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151.

The asymptotic Bode phase plot of G(s)=k(s+0.1)(s+10)(s+p1), with k and p1 both positive , is shown below.The value of p1 is1

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The asymptotic Bode phase plot of G(s)=k(s+0.1)(s+10)(s+p1), with k and p1 both positive , is shown below.



https://df0b18phdhzpx.cloudfront.net/ckeditor_assets/pictures/1185660/original_24.a1.pngThe value of p1 is





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152.

A unity feedback system has an open loop transfer function, G(s)=Ks2. Its root locus plot will be

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A unity feedback system has an open loop transfer function, G(s)=Ks2. Its root locus plot will be

153.

The loop transfer function of a feedback control system is given by,G(s)H(s)=K(s+6)s(s+4)The range of value of K for underdamped system will be

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The loop transfer function of a feedback control system is given by,

G(s)H(s)=K(s+6)s(s+4)

The range of value of K for underdamped system will be

154.

The frequency responseG(s)=1/[s(s+1)(s+2)] plotted in the complex G(jω) plane (for 0<ω<∞) is

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The frequency response

G(s)=1/[s(s+1)(s+2)] plotted in the complex G(jω) plane (for 0<ω<) is

155.

A second order control system has the settling time of 5 seconds (for ± 2) tolerance ) and the peak time of 2 seconds. The locations of poles in the s-plane are

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A second order control system has the settling time of 5 seconds (for ± 2) tolerance ) and the peak time of 2 seconds. The locations of poles in the s-plane are

156.

The loop transfer function of a negative feedback system is given byG(s)H(s)=Ks(s+2)(s+6),where k&gt;0. The value of K at the breakaway point of the root locus for the above system (rounded of to one decimal place) is5

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The loop transfer function of a negative feedback system is given by

G(s)H(s)=Ks(s+2)(s+6),where k>0. The value of K at the breakaway point of the root locus for the above system (rounded of to one decimal place) is



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157.

For a system with the transfer function: H(s)=3(s−2)s3+4s2−2s+1the matrix A in the state space form ˙x=Ax+Bu is equal to

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For a system with the transfer function:



H(s)=3(s2)s3+4s22s+1



the matrix A in the state space form ˙x=Ax+Bu is equal to

158.

The open-loop transfer function of a dc motor is given as ω(s)Va(s)=101+10s. When connected in feedback as shown below, the approximate value of Ka that will reduce the time constant of the closed loop system by one hundred times as compared to that of the open-loop system is

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The open-loop transfer function of a dc motor is given as ω(s)Va(s)=101+10s. When connected in feedback as shown below, the approximate value of Ka that will reduce the time constant of the closed loop system by one hundred times as compared to that of the open-loop system is


159.

In a Bode magnitude plot, which one of the following slopes would be exhibited at high frequencies by a 4th order all-pole system ?

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In a Bode magnitude plot, which one of the following slopes would be exhibited at high frequencies by a 4th order all-pole system ?

160.

Figure shows the root locus plot (location of poles not given) of a third order system whose open loop transfer function is

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Figure shows the root locus plot (location of poles not given) of a third order system whose open loop transfer function is




161.

The signal flow graph of a system is shown below. U(s) is the input and C(s) is the output.Assuming, h1=b1 and ho=b0−b1a1, the input- output transfer function, G(s)=C(s)U(s) of the system is given by

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The signal flow graph of a system is shown below. U(s) is the input and C(s) is the output.







Assuming, h1=b1 and ho=b0b1a1, the input- output transfer function, G(s)=C(s)U(s) of the system is given by




162.

The Nyquist plot for the open-loop transfer function G(s) of a unity negative feedback system is shown in the figure, if G(s) has no pole in the right-half of s-plane, the number of roots of the system characteristic equation in the right-half of s-plane is

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The Nyquist plot for the open-loop transfer function G(s) of a unity negative feedback system is shown in the figure, if G(s) has no pole in the right-half of s-plane, the number of roots of the system characteristic equation in the right-half of s-plane is