Reporte 7 Lugar Raices

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    Abstract In this paper is presented the geometric place of

    poles and zeros of three transfer functions using the Root Locus

    Analysis Method. Also is presented a brief analysis using the

    Ruth-Hurwitz theorem to determine critical stability points.

    I. NOMENCLATURE

    G(S) = Transfer Function.

    = Zero.=Poles.= Angle of the Asymptote.

    = Friction Coefficient.

    K= Gain

    II. INTRODUCTION

    f we consider the Closed Loop (CL) System like the shown

    in figure 1, we can de observe that many of its

    characteristics are determined by the CL poles. The CL poles

    are the roots of the characteristic polynomial. To find the

    roots, we must factorize the equation, but sometimes, this can

    be very laborious. The Root Locus Analysis its a graphic

    method that we can use to approach the poles place of the

    system at any K gain parameter in the system.

    Fig. 1.

    III. ROOT LOCUS METHOD

    To graphically determine the roots place, we need to follow

    the next steps:

    1. The graph will have N branches, where N isthe number of poles of the CL system.

    2. Draw the poles and zeros in a Cartesian coordinatesystem, where the X axis represent the Real

    numbers and Y axis the imaginary numbers. If

    there is less zeros than poles, we consider that the

    missing zeros have infinite magnitude. The

    branches always go from poles to zeros.

    3. Determine if there exist root place in the real axis.To the left of an impair number of zero/pole, it

    exist the root place. Fig. 2.

    Fig. 2.

    4. The branches that do not tend to the zeros of CL,tend asymptotically to the zeros with infinite

    magnitude. So we calculate the angle of the

    asymptote () by using:

    5. The point in the real axis in which asymptote begin(Fig.3) is defined by:

    Fig. 3.

    6. We must calculate all the input/output angle for allthe pole/zero of interest, and then solve from the

    phase condition:

    Where:

    Root Locus AnalysisProfessor: Dr. Luis Amzquita Brooks, Control Engineering, CIIIA-UANL,

    Student: Lic. Fernando Guerrero Vlez, CIIIA - UANL

    I

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    If and input/output angles are in the wrongdirection (This is, if the output angle of a pole arent pointing to the zero direction), we mustadd 180 to

    and

    .

    7. Calculate the input/output points from the real axisusing the Closed Loop Denominator (CLD), where

    the values of K remain real, this is, considering the

    CL system:

    Then:

    Where, the real solutions of the following

    equation:

    (

    )

    Are the input/output points that were looking for.

    8. Finally, we must calculate the point where theasymptote of CLD cross over the imaginary axis

    (Critical Stability), by using the Routh-Hurwitz

    Stability Criterion.

    IV. EXAMPLE PROBLEMS

    Solve the following problem using the Root Locus Method.

    a)

    Step 1:If we rewrite G(s) as:

    Then we can observe that exist 3 poles

    and 2 zeros. Thus, exist 3 branches.

    Step 2-3:Drawing the poles/zeros and finding the

    root place.

    Fig. 4.Where:

    Step 4:

    Step 5:

    Then, the graphic is:

    Fig. 5.

    Step 6:Input angles to Z1:

    () ( ) () ()

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    Using the phase condition:

    Then:

    Now, obtaining the output angles of :

    ( ) ( )

    () ()

    ( )

    Using again the phase condition, then we

    find:

    Step 7:To find the input/output point from real

    axis, then:

    (

    )

    Then, finding the numerator roots:

    So, the output point from the real axis is

    located in (-0.53,0). Finally the graphic is:

    Fig. 6.

    Step 8:Using Routh-Hurwitz to calculate the

    imaginary axis cross point:

    Where:

    That lead to the following values of k:

    b)

    Step 1:If we rewrite G(s) as:

    Then we can observe that exist 4 poles

    and 2 zeros. Thus, exist 4 branches.

    Step 2-3:Drawing the poles/zeros and finding the

    root place.

    Fig. 7.

    Where:

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    Step 4:

    Step 5:

    Then, the graphic is:

    Fig. 8.

    Step 6:Input angles to Z1:

    () () ( ) ( )

    Using the phase condition:

    Then:

    Now, obtaining the output angles of :

    ( )

    ()

    Using again the phase condition, then we

    find:

    Step 7:To find the input/output point from real

    axis, then:

    (

    )

    Then, finding the numerator roots:

    So, the output point from the real axis is

    located in (-8.24,0). Finally the graphic is:

    Fig. 9.

    Step 8:Using Routh-Hurwitz to calculate the

    imaginary axis cross point:

    Where:

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    Finally, the values of kmust be:

    c)

    Step 1:If we rewrite G(s) as:

    Then we can observe that exist 4 poles

    and 2 zeros. Thus, exist 4 branches.

    Step 2-3:Drawing the poles/zeros and finding the

    root place.

    Fig. 10.

    Where:

    Step 4:

    Step 5:

    Then, the graphic is:

    Fig. 11.

    Step 6:Because a pole always must end in a zero,

    and because we have the poles/zeros

    arranged in pair, then we can note that the

    pair of poles P3,P4will show a trajectory

    starting among themselves, and ending

    between the pair of zeros. The pair of

    poles P1,P2 will approach to the asymptote

    in (-4,0), to end in the zeros at theinfinite. This is, the input/output angle for

    de poles P3,P4 and the zeros Z1,Z2 are

    multiples of 180. The input/output point

    of these trajectories will be calculated in

    step 7.

    Step 7:To find the input/output point from real

    axis, then:

    (

    )

    Then, finding the numerator roots:

    So, the output point from the real axis is

    located in (1.45,0) and (-6.95,0), the input

    point is located in (-1.92,0). Finally thegraphic is:

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    Fig. 12.

    Step 8:Using Routh-Hurwitz to calculate the

    imaginary axis cross point:

    Where:

    Finally, the values of kmust be:

    V. RESULTS AND CONCLUSIONWe are now presenting the plots obtained for the following

    parameters:

    g = 9.8

    l = 2

    m = 1

    M = 3

    b = 0.3

    As wee see in the past plots, the pendulum exhibit a

    sinoidal behavior, and it tends to be in its acceleration,

    velocity and position equilibrium state.

    VI. REFERENCIAS

    [1] Dinmica de Sistemas, Katsuhiko Ogata, !era edicin en Espaol