Test 3 - Control System | Electronics and Communication (ECE)
Topic wise test 3 for Control System (ECE) of GATE Electronics and Communication
Questions
The magnitude plot of a rational transfer function G (s) with real coefficients is shown below. Which of the following compensators has such a magnitude plot?

- Lead compensator
- Lag compensator
- PID compensator
- Lead-lag compensator
Which one of the following polar diagrams corresponds to a lag network?
The pole-zero given below corresponds to a

- Law pass filter
- High pass filter
- Band filter
- Notch filter
The feedback system shown below oscillates at 2 rad/s when
- K = 2 and a = 0.75
- K = 3 and a = 0.75
- K = 4 and a = 0.5
- K = 2 and a = 0.5
Given G(s) H(s) = $\dfrac{K}{s(s+1)(s+3)}$. The point of intersection of the asymptotes of the root loci with the real axis is
- - 4
- 1.33
- - 1.33
- 4
Direction: The Nyquist plot of a stable transfer function G (s) and its closed loop system in the feedback configuration are shown below.

Which of the following statements is true?
- G (s) is an all-pass filter.
- G (s) has a zero in the right half plane.
- G (s) is the impedance of a passive network.
- G (s) is marginally stable.
The transfer function of a phase-lead compensator is given by Gc = $\dfrac{1+3T_s}{1+T_s}$, where T > 0. What is the maximum phase shift of the compensator?
- $\dfrac{\pi}{2}$
- $\dfrac{\pi}{3}$
- $\dfrac{\pi}{4}$
- $\dfrac{\pi}{6}$
Group I gives two possible choices for the impedance Z in the diagram. The circuit elements in Z satisfy the conditions R2C2 > R1C1. The transfer functions $\dfrac{V_0}{V_i}$represents a kind of controller.

Match the impedances in Group I with the type of controllers in Group II.

- Q - 1, R - 2
- Q - 1, R - 3
- Q - 2, R - 3
- Q - 3, R - 2
The signal flow graph of a system is shown in figure. The transfer function $\dfrac{C(s)}{R(s)}$ of the system is

- $\dfrac{6}{s^2+29s+6}$
- $\dfrac{6s}{s^2+29s+6}$
- $\dfrac{s(s+2)}{s^2+29s+6}$
- $\dfrac{s(s+27)}{s^2+29s+6}$
Consider the Bode magnitude plot shown in the fig. The transfer function H(s) is
- $\dfrac{s+10}{(s+1)(s+100)}$
- $\dfrac{10(s+1)}{(s+10)(s+100)}$
- $\dfrac{10^2(s+1)}{(s+10)(s+100)}$
- $\dfrac{10^3(s+100)}{(s+1)(s+10)}$
The asymptotic Bode plot of a transfer function is as shown in the figure. The transfer function G(s) corresponding to this Bode plot is

- $\dfrac{1}{(s+1)(s+20)}$
- $\dfrac{1}{s(s+1)(s+20)}$
- $\dfrac{100}{s(s+1)(s+20)}$
- $\dfrac{100}{s(s+1)(1+0.05s)}$
A control system with a PD controller is shown in the figure. If the velocity error constant KV = 1000 and the damping ratio $\xi$= 0.5, the values of KP and KD are

