Showing posts with label Control System. Show all posts
Showing posts with label Control System. Show all posts

PID controller

Ask
Most commonly used PID controller used to model behavior of control system is actually:
(a)Proportional-Integral - Derivative controller
(b) Proportion - Intuitive- Derived controller
(c)Partial -Integral - Dilutor

(d)none of these



Answer is ( )
Concept
Type Reasoning here



Error Voltage

Ask
If error voltage is e(t), then its integral square error =
(a) e^2(t) dt
(b) integral of 0 to infinity (e^2(t) dt)
(c) sqrt [integral of 0 to infinity (e^2(t) dt)]

(d) None of the above



Answer is ( )
Concept
Type Reasoning here


Steady state output

Ask
In the given figure the input is x(t) = A sin ωt. The steady state output y(t) =
(a) A sin (ωt + φ) where φ = tan_inverse |G(jω)|
(b) |G(jω)| A sin [ωt + ∠G(jω)]
(c) |G(jω)| A sin [2ωt + ∠G(jω)]
(d) A G(jω) sin [ωt + ∠G(jω)]




Answer is ( )
Concept
Type Reasoning here


Bode magnitude plot

Ask
Bode magnitude plot is drawn between
(a) magnitude of network function and ω
(b) dB magnitude and log ω
(c) dB magnitude and ω

(d) loge (magnitude) and log ω


Answer is ( )
Concept
Type Reasoning here


System Stability for Characteristic Equation

Ask
For the P(z) in the given equation,determine
(a) System is stable
(b) System is unstable
(c) System is partially stable
(d) cannot determine



Answer is ( )
Concept
Type Reasoning here

z-plane

Ask
STATEMENT A:
For a System to be STABLE all the closed loop poles or the roots of the characteristic equation must lie within the unit circle in z-plane.
STATEMENT B:
If a simple pole lies at |z| =1, the system becomes marginally stable. Similarly if a pair of complex conjugate poles lie on the |z|=1 circle, the system is marginally stable.
STATEMENT C - Multiple poles at the same location on unit circle make the system unstable.
Which of the above statements are true?
(a) STATEMENT A&B are True, STATEMENT C is false
(b) STATEMENT A,B&C are true
(c) STATEMENT A&C are true

(d)none of them are true




Answer is ( )
Concept
Type Reasoning here

Voltage Gain

Ask
In the given figure, if R = Xc, then voltage gain is
(a) 0 dB
(b) 3 dB
(c) -3 dB
(d) 20 dB




Answer is ( )
Concept
Type Reasoning here

Minimum Phase System

Ask
In a minimum phase system
(a) all poles lie in the left half plane
(b) all zeros lie in the left half plane
(b) all poles lie in the right half plane
(d) all except one pole or zero lie in the left half plane



Answer is ( )
Concept
Type Reasoning here



Routh - array

Ask
The first column of a Routh array is add shown in the figure. How many roots of the corresponding characteristic equation are in left half s-plane?
(a) 2
(b) 3
(c) 4

(d) 5



Answer is ( )
Concept
Type Reasoning here

Log Magnitude Plot

Ask
In Bode diagram (log magnitude plot) the factor $(jω)^n$ in the transfer function gives a line having slope
(a) 20 dB/decade
(b) 20n dB/decade
(c) 20/n dB/decade
(d) -20n dB/decade



Answer is ( )
Concept
Type Reasoning here


Slope of log-magnitude asymptote

Ask
The slope of log-magnitude asymptote changes by -40 dB/decade at a frequency ω1. This means that
(a) a double pole is present
(b) a pair of complex conjugate poles is present
(c) either a double pole or a pair of complex conjugate poles is present

(d) a pole or zero at origin is present



Answer is ( )
Concept
Type Reasoning here



ZOH Impulse Response FT

Ask
Zero Order Hold system has an impulse response given by
$u(t)- u(t-T)$
The Fourier transform of the system is
(a)$\frac{[1-e^{j\omega T}]}{ j\omega }$
(b)$\frac{[1-e^-j\omega T]}{j\omega}$
(c)$\frac{[1+e^j\omega T]}{j\omega}$
(d) none of these

Answer is ( b )
Concept
Lets understand an additional concept (may not be useful to solve the question ) of the Zero Order Hold impulse response graphically:


Laplace Transform of $u(t) \rightarrow \frac{1}{s}$ 
$u(t-T) \rightarrow \frac{e^{-Ts}}{s}$

Thus , $u(t) - u(t-T) $
$\implies \frac{1}{s} - \frac{e^{-Ts}}{s} $
$\implies \frac{1-e^{-Ts}}{s} $

For Fourier Transform ,  $s = j\omega$
 $u(t) - u(t-T) =   \frac{1-e^{-T j\omega}}{j\omega} $

http://nptel.ac.in/courses/108103008/4


Critical Damping

Ask
For the control system in the given figure, the value of K for critical damping is
(a) 1
(b) 5.125
(c) 6.831
(d) 10



Answer is ( b )
Concept
We should first consider simplifying the block - diagram in the question as:



Combining the two cascaded blocks , we get : $G(s) = (K)(\frac{2}{s^2+7s+2})$

A closed loop control system having a form as below:



Thus , the above diagram simplifies to $\frac{C(s)}{R(s)} = \frac{(\frac{2K}{s^2+7s+2})}{1+(\frac{2K}{s^2+7s+2})}$

$\implies \frac{C(s)}{R(s)}=  \frac{2K}{s^2+7s+2+2K}$

Now to Solve the Above Equation we need to understand the characteristic equation of a second - order system.

