88324 control system mid term2007

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  • 8/9/2019 88324 Control System Mid Term2007

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    88-324Mid-Term Test Summer 2007

    Name: Student Number:

    1.(30) Given a differential equation

    y + 3y + 2y = r(t), y(0) = a, y(0) = b,

    where a and b are constants,

    a)(10). Assuming that the input signal is a unit step signal: r(t) = 1(t), find the expression of the

    output signal y(t).

    Note that

    s2Y(s) as b + 3sY(s) 3a + 2Y(s) = R(s), Y(s) =as + b + 3a

    s2 + 3s + 2

    1

    s2 + 3s + 2R(s)

    If r(t) = 1(t), then R(s) = 1/s, so

    Y(s) =as + b + 3a

    s2 + 3s + 2+

    1

    s(s2 + 3s + 2)=

    2a + b

    s + 1+

    a + b

    s + 2+

    1

    2s

    1

    s + 1+

    1

    2(s + 2)

    So

    y(t) = (2a + b 1)et + (a + b +1

    2)e2t +

    1

    2.

    b)(10). Find the final value of limt

    y(t) when r(t) = (t), i.e., a unit impulse signal.

    If r(t) = (t), then we have R(s) = 1. So

    Y(s) =

    as + b + 3a

    s2 + 3s + 2 +

    1

    s2 + 3s + 2 , limt y(t) = lims0 sY(s) = 0

    c)(10). Assuming that a = b = 0, show that the unit-impulse response in (b) is the derivative of the

    unit-step response in (a).

    Note that in this case, for r(t) = (t), we have

    Y(s) =1

    s2 + 3s + 2=

    1

    s + 1

    1

    s + 2y(t) = et e2t

    and for r(t) = 1(t), we can obtain from (a) that

    y(t) = et +1

    2e2t +

    1

    2

    Obviously,

    d

    dt(et +

    1

    2e2t +

    1

    2) = et e2t.

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    2.(30) Given an electric network shown in the following Figure:

    The equations describing this network are stated as follows:

    R1i1 + Ld(i1 i2)

    dt= v,

    R2i2 + vc + Ld(i2 i1)

    dt= 0

    i2 = Cdvcdt

    ,

    where v(t) is a voltage source.

    a)(15). Derive transfer functions from v(s) to i1(s).

    Applying Laplace transformation to the equations above, we obtain

    R1i1(s) + sL(i1(s) i2(s)) = v(s), R2i2(s) + vc(s) + sL(i2(s) i1(s)) = 0, i2(s) = sCvc

    So i1(s)v(s) can be solved as

    i1(s)

    v(s)=

    LCs2 + R2Cs + 1

    (R1 + R2)LCs2 + (R1R2C+ L)s + R1

    b)(15). Let v(s) = 1/s. Find the steady state current limt i1(t) and limt i2(t).

    Now if v(s) = 1/s, i.e., v(t) = 1(t), then

    i1(s) =LCs2 + R2Cs + 1

    s [(R1 + R2)LCs2 + (R1R2C+ L)s + R1]

    Solimt

    i1(t) = lims0

    si1(s) =1

    R1

    Note that, if i1() =1R1

    , then vR1() = 1 = v(t). Therefore vL() = 0 and hence

    limt i2(t) = 0.

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    3.(40) A armature-controlled dc servomotor system is shown in the following figure

    where Ra = 1, La 0, ke = kt = 0.5, n =N1N2

    = 20, JL = 100kg m2, and DL = 100Nm

    s/rad. This system can be described by following equations:

    ea = Raia + kem, Tm = ktia, L = nm,1

    nTm = JLL + DLL

    where Tm is the torque generated by the motor.

    a)(20). Find transfer function model for this electro-mechanical system from ea to L and L.

    Note that, after implementing the values given, the Laplace transformed equations are

    ea(s) = ia(s) + 0.5sm(s), Tm = 0.5ia(s), L(s) = 20m(s),1

    20Tm = 100s

    2L(s) + 100sL

    Therefore, L(s)ea(s)

    and L(s)ea(s)

    can be solved as

    L(s)

    ea(s)

    =1

    s(4000s + 4000.025)

    ,L(s)

    ea(s)

    =1

    4000s + 4000.025b)(20). Let ea(t) = 1(t)v be a unit-step testing signal. Find the motor shaft angle L(t).

    If ea(t) = 1(t)v, then ea(s) = 1/s. Note that 4000.025/4000 1. So

    L(s) =1

    s2(4000s + 4000.025)=

    1

    4000s2

    1

    4000s+

    1

    4000(s + 1)

    and

    L(t) =1

    4000t

    1

    4000+

    1

    4000et.