About this set. These are original practice questions written
in GATE style for the 2020 Control Systems syllabus, with fully worked
solutions. They are not reproductions of the official 2020 question paper.
Question 01 · 1 MarkQuestion 1
In a control system the error signal \(E(s) = R(s) - C(s)\) drives a block \(G_1(s) = \dfrac{5}{s+3}\). The output of \(G_1\) drives a second block \(G_2(s) = \dfrac{2}{s}\), and the output of \(G_2\) is the system output \(C(s)\). An inner negative feedback path of constant gain \(H_1 = 4\) is taken from the output of \(G_2\) back to the summing junction placed just before \(G_2\). The overall transfer function \(C(s)/R(s)\) is
- \(\dfrac{10}{s^2 + 11s + 34}\)
- \(\dfrac{10}{s^2 + 11s + 24}\)
- \(\dfrac{10}{s^2 + 3s + 10}\)
- \(\dfrac{10}{s^2 + 8s + 34}\)
Solution
Reduce the inner loop first (see Chapter 4). For a negative feedback loop of forward gain \(G_2\) and feedback gain \(H_1\):
Equation
\[G_{inner}(s) = \frac{G_2}{1 + G_2 H_1} = \frac{2/s}{1 + (2/s)(4)} = \frac{2/s}{(s+8)/s} = \frac{2}{s+8}\]
The inner block is now in cascade with \(G_1\):
Equation
\[G_{fwd}(s) = \frac{5}{s+3} \times \frac{2}{s+8} = \frac{10}{(s+3)(s+8)}\]
Closing the outer unity negative feedback loop:
Equation
\[\frac{C(s)}{R(s)} = \frac{G_{fwd}}{1 + G_{fwd}} = \frac{10}{(s+3)(s+8) + 10} = \frac{10}{s^2 + 11s + 24 + 10}\]
Equation
\[\frac{C(s)}{R(s)} = \frac{10}{s^2 + 11s + 34}\]
A
Final Answer
Correct answer: (A) \(\dfrac{10}{s^2+11s+34}\).
Question 02 · 1 MarkQuestion 2
A unity negative feedback system has the open-loop transfer function
Equation
\[G(s) = \frac{50}{(s+1)(s+5)(s+10)}\]
The steady-state error for the input \(r(t) = 4\,u(t)\) is _____.
Solution
There is no pole at the origin, so the system is Type 0 and a step input leaves a finite non-zero error governed by the position error constant (see Chapter 9):
Equation
\[K_p = \lim_{s \to 0} G(s) = \frac{50}{1 \times 5 \times 10} = \frac{50}{50} = 1\]
For a step of amplitude \(A\), the steady-state error is \(e_{ss} = A/(1+K_p)\). Here \(A = 4\):
Equation
\[e_{ss} = \frac{4}{1 + 1} = 2\]
✓
Final Answer
Correct answer: 2
Question 03 · 1 MarkQuestion 3
A unity negative feedback system has the open-loop transfer function
Equation
\[G(s) = \frac{K}{(s+1)(s+3)(s+5)}\]
The range of \(K\) for which the closed-loop system is stable is
- \(0 < K < 23\)
- \(0 < K < 192\)
- \(0 < K < 207\)
- \(K > 192\)
Solution
Form the characteristic equation \(1 + G(s) = 0\). Expanding the denominator,
Equation
\[(s+1)(s+3)(s+5) = (s+1)(s^2 + 8s + 15) = s^3 + 9s^2 + 23s + 15\]
Equation
\[s^3 + 9s^2 + 23s + (15 + K) = 0\]
Construct the Routh array (see Chapter 11):
Equation
\[\begin{array}{c|cc} s^3 & 1 & 23 \\ s^2 & 9 & 15+K \\ s^1 & \dfrac{9(23) - (15+K)}{9} & 0 \\ s^0 & 15+K & \end{array}\]
The \(s^0\) row requires \(15 + K > 0\), i.e. \(K > -15\). The \(s^1\) row requires
Equation
\[207 - 15 - K > 0 \Rightarrow K < 192\]
Taking \(K\) positive as a gain, the stable range is \(0 < K < 192\). At \(K = 192\) the \(s^1\) row vanishes and the auxiliary equation \(9s^2 + 207 = 0\) gives sustained oscillation at \(\omega = \sqrt{23} = 4.796\) rad/s.