In general a second - order control system equation is given by :
$$\frac{C(s)}{R(s)}= \frac{\omega_n^2}{s^2+2\zeta\omega_n s+\omega_n^2}$$
where,
$\zeta$ = damping ratio ; $\omega_n$ = natural frequency
The characteristic Equation of the system is given by :$s^2+2\zeta\omega_n s+\omega_n^2 = 0$
Comparing this equation to an algebraic equation of the form $ax^2+bx+c=0$
The roots of the above equation are $ x= \frac{-b \pm \sqrt{b^2 - 4ac}}{2a}$
For a critical damping case $ b^2 - 4ac= 0 , \implies x= \frac{-b}{2a}$

The characteristic equation for the given problem : $s^2+7s+2+2K = 0 $
As for critical damping case $ b^2 - 4ac= 0 $
$\implies  7^2 - 4(1)(2+2K)= 0 $
$\implies  K=41/8 = 5.125 $











s-plane stability concept

Ask
The constant damping loci $s= a+jb$ where 'a' represents the real part ideally indicates
(a) damping factor
(b) rate of decay time of the system response
(c) rate of rise time of the system response
(d)All the Above

Answer is ( d )

Concept
A pole in s-plane is given by $s= a+jb$ where 'a' is real part and 'b' is the imaginary part.Here, the real - part 'a' determines the  damping factor . This ideally indicates the rate of rise  or rate of decay of time response of the system
Large value of 'a' represents small time constant $\implies$ faster decay.
As can be seen from figure, the loci on left half of s-plane denotes positive damping
While , the loci on the right half of s-plane denotes negative damping .

Concept of s-plane : http://nptel.ac.in/courses/108103008/6

Steady State Error 1.1

Ask
A system has position error constant $K_p = 3$. The steady error for input of 8tu(t) is
(a) 2.67
(b) 2
(c) $\infty$
(d) 0

Answer is (c  )
Concept
Positional Error Constant $K_p = 3$ , Input Signal = $r(t) = 8tu(t)$
$R(s) = \frac{8}{s^2}$ , Input signal is Ramp type, velocity error constant $K_v = 0$
Steady State Error $e_ss = 1/K_v = \infty$


Bode Diagram

Ask
In Bode diagram (log magnitude plot) the factor (1/j$\omega$) in the transfer function gives a line having slope
(a) -20 dB per octave
(b) -10 dB per octave
(c) -6 dB per octave
(d) -2 dB per octave


Answer is ( )
Concept
Type Reasoning here


System Response 1.2

Ask
A system with zero initial conditions has the closed loop transfer function $ T(s) = \frac{s^2 +4}{(s+1)(s+4)}$.The system output is zero at the frequency______rad/s
(a) 2
(b) 1
(c) 0
(d) none of above

Answer is ( a )
Concept
The transfer function of system is $T(s) = \frac{s^2+4}{(s+1)(s+4)} $
$T(j\omega) = \frac{(j\omega)^{2}+4}{(j\omega+1)(j\omega+4)} $
If system output is zero, $|T(j\omega)| = \frac{|4-\omega^2|}{|(j\omega+4)(j\omega+1|} = 0 $
$ - \omega^2 + 4 = 0, \omega = 2 rad/sec $

Damping ratio and natural frequency 1.1

Ask
The transfer function of a system is $T(s)=\frac{5}{(s+3)(s+6)}$.The damping ratio and natural frequency are respectively
(a) 4.24,2.12 rad/s
(b) 2.12,4.24 rad/s
(c) 4.24,1.06 rad/s
(d) 1.06,4.24 rad/s



Answer is ( )
Concept
The transfer function of a system is $T(s) = \frac{5}{s^2 + 9s +18}$
Characteristic Eqn. $s^2 + 9s +18 = 0$ STANDARD Characteristic Eqn. $s^2 + 2\zeta\omega_n s + \omega_n^{2} = 0$
Comparing both Std & Characteristic Characteristic Eqn. gives $\omega_n^{2} = 18$
$2\zeta\omega_n = 9$ .On Solving , $\omega_n = 4.24$ rad/sec & $\zeta = 1.06$

Transfer function problem 1.7

Ask
The closed loop transfer function of a control system is given as $T(s)= \frac{s-5}{(s+2)(s+3)}$.This is
(a) an unstable system
(b) an uncontrollable system
(c) a minimum phase system
(d) a non-minimum phase system

Answer is ( d )
Concept
All poles are on right side.But, the zero is on the right half zero.Hence,its a non-minimum phase system

Log Magnitude Curve

Ask
The log magnitude curve for a constant gain K is a
(a) horizontal straight line
(b) horizontal straight line of magnitude 20logK decibels
(c) an inclined line having slope K
(d) an inclined line having slope -K


Answer is ( )
Concept
Type Reasoning here