Control system miscellaneous
- The feedback system shown below oscillates at 2 rad/s when
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Characterisitic equation is
1 + G(s)H(s) = 0∴ 1 + k(s + 1) = 0 s3 + as2 + 2s + 1
⇒ s3 + s2a + s(k + 2) + (k + 1) = 0
as2 + (k + 1) = 0 ; s = jω ; s2 = – ω2; ; ω = 2
– aω2 + (k + 1) = 0 ; aω2 = k + 1 ; 4a = k + 1 ;
From options, k = 2, a = 0.75
Correct Option: A
Characterisitic equation is
1 + G(s)H(s) = 0∴ 1 + k(s + 1) = 0 s3 + as2 + 2s + 1
⇒ s3 + s2a + s(k + 2) + (k + 1) = 0
as2 + (k + 1) = 0 ; s = jω ; s2 = – ω2; ; ω = 2
– aω2 + (k + 1) = 0 ; aω2 = k + 1 ; 4a = k + 1 ;
From options, k = 2, a = 0.75
- The frequency response of a linear system G(jω) is provided in the tabular form below
| G(jω)| 1.3 1.2 1.0 0.8 0.5 0.3 ∠ G(jω) – 130° – 140° – 150° – 160° – 180° – 200°
The gain margin and phase margin of the system are
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At ∠ G(jω) = – 180, magnitude M = 0.5
∴ G.M = 20 log 1 = 6 dB 0.5
At | G(jω) | = 1, phase angle ∠ G(jω) = – 150
∴ P.M = 180 + (– 150) = 30°Correct Option: A
At ∠ G(jω) = – 180, magnitude M = 0.5
∴ G.M = 20 log 1 = 6 dB 0.5
At | G(jω) | = 1, phase angle ∠ G(jω) = – 150
∴ P.M = 180 + (– 150) = 30°
- The steady state error of a unity feedback linear system for a unit step input is 0.1. The steady state error of the same system, for a pulse input r(t) having a magnitude of 10 and a duration of one second, as shown in the figure is
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For step input, ess = 0.1 = 1 1 + k
Now input is pulse r(t) = 10 [u(t) – u(t – 1)]R(s) = 10 1 - e-s s
Correct Option: A
For step input, ess = 0.1 = 1 1 + k
Now input is pulse r(t) = 10 [u(t) – u(t – 1)]R(s) = 10 1 - e-s s
- A point z has been plotted in the complex plane, as shown in figure below.
The plot of the complex number y = 1 is z
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| Z| < 1, so | Y| > 1
Z is having +ve real part and positive imaginary part (from characteristics)
So,Y should have +ve real part and negative imaginary part.Correct Option: D
| Z| < 1, so | Y| > 1
Z is having +ve real part and positive imaginary part (from characteristics)
So,Y should have +ve real part and negative imaginary part.
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An open loop system represented by the transfer function G(s) = (s - 1) is (s + 2)(s + 3)
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Since, open loop system stability is depends only on pole locations, hence system is stable. There is one zero on right half of s-plane so system is non-minimum phase.
Correct Option: B
Since, open loop system stability is depends only on pole locations, hence system is stable. There is one zero on right half of s-plane so system is non-minimum phase.