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Control Systems Test 4

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Control Systems Test 4
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  • Question 1
    1 / -0

    Consider a stable system with the transfer function

    \(G\left( s \right) = \frac{{{s^p} + {b_1}\;{s^{p - 1}} + \ldots {b_p}}}{{{s^q} + {a_1}{s^{q - 1}} + \ldots {a_q}}}\)

    Where b1,…..,bp  and a1,…..,aq are real valued constants. The slope of the Bode log magnitude curve of G(s) converges to -60 dB/decade as ω → ∞. A possible pair of values for p and q is:
    Solution

    Bode plot transfer function is represented in standard time constant form as \(T\left( s \right) = \frac{{k\left( {\frac{s}{{{\omega _{{c_1}}}}} + 1} \right) \ldots }}{{\left( {\frac{s}{{{\omega _{{c_2}}}}} + 1} \right)\left( {\frac{s}{{{\omega _{{c_3}}}}} + 1} \right) \ldots }}\)

    ωc1, ωc2, … are corner frequencies.

    In a Bode magnitude plot,

    • For a pole at the origin, the initial slope is -20 dB/decade
    • For a zero at the origin, the initial slope is 20 dB/decade
    • The slope of magnitude plot changes at each corner frequency
    • The corner frequency associated with poles causes a slope of -20 dB/decade
    • The corner frequency associated with poles causes a slope of -20 dB/decade
    • The final slope of Bode magnitude plot = (Z – P) × 20 dB/decade


    Where Z is the number zeros and P is the number of poles

    Application:

    As the final slope is -60 dB/decade, it indicates that the difference between the poles and zeros is 3.

    Therefore, to get a final slope of -60 dB/decade, the condition required is, p-q = 3

  • Question 2
    1 / -0
    The open loop transfer function of a unity feedback system is given by \(G\left( s \right) = \frac{{\pi {e^{ - 0.25s}}}}{s}\). In G(s) plane, the Nyquist plot of G(s) passes through the negative real axis at the point
    Solution

    \(G\left( s \right) = \frac{{\pi {e^{ - 0.25s}}}}{s}\)

    In G(s) plane, the Nyquist plot of G(S) passes through the negative real axis at the point (-a, j0)

    a = magnitude of G(s) at ω = ωpc

    ωpc is phase cross over frequency.

    at \({\rm{\omega}} = {{\rm{\omega }}_{{\rm{pc}}}},\angle G\left( {j\omega } \right) = - 180^\circ\)

     -0.25 ωpc – 90 = -180

    ωpc = 2π

    \({\left| {G\left( {j\omega } \right)} \right|_{{\rm{\omega }} = {{\rm{\omega }}_{{\rm{pc}}}}}} = \frac{{\pi \left( 1 \right)}}{{2\pi }} = 0.5\)

    (-a, j0) = (0.5, j0)
  • Question 3
    1 / -0

    A unity feedback control system has an open-loop transfer function,

    \(G\left( s \right)H\left( s \right) = \frac{K}{{s\left( {s + 2} \right)\left( {s + 4} \right)}}\)

    What is the value of K so that the gain margin of the system becomes 20 dB?

    Solution

    The gain margin of the system is given by:

    \(GM = 20{\log _{10}}\left( {\frac{1}{a}} \right)\)

    Where ‘a’ is the intersection point of the Nyquist plot on the negative real axis, i.e.

    \(20\;dB = 20{\log _{10}}\left( {\frac{1}{a}} \right)\)

    \(\frac{1}{a} = 10\)

    a = 0.1    ---(1)

    The open-loop transfer function is:

    \(G\left( s \right)H\left( s \right) = \frac{K}{{s\left( {s + 2} \right)\left( {s + 4} \right)}}\)      ---(2)

    At the negative real axis, the phase angle of the system is – 180°, i.e.

    \(\angle G\left( {jω } \right)H\left( {jω } \right) = - 180^\circ \)

    \( - 90^\circ - {\tan ^{ - 1}}\frac{ω }{2} - {\tan ^{ - 1}}\frac{ω }{4} = - 180^\circ \)

    \({\tan ^{ - 1}}\left( {\frac{{\frac{ω }{2} + \frac{ω }{4}}}{{1 - \frac{{{ω ^2}}}{8}}}} \right) = 90^\circ \)

    \(1 - \frac{{{ω ^2}}}{8} = 0\)

    ω = √8 rad/sec

    Replacing s with jω, the transfer function can be written as:

    \(G\left( j\omega \right)H\left( j\omega \right) = \frac{K}{{j\omega\left( {j\omega + 2} \right)\left( {j\omega + 4} \right)}}\)

    So, the Nyquist plot crosses the negative real axis for ω = √8 rad/sec. Hence, the intersection point ‘a’ will be:

    \(|G\left( {jω } \right)H\left( {jω } \right){\left. | \right|_{ω = \sqrt 8 }} = a\)

    \(a={\left. {\frac{K}{{ω \sqrt {{ω ^2} + 4 }\sqrt {{ω ^2} + 16}}}} \right|_{ω = \sqrt 8 }} \)

    With a = 0.1, we can write:

    \({\left. {\frac{K}{{ω \sqrt {{ω ^2} + 4 }\sqrt {{ω ^2} + 16}}}} \right|_{ω = \sqrt 8 }}=0.1 \)

    \(\frac{K}{{48}} = 0.1\)

    K = 4.8

  • Question 4
    1 / -0

    A unit step input is applied to a unity feedback control system having open-loop transfer function,

    \(G\left( s \right)H\left( s \right) = \frac{K}{{s\left( {1 + sT} \right)}}\)

    The specification is such that the maximum overshoot is 20% and the resonant frequency is ωr = 6 rad/sec. The values of K and T are

    Solution

    The characteristic equation for the given open-loop transfer function is defined as:

    1 + G(s)H(s) = 0

    ∴ For the given open-loop transfer function, we will get the characteristic equation as:

    \({s^2} + \frac{1}{T}s + \frac{K}{T} = 0\)     ---(1)

    The standard form of the characteristic equation of the second-order system will be:

    \({s^2} + 2\xi {\omega _n}s + \omega _n^2 = 0\)

    Comparing this with Equation (1), we get:

    \({\omega _n} = \sqrt {\frac{K}{T}}\)    ---(2)

    Also \( \;2\xi {\omega _n} = \frac{1}{T}\)

    Using Equation (2), we get:

    \(\xi = \frac{1}{{2\sqrt {KT} }}\)      ---(3)

    From the given problem, we have the maximum overshoot as:

    Mp = 20%

    Since the maximum overshoot is defined as:

    \({M_p} = \frac{{ - \xi \pi }}{{e\sqrt {1 - {\xi ^2}} }} = \frac{{20}}{{100}}\)

    Putting on the respective values:

    \(\frac{{\xi \pi }}{{\sqrt {1 - {\xi ^2}} }} = 1.6\)

    ξ = 0.45

    Now, the resonant frequency is given by:

    \({\omega _r} = {\omega _n}\sqrt {1 - 2{\xi ^2}} = 6\)

    Therefore, the natural frequency will be:

    \({\omega _n} = \frac{6}{{\sqrt {1 - 2{{\left( {0.45} \right)}^2}} }}\)

    = 7.82 rad/sec

    Substituting the values of ξ and ωn in Equations (1) and (2), we get:

    \({\left( {7.82} \right)^2} = \frac{K}{T}\;and\)

    \(0.45 = \frac{1}{{2\sqrt {KT} }}\)

    Solving the above equations, we obtain the values of K and T as:

    K = 8.67 and T = 0.14 

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