Control and Intr 2 Indika

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  • 8/3/2019 Control and Intr 2 Indika

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    Part a

    )11.0)(1(

    10

    )(

    )()( 0

    ++==

    sssV

    swsG

    ++==sT

    sssE

    sVsG

    c

    106.01

    )(

    )()(

    As we know

    ++

    ++==

    sTs

    sssGsGsG

    cOL

    106.015

    )11.0)(1(

    10)()()(

    ++

    ++=

    sT

    TssT

    ss

    106.05

    )11.0)(1(

    10 2

    sTss

    sTTs

    )11.0)(1(

    )106.0(50 2

    ++

    ++=

    sTss

    sTTs

    )11.11.0(

    505032

    2

    ++

    ++=

    sTTsTs

    sTTssG

    OL ++++

    =23

    2

    1.11.0

    50503)(

    As we know)(1

    )()(

    sG

    sGsG

    OL

    OL

    CL +=

    sTTsTs

    sTTs

    sTTsTs

    sTTs

    sGCL

    ++++

    +

    ++++

    =

    23

    2

    23

    2

    1.11.0

    505031

    1.11.0

    50503

    )(

    505031.11.0

    50503223

    2

    +++++++

    =sTTssTTsTs

    sTTs

    50511.41.0

    50503)( 23

    2

    +++ ++= sTTsTssTTs

    sGCL

    1

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    Characteristics Equation 0)()(1 =+= sHsGK

    Characteristics Equation 050511.41.0 23 =+++= sTTsTs

    Dividing all terms by sTTsTs 511.41.0 23 ++

    0511.41.0

    50

    511.41.0

    511.41.02323

    23

    =++

    +++++

    =sTTsTssTTsTs

    sTTsTs

    [ ]0

    511.41.0

    501

    23=

    +++=

    sssT

    0511.41.0

    5011

    23=

    ++

    +=

    sssT

    TK

    1=

    Commands

    >>sys=tf([50],[0.1 4.1 51 0])

    >>rlocus(sys)

    Graph 1

    From Graph 1 it can be noted:

    At damping of 0.7

    2

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    Gain = 6.05 K = 6.05

    Therefore sK

    T 165.005.6

    11===

    Pole = -7.51+7.66i

    Part b

    Put T = 0.165 in GCL(s)

    50)165.0(51)165.0(1.4)165.0(1.0

    50)165.0(50)165.0(3)(

    23

    2

    +++

    ++=

    sss

    sssG

    CL

    50415.86765.00165.05025.8495.0)(

    23

    2

    +++ ++= ssssssG

    CL

    Commands

    >>sys=tf([0.495 8.25 50],[0.0165 0.6765 8.415 50])

    >>step(sys)

    Graph 2

    From Graph 2:

    Rise Time Tr= 0.0506s

    3

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    % Overshoot = 13.7

    Settling Time Ts = 0.339s

    Final Value = 1

    From Graph 2: % Overshoot = 13.7

    % Overshoot 1001

    exp2

    =

    =

    21

    exp

    100

    7.13

    21)137.0ln(

    =

    2

    2

    2

    1)99.1(

    =

    2

    22

    195.3

    =

    22295.395.3 =

    )5.9(95.3 22 +=

    286.0)95.3(

    95.32

    2 =+

    =

    Damping ratio: 535.0=

    n

    st

    = 4

    n

    st

    =

    535.0

    4

    Settling time: sts 339.0=

    n

    =535.0

    4339.0

    4

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    4535.0339.0 =n

    Natural frequency:535.0339.0

    4

    =

    n

    sradn /1.22=

    Frequency of oscillation: 21 =nd

    2)535.0(11.22 =

    845.01.22 =

    sradd

    /67.18=

    As Final value = 1, so the ess must be zero.

    Calculations

    Plotting pole -7.51+7.66i on the graph

    22266.751.7 i

    n+=

    222 )66.7()51.7( +=n

    1.1152 =n

    Natural frequency: sradn /72.10=

    Poles can be written as dn wws =

    5

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    nw=51.7

    Damping ratio: 7.0=

    % Overshoot 1001

    exp2

    =

    100)7.0(1

    7.0exp

    2

    =

    % Overshoot 6.4=

    n

    st

    =

    4

    72.107.0

    4

    =

    st

    Settling time: sts 533.0=

    Frequency of oscillation: 21 =nd

    2)7.0(172.10 =

    71.072.10 =

    sradd

    /66.7=

    ( )[ ])(1)(lim0

    sGsRseCL

    s

    s s=

    As the system is step response R(s) =s

    1

    +++

    ++=

    50415.86765.00165.0

    5025.8495.01

    123

    2

    0lim

    sss

    ss

    sse

    s

    ss

    50

    501=

    sse

    Steady State Error 0=sse

    6

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    The table below shows the results estimated in part b and results from the

    calculations.

    Discussion and Conclusion

    Estimates from Part b Calculation Results

    Damping ratio 0.535 0.7

    % Overshoot 13.7% 4.6%

    Settling Time st 0.339s 0.533s

    Natural frequencyn

    22.1 rad/s 10.72 rad/s

    Frequency of oscillation

    d

    18.67 rad/s 7.66 rad/s

    Steady State Error ess 0 0

    From the table above it can be seen that as the damping ratio is decreased in

    part b, this causes and increase in frequency of oscillation of the system causing it to

    settle quicker. In calculation results, damping ratio used was restricted not to be any

    lesser than 0.7. The reason for this restriction could be to prevent it to oscillate withhigher frequency causing the system to fail. This system shows an under-damped

    response which is stable as the function is reaching a steady state value of 1. This is

    not sustained oscillation so increase the gain until the point of instability is reached.

    7