Fuzzy Based Power System Stabilizer

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    FuzzyBasedPowerSystemStabilizer

    Abstract - A new type of Power System

    Stabilizer based on fuzzy set theory is

    proposed to improve the dynamic

    performance of a single machine power

    system. To have good damping characteristicover a wide range of operating conditions,

    speed deviation ( ) and acceleration ( ) of

    a machine are chosen as the input signals to

    the fuzzy stabilizer on the particular machine.

    These input signals are first characterized by

    a set of linguistic variables using fuzzy set

    notations. The fuzzy relation matrix, which

    gives the relationship between stabilizer

    inputs and stabilizer output, allows a set of

    fuzzy logic operations that are performed on

    stabilizer inputs to obtain the desiredstabilizer output. In this the effect of

    variations of of defuzzification techniques on

    the performance of FLPSS (fuzzy logic power

    system stabilizer) has been investigated.

    Key words - PSS, Dynamic stability, fuzzy

    based PSS, Single machine infinite bus power

    system.

    I. INTRODUCTION

    Power System Stabilizer (PSS) have beenextensively been used in modern power system

    for enhancing stability of the system. The PSS

    extends system stability limits by modulating

    generator excitation to provide damping to theoscillations of the synchronous machine rotors

    with respect to one another. The conventional

    Power System Stabilizer (CPSS), introducednearly five decades ago, comprising a cascade

    connected lead-lag network with rotor speed

    deviation as input signal has made great

    contributions in enhancing stability of the system[1].

    The conventional fixed structure PSS,designed using a laniaries model provides

    optimum performance for a nominal set of

    operating and system parameters. However, the

    performance becomes sub optimal followingvariations in system parameters and loading

    conditions from their nominal values. [2]-[4].In

    recent years, adaptive self tuning PSS genetic

    algorithm based PSS, artificial neural network

    based PSS and Fuzzy Logic based Power SystemStabilizer (FLPSS) [3-5] have been proposed to

    provide optimum damping to the system

    oscillations under wide variations in systemparameters and operating conditions. An

    adaptive self-tuning PSS suffers from a major

    drawback of requiring model identification in

    real-time, which is possible only with fastmicrocomputers. Although realization of a

    variable structure PSS is simple, it results in

    frequent change over of PSS structure and henceresults in the problem of chattering. In ANN

    based PSS the ANN is trained by using a training

    set obtained from off line studies consideration

    the laniaries model of the system over thecomplete range of operating conditions.

    Thus, the knowledge of the system model isprerequisite for designing ANN based adaptive

    PSS. Fuzzy Logic controllers (FLC) are suitable

    for systems that are structurally difficult tomodel due to naturally existing non-linearity and

    other model complexities. Fuzzy Logic Power

    System Stabilizers unlike other power systemstabilizers do not require a mathematical model

    of the system.In construct to a conventional PSS, which isdesigned in the frequency domain, a fuzzy logic

    PSS is designed in the time domain [4]. The

    fuzzy controllers determine the operating

    conditions from the measured values and selectthe appropriate actions from rules. Depending on

    the system state, the controllers operate in the

    range between no action and full action in anextremely nonlinear manner in order to damp out

    the oscillations. The fuzzy controller in it has no

    dynamic component, i.e. it can immediatelyperform the desired control action.

    II.SYSTEMINVESTIGATEDA machine infinite bus system with

    synchronous generator provided with IEEE

    TypeST1 static excitation system is considered.Nominal parameters of the system are taken from

    ref [6]

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    III. DYNAMICMODELOFTHE

    SYSTEM

    Following assumptions have been made in

    developing the dynamic model of the system.

    1. The mechanical power input remainsconstant during the period of the transient.

    2. Damping or a synchronous power is

    negligible.3. The synchronous machine can be represented(electrically) by a constant voltage source

    behind a transient reactance.

    4. The mechanical angle of the synchronousmachine rotor coincides with the electrical

    phase angle of the voltage behind transient

    reactance.5. If a local load is fed at the terminal voltage of

    the machine, it can be represented by a

    constant independence (or admittance) toneutral.