B
Final Answer
Correct answer: (B) \(0 < K < 192\).
Question 04 · 1 MarkQuestion 4
For the unity negative feedback system with
Equation
\[G(s)H(s) = \frac{K(s+4)}{s(s+1)(s+6)}, \qquad K > 0\]
the centroid of the root-locus asymptotes and the angles of the asymptotes are
- \(-3.5\) and \(\pm 90^\circ\)
- \(-1.5\) and \(\pm 60^\circ, 180^\circ\)
- \(-1.5\) and \(\pm 90^\circ\)
- \(-2.33\) and \(\pm 60^\circ, 180^\circ\)
Solution
The open-loop poles are \(0, -1, -6\) so \(n = 3\), and there is one finite zero at \(-4\) so \(m = 1\). The number of asymptotes is \(n - m = 2\) (see Chapter 12).
Equation
\[\sigma_A = \frac{\sum \text{poles} - \sum \text{zeros}}{n-m} = \frac{(0 - 1 - 6) - (-4)}{2} = \frac{-7 + 4}{2} = -1.5\]
The asymptote angles are
Equation
\[\theta_q = \frac{(2q+1)180^\circ}{n-m}, \qquad q = 0, 1\]
Equation
\[\theta_0 = \frac{180^\circ}{2} = 90^\circ, \qquad \theta_1 = \frac{3 \times 180^\circ}{2} = 270^\circ \equiv -90^\circ\]
So the two branches that go to infinity leave along the vertical asymptotes at \(\pm 90^\circ\) through \(\sigma_A = -1.5\).
C
Final Answer
Correct answer: (C) \(-1.5\) and \(\pm 90^\circ\).
Question 05 · 2 MarksQuestion 5
A unity negative feedback system has the open-loop transfer function
Equation
\[G(s) = \frac{K}{s(s+4)}, \qquad K > 0\]
The value of \(K\) that produces a phase margin of \(60^\circ\) is _____ (rounded off to two decimal places).
Solution
The phase of the loop is independent of \(K\), so the phase-margin specification fixes the gain crossover frequency first (see Chapter 17):
Equation
\[\angle G(j\omega) = -90^\circ - \tan^{-1}\!\frac{\omega}{4}\]
Equation
\[\text{PM} = 180^\circ + \angle G(j\omega_{gc}) = 90^\circ - \tan^{-1}\!\frac{\omega_{gc}}{4} = 60^\circ\]
Equation
\[\tan^{-1}\!\frac{\omega_{gc}}{4} = 30^\circ \Rightarrow \omega_{gc} = 4\tan 30^\circ = \frac{4}{\sqrt{3}} = 2.309\ \text{rad/s}\]
Now enforce unity magnitude at \(\omega_{gc}\):
Equation
\[\frac{K}{\omega_{gc}\sqrt{\omega_{gc}^2 + 16}} = 1 \Rightarrow K = \omega_{gc}\sqrt{\omega_{gc}^2 + 16}\]
With \(\omega_{gc}^2 = 16/3\), the term under the root is \(16/3 + 16 = 64/3\), so \(\sqrt{\cdot} = 8/\sqrt{3}\):
Equation
\[K = \frac{4}{\sqrt{3}} \times \frac{8}{\sqrt{3}} = \frac{32}{3} = 10.67\]
✓
Final Answer
Correct answer: \(K = 10.67\)
Question 06 · 2 MarksQuestion 6
A plant \(G_p(s) = \dfrac{5}{(s+1)(s+5)}\) is placed in a unity negative feedback loop with the PI controller
Equation
\[G_c(s) = K_p + \frac{K_i}{s}, \qquad K_p = 2\]
The largest value of \(K_i\) for which the closed-loop system remains stable is _____.