- Kp = 100, KD = 0.09
- Kp = 100, KD = 0.9
- Kp = 10, KD = 0.09
- Kp = 10, KD = 0.9
Consider a linear system whose state space representation is x and (t) = Ax (t). If the initial state vector of the system is x (0) =$
\left[
\begin{array}
\ 1 \\
-2
\end{array}
\right]
$, the system response is x (t) = $
\left(
\begin{array}
\ e^{-2t} \\
-2 e^{-2t}
\end{array}
\right)
$. If the initial state vector of the system changes, the system response becomes x(t) = $
\left[
\begin{array}
\ e^{-t} \\
- e^{-6}
\end{array}
\right]
$.
The system matrix A is
- $ \left[ \begin{array} \ 0 & 1 \\\\ -1 & 1 \end{array} \right] $
- $ \left[ \begin{array} \ 1 & 1 \\\\ -1 & -2 \end{array} \right] $
- $ \left[ \begin{array} \ 2 & 1 \\\\ -1 & -1 \end{array} \right] $
- $ \left[ \begin{array} \ 0 & 1 \\\\ -2 & -3 \end{array} \right] $
The open loop transfer function of a unity feedback is given by
$G(s) = \dfrac{3e^{-2s}}{s(s+2)}$
Based on the above results, the gain and phase margins of the system will be
- - 7.09 dB and 87.5�
- 7.09 dB and 87.5�
- 7.09 dB and - 87.5�
- - 7.09 dB and - 87.5�
Consider two transfer functions:
G1 (s) = $\dfrac{1}{s^2 + as +b}$ and G2 (s) = $\dfrac{1}{s^2 + as +b}$
The 3 dB bandwidths of their frequency responses respectively are
- $\sqrt{a^2-4b}, \sqrt{a^2+4b}$
- $\sqrt{a^2+4b}, \sqrt{a^2-4b}$
- $\sqrt{a^2-4b}, \sqrt{a^2-4b}$
- $\sqrt{a^2+4b}, \sqrt{a^2+4b}$
A unity negative feedback closed loop system has a plant with the transfer function G(s) = $\dfrac{1}{s^2 + 2s +2}$ and a controller Gc(S) in the feed forward path. For a unit set input, the transfer function of the controller that gives minimum steady state error is
- GC(s) = $\dfrac{s+1}{s+2}$
- GC(s) = $\dfrac{s+2}{s+1}$
- GC(s) = $\dfrac{(s+1)(s+4)}{(s+2)(s+3)}$
- GC(s) = 1 + $\dfrac{2}{s}$+ 3s
A ramp input applied to an unity feedback system results in 5% steady state error. The type number and zero frequency gain of the system are respectively
- 1 and 20
- 0 and 20
- 0 and $\dfrac{1}{20}$
- 1 and $\dfrac{1}{20}$
Consider a linear system with state space representation is x and (t) = Ax (t). If the initial state vector of the system is x (0) =$
\left[
\begin{array}
\ 1 \\
-2
\end{array}
\right]
$, the system response is x (t) = $
\left(
\begin{array}
\ e^{-2t} \\
-2 e^{-2t}
\end{array}
\right)
$. If the initial state vector of the system changes, the system response becomes x(t) = $
\left[
\begin{array}
\ e^{-t} \\
- e^{-6}
\end{array}
\right]
$.
The eigen value and eigen vector pairs ($\lambda_i, V_i$) for the system are
- $ \left( \begin{array} \ -1, & \left[ \begin{array} \ 1 \\\\ -1 \end{array} \right] \end{array} \right) $and $ \left( \begin{array} \ -2, & \left[ \begin{array} \ 1 \\\\ -2 \end{array} \right] \end{array} \right) $
- $ \left( \begin{array} \ -1, & \left[ \begin{array} \ 1 \\\\ -1 \end{array} \right] \end{array} \right) $and $ \left( \begin{array} \ 2, & \left[ \begin{array} \ 1 \\\\ -2 \end{array} \right] \end{array} \right) $
- $ \left( \begin{array} \ 1, & \left[ \begin{array} \ 1 \\\\ -1 \end{array} \right] \end{array} \right) $and $ \left( \begin{array} \ -2, & \left[ \begin{array} \ 1 \\\\ -2 \end{array} \right] \end{array} \right) $
- $ \left( \begin{array} \ -2, & \left[ \begin{array} \ 1 \\\\ -1 \end{array} \right] \end{array} \right) $and $ \left( \begin{array} \ -1, & \left[ \begin{array} \ 1 \\\\ -2 \end{array} \right] \end{array} \right) $
The open loop transfer function of a unity feedback is given by
$G(s) = \dfrac{3e^{-2s}}{s(s+2)}$
The gain and phase crossover frequencies in rad/sec are respectively
- 0.632 and 1.26
- 0.632 and 0.485
- 0.485 and 0.632
- 1.26 and 0.632
Directions : The Nyquist plot of a stable transfer function G (s) and its closed loop system in the feedback configuration are shown below.

The gain and phase margins of G (s) for closed loop stability are
- 6 dB and 1800 respectively
- 3 dB and 1800 respectively
- 6 dB and 900 respectively
- 3 dB and 900 respectively