    The non-linear model of the system is obtained

    as follows

    ( )

    2

    m ed T T

    dt H

    =

    (1)

    02 ( )d

    fdt

    =

    (2)

    11( ) /t R

    dvE V T

    dt

    =

    (3)

    2 [ ]fd fd

    fd fd fd

    adu

    d Ef R R L

    dt L

    =

    (4)

    a linear model of the system is obtained by line

    arising the nonlinear model around a nominal

    operating point(transfer function model is givenin the Fig. (1). The dynamic model of the

    liberalized system in the state space form is

    obtained from the transfer function model in the

    form: X AX p= + &

    (5)

    Where

    1 2

    0

    3 4 3

    3 3 3

    5 6

    02 2 2

    2 0 0 0

    10

    10

    D

    A

    R R R

    K K K

    H H H

    f

    A K K K K

    T T T

    K K

    T T T

    =

    1

    fd

    X

    v

    =

    ,

    1

    2

    0

    0

    0

    H

    =

    ,

    P= [ mT ]

    Fig1.ModelforConstantEfd

    Fig. 2. Shows that transfer function of the systemwith PSS. The linear state space model is given

    in the form

    X AX p= + &

    (6)

    1 2

    3 4 3 3

    3 3 3 3

    5 6

    1 2

    1 51 1 52 1 53 1 55

    2

    2 2 2 2 2

    0 0 02 2 2

    2 0 0 0 0 0

    10 0

    10 0 0

    . . . 10 0

    2 2 2

    10

    D

    A A

    R R R

    STAB D STAB STAB

    R

    K K K

    H H H

    f

    K K K K K K

    T T T T A K K

    T T T

    K K K K K K

    H H H T

    T a T a T a T aT

    T T T T T

    =

    +

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    X =

    2

    1

    fd

    t

    v

    v

    u

    ,

    3

    3

    1

    2

    10

    2

    0 0

    0

    02

    02

    A

    STAB

    STAB

    H

    K K

    T

    K

    H

    T K

    T H

    =

    m

    ref

    Tp

    v

    =

    Fig2.SystemModelwithCPSS

    IV. FUZZYLOGICPSS

    Selection of Input Signals to Fuzzy Logic PSS:For the present investigations generators

    speed deviation ( ) and acceleration ( ) arechosen as the input signals to the FLPSS.

    In practice, only shaft speed deviation ( ) isreadily available. The acceleration ( ) isderived from the measured at twosuccessive sampling instants

    (KT) =( ) [( 1) ]KT K T

    T

    Where T is the sampling period.

    SelectionofLinguisticVariables:The number of linguistic variables

    determines the quality of the control, which canbe achieved using Fuzzy Logic Controllers. As

    the numbers of linguistic variables increases, the

    quality of control improves at the cost of

    increased computational time and computermemory. A compromise is needed between the

    two. For the power system under study, seven

    linguistic variables for each of the inputs and the

    output signals are considered. These seven

    linguistic variables are PB (positive big), NS(negative small), NM (negative medium) and NB

    (negative big). A choice of 7 linguistic variables

    results in a set of 49IF-THEN rules (Table.1)shows the decision table. This table is obtained

    from the expert knowledge of the operators.

    In order to obtain the minimum and themaximum values of the stabilizer inputs thedynamic performance of the system without PSS

    is obtained for different magnitudes of

    perturbations. After choosing the linguisticvariables, it is required to determine the

    membership functions for these linguistic

    variables. Generally gauss Ian, triangular ortrapezoidal membership functions are prevalent.

    Here triangular membership function is used to

    define the degree of membership (Fig. 3.).Degree of membership plays a very important

    part in designing a fuzzy controller.

    Fig3.SymmetricalTriangularMembership

    function

    Now it is required to find the fuzzy regionfor the output for each fuzzy rule, for which

    Madman implication is used.

    Decisiontable1.

