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    Root Locus MethodRoot Locus Method446446--2020

    Prof. Neil A. DuffieProf. Neil A. DuffieUniversity of WisconsinUniversity of Wisconsin--MadisonMadison

    Neil A. Duffie, 1996 Neil A. Duffie, 1996

    All rights reservedAll rights reserved

    2020 22

    Importance of Pole LocationImportance of Pole Location

    Performance is a function of pole locationPerformance is a function of pole location

    -- transient responsetransient response

    -- absolute stability (stable or not?)absolute stability (stable or not?)

    -- relative stability (how stable?)relative stability (how stable?)

    Poles migrate as control parameters varyPoles migrate as control parameters vary

    -- function of controller gains, zeros, polesfunction of controller gains, zeros, poles

    -- what values produce good locations?what values produce good locations?

    -- design (place poles) using root locusdesign (place poles) using root locus

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    Transient ResponseTransient Response

    Re

    Im

    00

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    Absolute StabilityAbsolute Stability

    00

    Stable regionStable region(negative real parts)(negative real parts)

    Unstable regionUnstable region(non(non--negativenegative

    real parts)real parts)

    ImIm

    ReRe

    left 1/2left 1/2--planeplane

    2020 55

    RouthRouth--Hurwitz Stability CriterionHurwitz Stability Criterion

    Rouths criterion is a method forRouths criterion is a method for

    assessing stability without finding roots.assessing stability without finding roots.

    The method is tabular, finds the numberThe method is tabular, finds the number

    of roots with positive real parts, and isof roots with positive real parts, and is

    described in most controls textbooks.described in most controls textbooks.

    The method was developed in the lateThe method was developed in the late

    1800s when finding roots was difficult.1800s when finding roots was difficult.

    Powerful calculation tools on the desktopPowerful calculation tools on the desktop

    have made the method less useful.have made the method less useful.

    Review it at a high level at this point.Review it at a high level at this point.

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    Characteristic EquationCharacteristic Equation

    ProcessProcessControlControl

    ++--

    R(s)R(s) C(s)C(s)E(s)E(s) M(s)M(s)GGcc(s)(s)

    C(s)C(s)

    GGpp(s)(s)

    System transfer function:System transfer function:

    Characteristic equation:Characteristic equation:

    D(z) =1 +Gc(s)Gp(s) = 0

    C(s)

    R(s)= Gc (s)Gp (s)

    1+ Gc (s)Gp (s) =N(s)

    D(s)

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    Signs in Characteristic EquationSigns in Characteristic Equation

    All coefficients of characteristic equation:All coefficients of characteristic equation:

    -- must have the same signmust have the same sign

    -- must be nonmust be non--zerozero

    Necessary (but not sufficient) condition forNecessary (but not sufficient) condition for

    absolute stability (from Rouths Criterion)absolute stability (from Rouths Criterion)

    Examples:Examples:

    ss33 + 2s+ 2s22 + s + 5 = 0+ s + 5 = 0 (may be stable)(may be stable)

    ss33 + 2s+ 2s22 -- s + 5 = 0s + 5 = 0 (unstable)(unstable)

    ss33 + 2s+ 2s22 + 5 = 0+ 5 = 0 (unstable)(unstable)

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    Relative StabilityRelative Stability

    How stable is a system?How stable is a system?

    -- compared to another systemcompared to another system

    -- distance to the border of instabilitydistance to the border of instability

    Measures of relative stabilityMeasures of relative stability

    -- damping associated with each rootdamping associated with each root

    -- real parts of rootsreal parts of roots

    -- gain and phase marginsgain and phase margins

    (frequency response concept:(frequency response concept:study later)study later)

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    Relative StabilityRelative Stability

    ReRe

    ImIm

    00ReRe

    ImIm

    00

    11

    22

    dd11 dd22

    SystemSystem

    #1#1SystemSystem

    #2#2

    11 > 22))dd11 < d< d22

    System #2 is relatively moreSystem #2 is relatively more

    stable than System #1!stable than System #1!

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    Step Response of Systems #1 and #2Step Response of Systems #1 and #2

    System #2System #2

    System #1System #1

    System #1:System #1:

    -- is relatively less stable than System #2is relatively less stable than System #2

    -- has more oscillatory step responsehas more oscillatory step response

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    Root LocusRoot Locus

    Definition: The root locus is the path of theDefinition: The root locus is the path of the

    roots of the characteristic equationroots of the characteristic equation

    plotted in the splotted in the s--plane as a systemplane as a system

    parameter is changed.parameter is changed.

    Design: Choose a parameter value forDesign: Choose a parameter value for

    which the locus lies in a good area ofwhich the locus lies in a good area of

    the sthe s--plane (where dynamics meet specs).plane (where dynamics meet specs).

    Iteration: If no part of the root locus lies inIteration: If no part of the root locus lies in

    a good area of the sa good area of the s--plane, then changeplane, then change

    the structure of the controller to modifythe structure of the controller to modifythe locus. Then choose parameter value.the locus. Then choose parameter value.

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    Root Locus of 3Root Locus of 3rdrd--Order SystemOrder System

    k < 2:k < 2: > 1> 1k > 2:k > 2: < 1< 1k < 30: stablek < 30: stable

    k > 30: unstablek > 30: unstable

    --66 --44 --22 00 44 66--66

    --44

    --22

    22

    44

    66

    ReRe

    ImIm

    00

    22

    G(s) = ks s + 3) s + 2) C(s)R(s) = ks s + 3) s + 2)+ k

    00 00 00

    3030

    3030

    3030 2222

    300300

    300300

    3003003.53.5

    3.53.53.53.5

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    Choice of k forChoice of k for = 0.707= 0.707

    --66 --44 --22 00 44 66--66

    --44

    --22

    22

    44

    66

    ReRe

    ImIm

    00

    22

    00 00 00

    3030

    3030

    3030 2222

    ForFor = 0.707:= 0.707:k 3.5k 3.5

    300300

    300300

    3003003.53.5

    3.53.53.53.5

    4545

    G(s) = ks s + 3) s + 2) C(s)R(s) = ks s + 3) s + 2)+ k

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    Unit Step Response for k = 3.5Unit Step Response for k = 3.5

    00 11 22 33 44 55 66 77 88 99 101000

    0.20.2

    0.40.4

    0.60.6

    0.80.8

    11

    1.21.2

    c(t)c(t)

    tt

    0.707 0.707