Control systems miscellaneous


Control systems miscellaneous

  1. For the transfer function
    G(s) H(s) =
    1
    s(s + 1) (s + 0·5)

    the phase cross-over frequency is—









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    Phase cross-over frequency for the given transfer function

    G(s)H(s) =
    1
    s(s + 1)(s + 0·5)

    ∠G(s H(s) = – 90° – tan–1(ω/1) – tan–1(ω/0.5)
    – 180° = – 90° – tan–1 ω – tan–1 (2ω)
    or 90° = tan–1
    ω + 2ω
    at ω = ωP
    1 – ω.2ω

    or tan 90° =
    at ω = ωP
    1 – 2ω2

    or
    1
    =
    at ω = ωP
    01 – 2ω2

    or 1 – 2 ω2P = 0
    or ωP = 1/√2
    ωP = 0.707 rad/sec.

    Correct Option: B

    Phase cross-over frequency for the given transfer function

    G(s)H(s) =
    1
    s(s + 1)(s + 0·5)

    ∠G(s H(s) = – 90° – tan–1(ω/1) – tan–1(ω/0.5)
    – 180° = – 90° – tan–1 ω – tan–1 (2ω)
    or 90° = tan–1
    ω + 2ω
    at ω = ωP
    1 – ω.2ω

    or tan 90° =
    at ω = ωP
    1 – 2ω2

    or
    1
    =
    at ω = ωP
    01 – 2ω2

    or 1 – 2 ω2P = 0
    or ωP = 1/√2
    ωP = 0.707 rad/sec.


  1. Consider the system
    X(t) =
    1
    1
    X(t) +
    b1
    u(t)
    0-1b2

    c (t) = d1 d2 X (t)
    The conditions for complete state controllability and complete observability is—









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    Given

    A =
    1
    1
    , B =
    b1
    01b2

    C=[d1d2]
    For observability
    Q0 = [CT: AT CT] ≠ 0
    where,
    CT =
    b1
    b2

    AT =
    1
    0
    11

    AT CT =
    1
    0
    11

    AT CT =
    1
    0
    d1
    =
    d1
    11d2d1 + d2

    Now,
    Q0 =
    d1
    d1
    ≠ 0
    d2d1 + d2

    or
    d1(d1 + d2) - d1 d22 ≠ ≠ 0
    or
    d12 + d1d2 ≠ 0
    or
    d12 ≠ 0
    or
    d1 ≠ 0
    For controllability
    θC = [B: A B] ≠ 0
    where,
    B =
    d1
    d2

    AB =
    1
    1
    d1
    =
    d1 + d2
    01d2d2

    or
    Qc =
    d1
    d1 + d2
    d2d2

    or
    b1 b2 – b2 (b1 + b2) ≠ 0
    or
    b1 b2 – b22 – b1 b2 ≠ 0
    or
    – b22 ≠ 0
    or
    b2 ≠ 0
    Finally we conclude that only option (A) fulfils this condition.

    Correct Option: A

    Given

    A =
    1
    1
    , B =
    b1
    01b2

    C=[d1d2]
    For observability
    Q0 = [CT: AT CT] ≠ 0
    where,
    CT =
    b1
    b2

    AT =
    1
    0
    11

    AT CT =
    1
    0
    11

    AT CT =
    1
    0
    d1
    =
    d1
    11d2d1 + d2

    Now,
    Q0 =
    d1
    d1
    ≠ 0
    d2d1 + d2

    or
    d1(d1 + d2) - d1 d22 ≠ ≠ 0
    or
    d12 + d1d2 ≠ 0
    or
    d12 ≠ 0
    or
    d1 ≠ 0
    For controllability
    θC = [B: A B] ≠ 0
    where,
    B =
    d1
    d2

    AB =
    1
    1
    d1
    =
    d1 + d2
    01d2d2

    or
    Qc =
    d1
    d1 + d2
    d2d2

    or
    b1 b2 – b2 (b1 + b2) ≠ 0
    or
    b1 b2 – b22 – b1 b2 ≠ 0
    or
    – b22 ≠ 0
    or
    b2 ≠ 0
    Finally we conclude that only option (A) fulfils this condition.



  1. The value of A matrix in X′ = AX for the system described by the differential equation ÿ + 2y · + 3y = 0 is—









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    Try yourself

    Correct Option: D

    Try yourself


  1. The state and output equation of a system are as under state equation:
    x1
    (t)
    =01
    x1
    (t)
    +0u(t)
    x2(t)-1-2x2(t)1

    And
    C(t) =[1 1]
    x1
    (t)
    x2(t)

    The system is—









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    Given state equation:

    x1
    (t)
    =
    0
    1
    x1
    (t)
    +
    0
    u(t)
    x2(t)-1-2x2(t)1

    C(t) = [1 1]
    x1
    (t)
    x2(t)

    Here,
    A =
    0
    1
    -1-2

    B =
    0
    1

    C = [1 1]
    Check for controllability
    AB =
    0
    1
    0
    =
    1
    -1-21-2

    ∴ QC = [B: AB] = – 1, which is non-singular.
    Hence, the state equation is controllable.
    Check for observability :
    A =
    0
    1
    -1-2

    then
    AT =
    0
    -1
    1-2

    C = [1 1]
    then
    CT =
    1
    1

    Now,
    ATCT =
    0
    -1
    1
    1-21

    =
    -1
    -1

    θ0 = [CT : AT CT]
    ATCT =
    1
    -1
    1-1

    = 0 i.e., singular.
    Hence given system equation is not observable.
    Therefore alternative (B) is the correct choice.

    Correct Option: B

    Given state equation:

    x1
    (t)
    =
    0
    1
    x1
    (t)
    +
    0
    u(t)
    x2(t)-1-2x2(t)1

    C(t) = [1 1]
    x1
    (t)
    x2(t)

    Here,
    A =
    0
    1
    -1-2

    B =
    0
    1

    C = [1 1]
    Check for controllability
    AB =
    0
    1
    0
    =
    1
    -1-21-2

    ∴ QC = [B: AB] = – 1, which is non-singular.
    Hence, the state equation is controllable.
    Check for observability :
    A =
    0
    1
    -1-2

    then
    AT =
    0
    -1
    1-2

    C = [1 1]
    then
    CT =
    1
    1

    Now,
    ATCT =
    0
    -1
    1
    1-21

    =
    -1
    -1

    θ0 = [CT : AT CT]
    ATCT =
    1
    -1
    1-1

    = 0 i.e., singular.
    Hence given system equation is not observable.
    Therefore alternative (B) is the correct choice.



  1. Obtain the transfer function for the response curve shown below—











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    From figure
    20 log10 K = 12
    K = 1012/20
    or K = 3·98 ≈ 4
    one pole atω = 100
    i.e., (1 + sT),
    where
    T0 = 1/ω = 1/100
    (1 + 0·01s)
    Hence transfer function, G(s) H(s) = 4/1 + 0·01s
    Hence alternative (C) is the correct choice.


    Correct Option: C

    From figure
    20 log10 K = 12
    K = 1012/20
    or K = 3·98 ≈ 4
    one pole atω = 100
    i.e., (1 + sT),
    where
    T0 = 1/ω = 1/100
    (1 + 0·01s)
    Hence transfer function, G(s) H(s) = 4/1 + 0·01s
    Hence alternative (C) is the correct choice.