Question 7 of 8: Rate-Feedback vs. PD Control — Same $K_p,T_d$, Very Different Outcomes
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. 17-Phys-B5 Systems and Control, National Exams May 2018
— a three-hour closed-book examination with one double-sided handwritten formula/notes
sheet permitted and an approved calculator. Questions 1 and 2 are compulsory; candidates choose
three of the remaining six (3–8). Every question is nonetheless answered in full below so
the paper remains a complete study resource. All eight questions carry equal value (20 marks
each).
Reference texts. N. S. Nise, Control Systems Engineering, 7th ed.
(transient-response specifications, root locus, Routh–Hurwitz, frequency-response and lead
compensator design, state-space representation, steady-state errors); K. Ogata, Modern
Control Engineering, 5th ed. (root-locus and PID/rate-feedback compensator design,
controllability/observability, Mason's Gain Formula on signal-flow graphs).
Question 7: Rate-Feedback vs. PD Control — Same $K_p,T_d$, Very Different
Outcomes (20 marks)
Given. Process $30/(s^2+10s+5)$ in both configurations; Q7.1: rate-feedback
path $T_ds$ taps $Y(s)$ and is ADDED (per the source figure, flagged there as atypical) at the
second summing node; Q7.2: standard unity feedback with a PD controller $K_p(T_ds+1)$ acting on
the error.
Find. 1) $K_p,T_d$ for $PO=5\%,e_{ss(step)}=5\%$ in the Q7.1 configuration.
2) $G_{cl1}(s)$, $T_{settle}$. 3) $G_{cl2}(s)$ with the SAME $K_p,T_d$; compare.
Approach. Reduce Q7.1's block diagram to a standard 2nd-order closed-loop
form (proportional gain sets $\omega_n^2$ via the DC gain / step-error spec; rate feedback sets
$2\zeta\omega_n$), match to the $PO,e_{ss}$ specification, then reuse the SAME numeric $K_p,T_d$
in Q7.2's differently-structured loop and compare the resulting characteristic equations
directly.
Part 1) — solving for $K_p,T_d$. With $e=R-Y$ and
$u=K_pe+T_dsY$ (both added, as drawn), $Y=P(s)u\Rightarrow
Y=P(K_p(R-Y)+T_dsY)\Rightarrow Y[1+K_pP-T_dsP]=K_pPR$, giving
$$G_{cl1}(s)=\frac{30K_p}{s^2+(10-30T_d)s+(5+30K_p)}.$$
$PO=5\%\Rightarrow\zeta=-\ln(0.05)/\sqrt{\pi^2+\ln^2(0.05)}=\boxed{0.6901}$.
$e_{ss(step)}=1-G_{cl1}(0)=5/(5+30K_p)=0.05\Rightarrow 5+30K_p=100\Rightarrow
\boxed{K_p=95/30=19/6\approx3.167}$, which fixes $\omega_n^2=5+30K_p=100\Rightarrow\omega_n=10$.
Matching $2\zeta\omega_n=10-30T_d$: $\ 2(0.6901)(10)=13.80=10-30T_d\Rightarrow$
$$\boxed{T_d=\frac{10-13.80}{30}=-0.1267\ \text{s}}$$
(negative — a direct consequence of the source diagram's atypical ADDITION at the
rate-feedback node: reaching MORE damping than the $\zeta=0.5$ baseline the proportional-only
loop already gives ($2\zeta\omega_n=10$ at $T_d=0$) requires REDUCING the $s^1$ coefficient
below 10, which this diagram's sign convention needs a negative $T_d$ to do — physically
equivalent to a CONVENTIONAL (subtracting) rate-feedback gain of $+0.1267$.)
Part 2) — $G_{cl1}(s)$ and settling time. Substituting,
$$\boxed{G_{cl1}(s)=\frac{95}{s^2+13.80s+100}}$$
(poles at $-6.90\pm j7.24$, both stable), and
$$T_{settle(\pm2\%)}=\frac{4}{\zeta\omega_n}=\frac{4}{6.901}=\boxed{0.580\ \text{s}}.$$
Part 3) — SAME $K_p,T_d$ in the PD configuration. For Q7.2, the
derivative acts on the error itself: forward path $K_p(T_ds+1)\times30/(s^2+10s+5)$, giving
$$G_{cl2}(s)=\frac{30K_p(T_ds+1)}{s^2+(10+30K_pT_d)s+(5+30K_p)}
=\frac{30K_pT_d\,s+30K_p}{s^2+(10+30K_pT_d)s+100}.$$
With $30K_p=95$ and $T_d=-0.1267$: numerator $=-12.04s+95$; denominator
$s^1$-coefficient $=10+30K_pT_d=10+95(-0.1267)=10-12.04=\boxed{-2.04}$ — NEGATIVE, so
$$\boxed{G_{cl2}(s)=\frac{-12.04s+95}{s^2-2.04s+100}}$$
has poles at $+1.02\pm j9.95$ (verified directly): the closed loop is
UNSTABLE, unlike the well-behaved, stable $G_{cl1}(s)$ above. Why the same
numbers behave so differently: rate feedback (Q7.1) only ever enters the CHARACTERISTIC
EQUATION (no closed-loop zero is created, since $T_d$ acts on $Y$, not on the forward-path
signal reaching the output directly) — so a negative $T_d$ there simply reduces the
$s^1$ coefficient, and the design compensates by choosing it negative enough to reach the target
$\zeta$. PD control (Q7.2) instead applies $T_d$ to the ERROR: it both changes the SAME-LOOKING
$s^1$ coefficient (with the OPPOSITE sign convention, $+30K_pT_d$ instead of $-30T_d$) AND adds
a closed-loop ZERO at $s=-1/T_d=+7.89$ (a right-half-plane zero, since $T_d<0$). Reusing "the
same $K_p,T_d$" therefore flips a well-damped, stable rate-feedback design into an outright
unstable PD loop: $PO$ and settling time become meaningless (the step response diverges) rather
than merely worse, and the rise-time comparison is moot. This starkly illustrates that rate
(tachometer) feedback and PD control are NOT interchangeable just because they share the same
nominal "$K_p,T_d$" labels — the physical signal each gain multiplies (the output vs. the
error) fixes both the sign convention AND whether a closed-loop zero appears.
Final results — Question 7
Item
Result
$K_p$
$19/6\approx3.167$
$T_d$ (rate-feedback config.)
$-0.1267$ s
$G_{cl1}(s)$
$95/(s^2+13.80s+100)$, poles $-6.90\pm j7.24$ — STABLE
$T_{settle(\pm2\%)}$
$0.580$ s
$G_{cl2}(s)$ (PD, same $K_p,T_d$)
$(-12.04s+95)/(s^2-2.04s+100)$, poles
$+1.02\pm j9.95$ — UNSTABLE