Solution
The PI controller adds a pole at the origin, raising the system to Type 1 (see Chapter 19). The characteristic equation is \(1 + G_c(s)G_p(s) = 0\):
Equation
\[1 + \frac{(K_p s + K_i)}{s} \cdot \frac{5}{(s+1)(s+5)} = 0\]
Equation
\[s(s+1)(s+5) + 5(K_p s + K_i) = 0\]
Expanding \(s(s+1)(s+5) = s^3 + 6s^2 + 5s\) and substituting \(K_p = 2\):
Equation
\[s^3 + 6s^2 + (5 + 10)s + 5K_i = s^3 + 6s^2 + 15s + 5K_i = 0\]
Routh array:
Equation
\[\begin{array}{c|cc} s^3 & 1 & 15 \\ s^2 & 6 & 5K_i \\ s^1 & \dfrac{90 - 5K_i}{6} & 0 \\ s^0 & 5K_i & \end{array}\]
Both conditions must hold: \(5K_i > 0\) gives \(K_i > 0\), and
Equation
\[90 - 5K_i > 0 \Rightarrow K_i < 18\]
The stable range is \(0 < K_i < 18\), so the limiting value is \(K_i = 18\). At that value the auxiliary equation \(6s^2 + 90 = 0\) gives sustained oscillation at \(\omega = \sqrt{15} = 3.873\) rad/s.
✓
Final Answer
Correct answer: \(K_i = 18\)
Question 07 · 2 MarksQuestion 7
The loop transfer function of a unity negative feedback system is
Equation
\[G(s)H(s) = \frac{20}{(s+1)(s+2)(s+4)}\]
Using the Nyquist criterion, the closed-loop system is
- unstable, with two encirclements of \(-1+j0\)
- stable, with a gain margin of \(13.06\) dB
- stable, with a gain margin of \(6.02\) dB
- marginally stable
Solution
The loop transfer function has no poles in the right half plane, so \(P = 0\) and the Nyquist criterion \(N = Z - P\) requires zero encirclements of \(-1+j0\) for stability (see Chapter 16). Find where the plot crosses the negative real axis. Expanding,
Equation
\[(s+1)(s+2)(s+4) = s^3 + 7s^2 + 14s + 8\]
With \(s = j\omega\):
Equation
\[D(j\omega) = (8 - 7\omega^2) + j(14\omega - \omega^3)\]
Equation
\[14\omega - \omega^3 = 0 \Rightarrow \omega_{pc} = \sqrt{14} = 3.742\ \text{rad/s}\]
At that frequency \(D = 8 - 7(14) = -90\), so
Equation
\[G(j\omega_{pc})H(j\omega_{pc}) = \frac{20}{-90} = -0.2222\]
The crossing occurs at \(-0.222\), which is to the right of \(-1\). The critical point is therefore not enclosed, \(N = 0\), and with \(P = 0\) the number of closed-loop right-half-plane poles is \(Z = 0\): the system is stable. The gain margin is
Equation
\[\text{GM} = 20\log_{10}\frac{1}{0.2222} = 20\log_{10} 4.5 = 13.06\ \text{dB}\]
B
Final Answer
Correct answer: (B) stable, with a gain margin of \(13.06\) dB.
