Showing posts with label Control System. Show all posts
Showing posts with label Control System. Show all posts
z-plane
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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
Slope of log-magnitude asymptote
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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
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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 theseAnswer is ( b )
Lets understand an additional concept (may not be useful to solve the question ) of the Zero Order Hold impulse response graphically:
Concept
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
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For the control system in the given figure, the value of K for critical damping is
(a) 1
(c) 6.831
(d) 10Answer is ( b )
We should first consider simplifying the block - diagram in the question as:
Concept

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
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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 systemLarge 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
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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)$$R(s) = \frac{8}{s^2}$ , Input signal is Ramp type, velocity error constant $K_v = 0$Steady State Error $e_ss = 1/K_v = \infty$
System Response 1.2
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A system with zero initial conditions has the closed loop transfer function $ T(s) = \frac{s^2 +4}{(s+1)(s+4)}$.The system output is zero at the frequency______rad/s
(a) 2
(b) 1
(c) 0
(d) none of above
Answer is ( a )
Concept
The transfer function of system is $T(s) = \frac{s^2+4}{(s+1)(s+4)} $$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 $$ - \omega^2 + 4 = 0, \omega = 2 rad/sec $
Damping ratio and natural frequency 1.1
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The transfer function of a system is $T(s)=\frac{5}{(s+3)(s+6)}$.The damping ratio and natural frequency are respectively
(a) 4.24,2.12 rad/s
(b) 2.12,4.24 rad/s
(c) 4.24,1.06 rad/s
(d) 1.06,4.24 rad/s
Answer is ( )
Concept
The transfer function of a system is $T(s) = \frac{5}{s^2 + 9s +18}$Characteristic Eqn. $s^2 + 9s +18 = 0$ STANDARD Characteristic Eqn. $s^2 + 2\zeta\omega_n s + \omega_n^{2} = 0$Comparing both Std & Characteristic Characteristic Eqn. gives $\omega_n^{2} = 18$$2\zeta\omega_n = 9$ .On Solving , $\omega_n = 4.24$ rad/sec & $\zeta = 1.06$
Transfer function problem 1.7
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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
Concept
All poles are on right side.But, the zero is on the right half zero.Hence,its a non-minimum phase system
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