Question 1 of 6: Unity-feedback system — real-pole range, step response, steady-state error
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper: National Exams — May 2013 · 07-Mec-A3 System Analysis and Controls · 3 hours · closed book (Casio/Sharp calculator + semi-log graph paper only) · any four of six questions constitute a complete paper; all questions of equal value. All six questions are solved here as a study resource.
Reference texts (subject). K. Ogata, Modern Control Engineering, 5th ed. (root locus Ch. 6, frequency response/Bode Ch. 7, steady-state error §5.8, Routh–Hurwitz §5.6); N. S. Nise, Control Systems Engineering, 8th ed.; R. C. Dorf & R. H. Bishop, Modern Control Systems, 13th ed.; G. F. Franklin, J. D. Powell & A. Emami-Naeini, Feedback Control of Dynamic Systems, 7th ed. Laplace-transform pairs are supplied with the exam.
The plant is an undamped second-order term ($s^{2}+25$, poles at $\pm j5$) with a real open-loop zero at $s=-12$.
Find. (i) the closed-loop denominator; (ii) the range of $K$ for which the closed-loop poles are real; (iii) with $K=24$, the closed-loop unit-step response $c(t)$ and the steady-state error $e_{ss}$ following a step.
Closed-loop unit-step response for $K=24$. The response is under-damped ($\zeta\approx0.68$), overshoots, and settles to $c(\infty)=0.920$; the gap to the input value of $1$ is the steady-state error $e_{ss}=0.080$.
Approach. Form $1+G(s)H(s)=0$ to get the characteristic polynomial, apply the discriminant test for real roots, then invert $C(s)=T(s)/s$ by partial fractions and read $e_{ss}$ from the position error constant.
Closed-loop denominator. For unity feedback the closed-loop transfer function is $T(s)=G/(1+G)$, whose denominator is the numerator of $1+G$:
$$1+G(s)=\frac{(s^{2}+25)+K(s+12)}{s^{2}+25}\;\Longrightarrow\; \boxed{\,D(s)=s^{2}+K\,s+(25+12K)\,}.$$
The loop turns the marginally-stable plant into a genuine second-order system with adjustable damping $Ks$ and stiffness $25+12K$.
Range of $K$ for real poles. The two poles are real when the discriminant of $D(s)$ is non-negative:
$$K^{2}-4(25+12K)\ge 0\;\Longrightarrow\;K^{2}-48K-100\ge0\;\Longrightarrow\;(K-50)(K+2)\ge0.$$
Hence $K\le-2$ or $K\ge 50$. For a physical positive gain the poles are real (and equal at the boundary) for
$$\boxed{\,K\ge 50\,}\qquad(\text{repeated real pole exactly at }K=50).$$
For $0<K<50$ the closed-loop poles are complex conjugates.
Pole location at $K=24$. With $K=24$, $D(s)=s^{2}+24s+313$, so
$$s=\frac{-24\pm\sqrt{24^{2}-4(313)}}{2}=-12\pm j13,\qquad \omega_n=\sqrt{313}=17.69\ \text{rad/s},\ \ \zeta=\frac{12}{\omega_n}=0.678.$$
Since $24<50$ the poles are complex, as expected — the response will be under-damped.
Unit-step response. The closed-loop transfer function is $T(s)=\dfrac{24(s+12)}{s^{2}+24s+313}$; for a unit step $R(s)=1/s$,
$$C(s)=\frac{24(s+12)}{s\,(s^{2}+24s+313)}=\frac{A}{s}+\frac{B\,s+D}{s^{2}+24s+313}.$$
Matching coefficients gives $A=\dfrac{24\cdot12}{313}=0.9201$, $B=-A=-0.9201$, $D=24(1-A)=1.917$. Completing the square $s^{2}+24s+313=(s+12)^{2}+13^{2}$ and rewriting the numerator about $(s+12)$,
$$\boxed{\,c(t)=0.920+e^{-12t}\!\left[-0.920\cos 13t+0.997\sin 13t\right]\,},\qquad t\ge0.$$
The transient decays with time constant $1/12\approx0.083$ s; the ringing frequency is $13$ rad/s.
Steady-state error to a step. This is a type-0 loop (no free integrator), so the static position error constant is finite:
$$K_p=\lim_{s\to0}G(s)=\frac{24\cdot12}{25}=11.52,\qquad e_{ss}=\frac{1}{1+K_p}=\frac{1}{12.52}=\boxed{0.0799}.$$
Equivalently the response settles to $c(\infty)=T(0)=288/313=0.920$, and $e_{ss}=1-c(\infty)=0.080$ — the two routes agree.