1314sem1finalexam_soln-cntrl

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    SEE 3113

    Question 1

    a)

    i) The exponential term increases indefinitely

    ii) No. That will only be the case if there is no sign change from ROZ

    downwards.

    iii) The system is unstable

    b)

    i) The system is unstable because of the negative sign occurred in the

    characteristic equation.

    ii)

    S5 1 4 3

    S4 -1 -4 -2

    S3 1 0

    S2

    41

    -2 0

    S1

    41

    412 2

    +

    0 0

    S

    0

    -2 0 0

    3 right hand-plane, 2 left hand-plane. The systemis unstable.

    c) Since the system oscillates, it is marginally stable. The characteristic equation

    of the system becomes:

    1 +( + 2)

    3 +

    2 + 3

    + 2

    = 0

    Or 3 + 2 + ( + 3) + 2( + 1) = 0

    Rouths

    s3

    1 K+3

    s2

    p 2(K+1)

    s1

    (

    + 3)

    2(

    + 1)

    0

    s0

    2(K+1)

    1

    1

    1

    3

    3

    1

    2

    2

    1

    1

    2

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    SEE 3113

    At marginal value of K (+3)2(+1) = 0Or

    =2(+1)+3

    Again at this value of p,

    () =2 + 2( + 1) = 0Or

    2 =2( + 1) = 2( + 1)

    Given =2.5rad/sec. Therefore:

    2(+1) = 2.5[1mark]

    = 2( + 1)6.25

    Substitute equation (1) into (2)2(+1)+3 =2(+1)6.25 K=3.25Therefore

    p=2(3.25+1)/6.25= 1.36

    (2)

    1

    1

    2

    2

    1

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    SEE 3113

    Question 2

    a)

    By looking at the locations of the open loop poles and zeros. If there are some

    on the LHP and some on the RHP, so the root locus will cross the imaginary

    axis.

    b)

    ()() = (+1)(+5)(+1)+(62)+5+2Then,

    s2 K + 1 5K + 2

    s1 6K 2 0

    s0 5K + 2 0

    Therefore K > 0.333

    From auxiliary equation and substituting K = 0.333,

    43 2 +113 = 0 = 1.66

    c)

    i. K = 0: closed loop poles = 1+j ; 1-j

    ii. K -> infinity: closed loop poles = -1 ; -5

    iii. 2 branches

    iv. symmetrical about real axis

    v. no asymptote angle

    vi. no asymptotes crossings

    vii locus on real axis : between -5 and -1

    viii Departure angles = 180 90 + 26.6 + 9.5 = 126.1

    ix jw-crossings : from part (b), s =1.66x

    . (+1)(+5)(2+2) = 0solving this will obtain 1.325 and -2.075so the break-in point is at -2.075

    therefore the root locus:

    2

    1

    1.5

    1.5

    2

    1

    1

    2

    1

    2

    1

    2

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    SEE 3113

    d)

    From the root locus, if the damping ratio is 0.6

    the dominant poles are at

    1.13

    1.52

    and the value of K = 1.14

    -5 -4 -3 -2 -1 0 1-2

    -1.5

    -1

    -0.5

    0

    0.5

    1

    1.5

    2

    Root Locus

    Real Axis

    ImaginaryAxis

    2

    2

    3

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    SEE 3113

    Question 3

    a)

    b) A vehicle speed control system is shown in Figure Q3b.

    2

    11

    2

    2

    0.5

    1

    0.5

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    SEE 3113

    c) Roughly sketch the root locus of the uncompensated and compensated systems

    in part (b) above.

    5

    2

    2

    1

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    SEE 3113

    2.5

    2.5

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    SEE 3113

    Question 4

    a)

    i) A measurement of output response of a system in frequency domain. The

    output response consists of the magnitude and phase values as the

    frequency is varied.

    ii) By obtaining the gain margin and phase margin. The system is said to

    stable if the gain and phase margins are positive.

    b)

    i) By using the straight line approximation methods, plot the Bode plot of the

    open-loop system for K= 1.

    ii) Gain Margin = 53.2 dB

    Phase Margin = 91.6

    iii)Stable. Positive values of GM and PM

    iv)The value of gain Kneeded is 40.3 dB

    -200

    -150

    -100

    -50

    0

    50

    Magnitude(dB)

    10-2

    10-1

    100

    101

    102

    103

    104

    -270

    -225

    -180

    -135

    -90

    -45

    Phase(deg)

    Bode Diagram

    Frequency (rad/sec)

    1.5

    1.5

    7

    7

    1

    1

    2

    2

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    SEE 3113

    v)

    Bode Diagram

    Frequency (rad/sec)

    10-2

    10-1

    100

    101

    102

    103

    104

    -270

    -225

    -180

    -135

    -90

    -45

    System: G1

    Phase Margin (deg): 44.6

    Delay Margin (sec ): 0.0652

    At frequency (r ad/sec): 11.9

    Closed Loop Stable? Yes

    Phase(de

    g)

    -150

    -100

    -50

    0

    50

    100

    System: G1

    Gain Margin (dB): 12.9

    At frequency (r ad/sec): 27.2

    Closed Loop Stable? Yes

    Magnitude(dB) 2

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    SEE 3113

    Question 5

    a)

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    SEE 3113

    b)