Question 08 · 2 MarksQuestion 8
A system is described by
Equation
\[\dot{x} = \begin{bmatrix} -2 & 1 \\ 0 & -3 \end{bmatrix} x, \qquad y = \begin{bmatrix} 1 & \alpha \end{bmatrix} x\]
The value of \(\alpha\) for which the system is not completely observable is
- \(\alpha = -1\)
- \(\alpha = 0\)
- \(\alpha = 1\)
- \(\alpha = 3\)
Solution
For a second-order system the observability matrix is \(Q_o = \begin{bmatrix} C \\ CA \end{bmatrix}\), and complete observability requires \(\det Q_o \neq 0\) (see Chapter 25). Compute \(CA\):
Equation
\[CA = \begin{bmatrix} 1 & \alpha \end{bmatrix}\begin{bmatrix} -2 & 1 \\ 0 & -3 \end{bmatrix} = \begin{bmatrix} -2 & 1 - 3\alpha \end{bmatrix}\]
Equation
\[Q_o = \begin{bmatrix} 1 & \alpha \\ -2 & 1-3\alpha \end{bmatrix}\]
Equation
\[\det Q_o = (1)(1 - 3\alpha) - \alpha(-2) = 1 - 3\alpha + 2\alpha = 1 - \alpha\]
The determinant is zero only at \(\alpha = 1\), where \(Q_o\) has rank one and the mode associated with the eigenvalue \(-3\) becomes invisible at the output.
C
Final Answer
Correct answer: (C) \(\alpha = 1\).
Question 09 · 2 MarksQuestion 9
A unity negative feedback system has the open-loop transfer function
Equation
\[G(s) = \frac{16}{s(s+4)}\]
For a unit-step input, the percentage peak overshoot is _____ % (rounded off to two decimal places), and the \(2\%\) settling time is _____ s.
Solution
Close the loop:
Equation
\[T(s) = \frac{G(s)}{1+G(s)} = \frac{16}{s^2 + 4s + 16}\]
Comparing with \(s^2 + 2\zeta\omega_n s + \omega_n^2\) (see Chapter 8):
Equation
\[\omega_n = 4\ \text{rad/s}, \qquad 2\zeta\omega_n = 4 \Rightarrow \zeta = \frac{4}{8} = 0.5\]
Equation
\[\sqrt{1-\zeta^2} = \sqrt{0.75} = 0.8660\]
Percentage peak overshoot:
Equation
\[\%M_p = 100\exp\!\left(\frac{-\pi \times 0.5}{0.8660}\right) = 100 e^{-1.8138} = 16.30\%\]
The \(2\%\) settling time uses the envelope \(e^{-\zeta\omega_n t}\):
Equation
\[t_s = \frac{4}{\zeta\omega_n} = \frac{4}{0.5 \times 4} = 2\ \text{s}\]
✓
Final Answer
Correct answer: \(16.30\%\) and \(2\) s.
Question 10 · 2 MarksQuestion 10
The unforced state equation of a system is \(\dot{x} = Ax\) with
Equation
\[A = \begin{bmatrix} -1 & 1 \\ 0 & -1 \end{bmatrix}, \qquad x(0) = \begin{bmatrix} 1 \\ 2 \end{bmatrix}\]
The value of \(x_1(t)\) at \(t = 1\) s is _____ (rounded off to three decimal places).
Solution
The matrix has a repeated eigenvalue at \(-1\). Split it as \(A = -I + N\) where
Equation
\[N = \begin{bmatrix} 0 & 1 \\ 0 & 0 \end{bmatrix}, \qquad N^2 = \begin{bmatrix} 0 & 0 \\ 0 & 0 \end{bmatrix}\]
Since \(-I\) and \(N\) commute and \(N\) is nilpotent, the series for the state transition matrix terminates after two terms (see Chapter 24):
Equation
\[\phi(t) = e^{At} = e^{-t}\left(I + Nt\right) = e^{-t}\begin{bmatrix} 1 & t \\ 0 & 1 \end{bmatrix}\]
The zero-input response is \(x(t) = \phi(t)x(0)\), so
Equation
\[x_1(t) = e^{-t}\left(1 \times 1 + t \times 2\right) = e^{-t}(1 + 2t)\]
At \(t = 1\) s:
Equation
\[x_1(1) = 3e^{-1} = \frac{3}{2.71828} = 1.104\]
✓
Final Answer
Correct answer: \(x_1(1) = 1.104\)