Question 6 of 6: Effect of Loop Gain on Step Response and Steady-State Error
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. 07-Mec-A3 System Analysis and Control,
National Exams May 2015 — 3 hours, closed book (approved Casio or
Sharp calculator and semi-log graph paper only). Six questions; the paper instructs that
"any four questions constitute a complete paper" and that all questions are of equal
value, so each question is worth 25 marks. All six are solved here. A Laplace-transform table
is supplied with the paper (pages 5–6).
Reference texts. K. Ogata, Modern Control Engineering, 5th ed.
(Pearson) — Ch. 5 (transient response), Ch. 6 (root locus), Ch. 7 (frequency
response); N. S. Nise, Control Systems Engineering, 8th ed. (Wiley) — Ch. 4,
6, 8, 10; R. C. Dorf and R. H. Bishop, Modern Control Systems, 13th ed.
(Pearson); G. F. Franklin, J. D. Powell and A. Emami-Naeini, Feedback Control of
Dynamic Systems, 8th ed. (Pearson).
Question 6: Effect of Loop Gain on Step Response and Steady-State Error (25 marks)
Given. Unity-feedback loop of Fig. 3 with forward gain $K$ and
plant $G(s)=\dfrac{1}{(s+2)(s+10)}$; unit-step input; two gain settings, $K = 7$ and
$K = 20$.
Find. (a) the closed-loop step responses $c(t)$ at both gains;
(b) the steady-state errors, verified both from the time responses and from the static
error constant; (c) a comparison of settling time and response character.
Figure 3 — unity-feedback loop with adjustable forward gain $K$ and plant $G(s)=1/[(s+2)(s+10)]$.
Approach. Form the closed-loop transfer function once in terms of
$K$, factor its denominator at each gain, invert by partial fractions, then check each
final value against $e_{ss}=1/(1+K_p)$ and compare the dominant time constants.
Form the closed-loop transfer function. With unity feedback,
$$\frac{C(s)}{R(s)}=\frac{KG(s)}{1+KG(s)}=\frac{K}{(s+2)(s+10)+K}
=\frac{K}{s^2+12s+(20+K)}$$
The damping term $12s$ is fixed by the plant; only the constant term moves with $K$, so
raising the gain raises $\omega_n=\sqrt{20+K}$ and lowers
$\zeta = 6/\sqrt{20+K}$.
Case $K = 7$: factor and invert. The denominator becomes
$s^2+12s+27=(s+3)(s+9)$ — two real poles, so the response is overdamped. With
$C(s)=7/[s(s+3)(s+9)]$ the residues are $7/27$, $-7/18$ and $7/54$, giving
$$\boxed{c_1(t)=\frac{7}{27}-\frac{7}{18}e^{-3t}+\frac{7}{54}e^{-9t}}$$
The coefficients sum to zero at $t = 0$ as required, and
$c_1(\infty)=7/27=0.2593$.
Case $K = 20$: factor and invert. Now
$s^2+12s+40$, whose roots are $s=-6\pm j2$: complex, so the response is underdamped with
$\omega_n=\sqrt{40}=6.325\ \text{rad/s}$ and $\zeta = 6/6.325 = 0.949$. Expanding
$C(s)=20/[s(s^2+12s+40)]$ as $0.5/s + (Bs+D)/(s^2+12s+40)$ gives $B=-0.5$, $D=-6$, and
completing the square as $(s+6)^2+2^2$ yields
$$\boxed{c_2(t)=0.5-e^{-6t}\left(0.5\cos 2t+1.5\sin 2t\right)}$$
with $c_2(0)=0$ and $c_2(\infty)=0.5$.
Question 6(a): computed unit-step responses at $K=7$ (overdamped, final value 0.2593) and $K=20$ (lightly underdamped, final value 0.5000).
Part (b): verify the errors directly from the responses. Because
$E = R - C$ and $R$ is a unit step, the steady-state error is simply
$1-c(\infty)$:
$$e_{ss}\big|_{K=7}=1-\frac{7}{27}=\frac{20}{27}=0.7407,\qquad
e_{ss}\big|_{K=20}=1-0.5=0.5000$$
Part (b): confirm against the static error constant. The loop is type
0, with
$$K_p=\lim_{s\to0}\frac{K}{(s+2)(s+10)}=\frac{K}{20}$$
so $K_p = 0.35$ at $K=7$ and $K_p = 1.0$ at $K=20$, giving
$$\frac{1}{1+0.35}=0.7407,\qquad \frac{1}{1+1.0}=0.5000$$
Both agree exactly with the time-domain values, which is the "direct verification" the
question asks for. Note that even at $K = 20$ the error is still 50 % — a type-0
loop cannot be made accurate by gain alone without eventually destroying its damping.
Part (c): compare settling times. At $K=7$ the dominant pole is
$s=-3$, so the $2\ \%$ settling time is approximately $4/3 = 1.33\ \text{s}$; evaluating
the exact response gives $1.44\ \text{s}$. At $K=20$ both poles have real part $-6$,
giving $4/6 = 0.67\ \text{s}$ by the envelope estimate and $0.83\ \text{s}$ exactly (the
sine term inflates the envelope slightly). The higher gain therefore settles about
1.7 times faster.
Part (c): compare the nature of the responses. At $K=7$ the poles are
real and distinct, so the response rises monotonically to $0.2593$ with no overshoot and no
oscillation. At $K=20$ the poles are complex with $\zeta = 0.949$; the response is
nominally underdamped but so heavily damped that its overshoot is only
$M_p = e^{-\pi\zeta/\sqrt{1-\zeta^2}} = 0.008\ \%$ — a peak of $0.50004$ at
$t = \pi/2\ \text{s}$, entirely invisible in practice. In summary, raising $K$ from 7 to
20 halves the steady-state error, nearly halves the settling time, and moves the system
from overdamped to just inside the underdamped region without producing any practically
significant overshoot. Continuing past $K=20$ would keep improving accuracy and speed of
response only until the overshoot became objectionable; since $\zeta$ falls as
$6/\sqrt{20+K}$, a common design limit of $\zeta = 0.7$ would already be reached at
$K \approx 53$.