88324 control system mid term2008

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  • 8/9/2019 88324 Control System Mid Term2008

    1/3

    Solution to Mid-term

    1)

    1)

    3 65 1 1 5( ) ( ) ( ) ( )

    3 3 6 3

    9 3, 3 2, 1.06

    2*3 2 2 2

    t t

    n

    F s f t e es s

    overdamped

    = =

    + +

    = = = =

    2)

    2 2 2 2

    1( ) (sin 5 sin )

    2

    1 5( ) ( )

    2 25

    f t t t

    F s

    s s

    =

    =

    + +

    Two under-damped components

    3)

    6 1144 12, 0.25

    2*12 4n

    underdamped = = = = =

    Note that

    2 2

    3

    20 20 135( )

    ( 3) 135 ( 3) 135135

    20( ) sin 135

    135

    t

    F ss s

    f t e t

    = =+ + + +

    =

    4)

    2 2

    2( )

    9 9

    2( ) cos3 sin 3

    3

    sF s under damped

    s s

    f t t t

    = + + +

    = +

    5)

    2

    4

    2 2

    ( ) 10( ) 5( ) 8 25

    8 80.8

    2*5 10

    10 3 10( ) ( ) sin 3

    3 ( 4) 3 3

    n

    t

    X sF sU s s s

    underdamped

    F s f t e t s

    = = =+ +

    = = =

    = =+ +

  • 8/9/2019 88324 Control System Mid Term2008

    2/3

    2) Note that

    50b t t

    a a

    K K KT gives

    R R= +

    0 100T= = (See figure), so

    100 50

    0 150, : 150 50 0

    t

    a

    b t t

    a a

    K

    R

    K K KT so

    R R

    =

    = = + =

    we have :

    13

    1

    6

    t b

    a

    K K

    R

    = =

    =

    1) Since

    '

    1 1( ) ( ) ( )

    6 3

    1 50 1( ),

    3 150 3

    1(18* ( ) 36 ( )) 2*3 ( ) 2*3 ( )3

    a a

    a

    f f L L L L

    E s I s s

    T I s N

    T T T NT T s s s s s s

    = +

    = = =

    = = + = +

    So

    (6 6) ( ) 6 ( ) 12 ( )

    (12 18) ( ) (12 18) ( )

    L L L

    L L

    T s s s s s

    s s s s s

    = + + +

    = + = +

    and

    ( ) 3 (12 18) ( )

    1 1 1( ) 3 (12 18) ( ) 3 ( ) (12 18) ( )

    6 3 2( ) 1

    ( ) (6 10)

    a L

    a L L L

    L

    a

    I s s s s

    E s s s s s s s s s s

    s

    E s s s

    = +

    = + + = + +

    =+

  • 8/9/2019 88324 Control System Mid Term2008

    3/3

    2) For

    5

    3

    ( ) ( ) 1

    1 1 6( )

    (6 10) 10 10(6 10)

    ( ) 0.1(1( )) 0.1

    a a

    L

    t

    L

    e t E s

    ss s s s

    t t e

    = =

    = = + +

    =

    3)

    1) Note for 0ref = , we have :

    1( ) 0.5 1

    10 1( ) (0.5 1)( ) 101

    0.5 1

    ms s Js b

    kp D s s Js b kp

    s Js b

    ++= =

    + + ++

    + +

    when1

    ( ) , ( ( ) 1( )) D s D t t s

    = =

    1 0.5 1( )

    (0.5 1)( ) 10m

    ss

    s s Js b kp

    + =

    + + +

    so0

    1 1( ) lim ( )

    10 1 10m m

    ss s

    b kp kp = = =

    + +

    2) For D(t)=0, then

    ( ) 1

    10( )1

    (0.5 1)( )ref

    E s

    kps

    s Js b

    =+

    + +

    1 1( )

    101

    (0.5 1)( )

    E skps

    s Js b

    =

    ++ +

    for1

    ( ) , ( ) 1( )ref ref s t ts

    = =

    0

    1( ) lim ( )

    1 10se sE s

    kp = =

    +

    Obviously, the disturbance will incur a comparable error in the tracking error at the steady state.