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    1

    Fig4.SystemModelwithFLPSS

    V COMPARISON OF PERFORMANCE OF

    THESYSTEMWITHCPSSANDFLPSS

    Fig. 5 and 6 shows the transient response

    for and respectively following a 5 % stepchange in mechanical torque with conventionalPSS and FLPSS obtained considering a linear

    model of the system. The scaling factors for

    and.

    the stabilizing signals are respectively

    5000, 350 and 500. Examination of the responses

    clearly shows that dynamic performance of the

    system with FLPSS is very close to that withconventional PSS and is in fact slightly better in

    terms of settling time. Further, in order to

    compare the dynamic performancesquantitatively a quadratic performance index is

    evaluated

    2 2

    00[ ( )] [ ( )]

    kJ t kt t

    == =

    Fig5.SpeeddeviationVsTimeTable 2. Shows the value of J for CPSS and

    FLPSS.it also shows the peak overshoot of the

    dynamic response for and . COGdefuzzifier has been used and symmetrical

    triangular membership functions with equal basewidths have been considered.

    Table2

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    Fig.6. Rotor angle deviation Vs

    Time

    VI. EFFECT OF VARIATION IN

    COORDINATES OF MEMBERSHIP

    FUNCTIONAn attempt has been made towards gain

    tuning of the fuzzy logic controller by altering

    the coordinates of the membership functions.

    Center of Gravity / Area (COG/COA) defuzzifieris used in the analysis.

    Fig.7 shows a triangular membership

    functions, , , are the coordinates of the

    function. denotes the left coordinate of the

    base denotes the abscissa of the peak and

    denotes the right coordinates of the base. Let 1 ,

    2 and 3 be the X coordinates of the peaks of

    the membership functions PS, PM and PB

    respectively.

    For the membership functions PS let 1c = 1

    For the membership functions PM let y = 2 -

    1

    For the membership functions PB let

    z = 3 - ( 1 + 2 )

    =3-(y + 1c )

    Fig.7.

    Fig.8.Trangular Membership Function

    At this stage, we assume that the separation

    between the peaks vary in geometric ratio i.e.

    1

    y z

    c y= .It can be clearly seen from Fig (9) that

    the coordinates of PS, PM and PB are1 2 1 2 3(0, , ), ( , , ) and 2 3( , ,...) . 3 =3.0,

    the positive limit of the universe of discourse(universe of discourse is 3.0 to 3.0.

    The value of 1c is varied over a wide

    range in order to obtain its optimum value. Figs.(9) and Fig(10) show the transient response for

    and for a step increase in mechanicaltorque i.e. Tm = 0.05 pu for 1c = 1.2,1.0 and0.4.Examination of the responses shows that the

    maximum peak overshoot is nearly the same for1c = 1.2and 1c = 1.0 and increases slightly for1c = 0.4 whereas there is considerable reduction

    in setting time as 1c is reduced to 0.4 whereasthere is considerable reduction in setting time for

    1c is equal to 0.4.Examination shows that the

    performance index J decreases slightly while thesettling time decreases to about 50% with change

    in 1c from 1.2 to 0.4.The change in peak

    deviation is quite insignificant.Fig. 9.Speed deviation Vs Time

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    Fig.10. Rotor angle deviation Vs Time

    VII CONCLUSION

    A systematic approach for realizing Fuzzy

    Logic PSS has been presented. An attempt hasbeen made to study the effect of variation of co-

    ordinates of the membership functions and

    scaling factors on performance of the FLPSS.

    Performance of the FLPSS has been comparedwith CPSS. Following are the significant results

    of the investigations carried out in this paper:

    1. Performance of an optimum conventionalPSS is similar to that of FLPSS.

    2. Unsymmetrical triangular membership

    functions with 1c = 0.4 provides the bestdynamic performance of the FLPSS.

    3. The scaling factors decrease inversely withincrease in magnitude of perturbation.

    4. FLPSS using adaptive scaling factors provide

    good performance.