$ / $8.83$$45^\circ$ / $4$ rad/s
$PO$ / $T_{settle}$$\approx58\%$ / —$\approx20\%$ / $2.2$ s
Controller$G_c(s)=\dfrac{2.59s+4.9}{9.80s+1}$ (lag)