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22-Elec-A2 Systems and Control · December 2013

Question 4 of 7: PD vs. proportional-plus-rate-feedback control

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 2013, 3 hours, closed book (approved calculator plus one signed 8.5 × 11" formula sheet). Questions 1 and 2 are compulsory; answer three of the remaining five (Q3–Q7). Each question is worth 20 marks. All seven are worked below so the set is complete.

Reference texts: N. S. Nise, Control Systems Engineering (7th ed., Wiley) — root locus (Ch. 8), frequency response / Bode and gain–phase margins (Ch. 10), stability and Routh–Hurwitz (Ch. 6), PID and cascade lead/lag compensation (Ch. 9–11), steady-state error and error constants (Ch. 7), state space and canonical forms (Ch. 3, 12); K. Ogata, Modern Control Engineering (5th ed., Prentice Hall) — companion treatment of dominant-poles modelling, lead design and controllability; G. F. Franklin, J. D. Powell & A. Emami-Naeini, Feedback Control of Dynamic Systems. All block diagrams, pole–zero maps, root loci and Bode plots below are redrawn as inline figures.

Reading the exam figures. Two questions supply printed plots: Q1 gives an open-loop Bode plot (used for the gain-margin reading) and Q6 Part B gives a measured step-response curve (used to read $K_{dc},\zeta,\omega_n$). The transfer functions are given exactly in the question text, so every reading below is also confirmed analytically (Bode by direct evaluation, stability by Routh–Hurwitz). Where the printed plot annotation and the exact model differ slightly, the exact model governs.

Question 4 — PD vs. proportional-plus-rate-feedback control [8 + 4 + 8]

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. Plant $\dfrac{30}{s^2+10s+5}$; specs $e_{ss}=5\%$, $\zeta=0.7$.

Find. $G_{cl1}$ and $K_p,T_d$ (A); step-response specs (B); $G_{cl2}$ and comparison (C).

[Figure not reproduced: Figure Q4.1 (redrawn) — forward gain $K_p$ with inner rate ($T_d s$) feedback added to the unity output feedback, so the feedback transfer function is $1+T_d s$. See the official exam paper.]

Part A — Rate-feedback closed loop and controller sizing [8]

Approach. The rate path makes the feedback $H(s)=1+T_d s$; form $G_{cl1}=K_pG/(1+K_pGH)$ and match the resulting second-order denominator to the $e_{ss}$ and $\zeta$ specs.

  1. Closed-loop transfer function. With forward $K_p\cdot\dfrac{30}{s^2+10s+5}$ and feedback $1+T_d s$, $$G_{cl1}(s)=\frac{30K_p}{s^2+(10+30K_pT_d)s+(5+30K_p)}.$$
  2. Stability restrictions. For a second-order denominator, stability needs both middle and constant coefficients positive: $5+30K_p\gt0$ and $10+30K_pT_d\gt0$, i.e. $K_p\gt0$ and $T_d\gt-\dfrac{1}{3K_p}$ — any $K_p\gt0,\ T_d\ge0$ is safe.
  3. Gain from steady-state error. $e_{ss}=1-G_{cl1}(0)=\dfrac{5}{5+30K_p}=0.05\Rightarrow 5+30K_p=100\Rightarrow \boxed{K_p=3.17}$, giving $\omega_n^2=5+30K_p=100$, $\omega_n=10$ rad/s.
  4. Rate gain from damping. $2\zeta\omega_n=10+30K_pT_d\Rightarrow 14=10+95T_d\Rightarrow \boxed{T_d=0.0421\ \text{s}}.$
  5. Numerical closed loop. $$G_{cl1}(s)=\frac{95}{s^2+14s+100}.$$

Part B — Step-response specifications of $G_{cl1}$ [4]

Approach. Read the specs directly from $\zeta=0.7$, $\omega_n=10$.

  1. Percent overshoot. $\text{PO}=e^{-\zeta\pi/\sqrt{1-\zeta^2}}\times100=e^{-2.199/0.714}\times100=\boxed{4.6\%}.$
  2. Settling time. $T_{s(\pm2\%)}=\dfrac{4}{\zeta\omega_n}=\dfrac{4}{7}=\boxed{0.57\ \text{s}}.$
  3. Steady-state error. $e_{ss}=\boxed{5\%}$ by design (DC gain $0.95$).

Part C — PD control and comparison [8]

[Figure not reproduced: Figure Q4.2 (redrawn) — the same plant under forward PD control $K_p(T_d s+1)$ with plain unity feedback. See the official exam paper.]

Approach. The forward PD zero enters the numerator while the denominator is unchanged; compare the two closed loops term by term.

  1. PD closed loop. $G_{cl2}(s)=\dfrac{30K_p(T_d s+1)}{s^2+(10+30K_pT_d)s+(5+30K_p)}$; with the same $K_p,T_d$ $$G_{cl2}(s)=\frac{95(0.0421s+1)}{s^2+14s+100}=\frac{4.0s+95}{s^2+14s+100}.$$
  2. The difference. $G_{cl1}$ and $G_{cl2}$ share the identical denominator (same poles, same $\zeta=0.7$, $\omega_n=10$); $G_{cl2}$ adds a finite zero at $s=-1/T_d=-23.75$.
  3. Effect on the Part-B specs. $e_{ss}$: unchanged ($G_{cl2}(0)=95/100=0.95$, so $e_{ss}=5\%$). PO: the extra LHP zero raises the overshoot well above $4.6\%$ (the derivative kick), and gives a faster rise/peak time. $T_s$: governed by the same $\zeta\omega_n=7$, so the $\pm2\%$ envelope is essentially the same. In short, rate feedback (Q4.1) avoids the numerator zero and keeps the clean, low-overshoot response, whereas forward PD (Q4.2) is faster but more oscillatory for identical gains.
QuantityResult
$K_p,\ T_d$$3.17,\ 0.0421$ s
$G_{cl1}$ (rate feedback)$\dfrac{95}{s^2+14s+100}$
PO, $T_s$, $e_{ss}$$4.6\%,\ 0.57$ s, $5\%$
$G_{cl2}$ (PD)$\dfrac{4.0s+95}{s^2+14s+100}$
DifferencePD adds zero at $-23.75$ → higher PO, same poles/$e_{ss}$