Power System Dynamic Load Identification and Stability

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    Power System Dynamic Load Identification and Stability

    S.

    Z.

    Zhu* Z. Y. Dong** K. P.

    Won

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    loads. Given wl , w2 nd w3 as the weighting factor of

    each compone nt, the compos ite load is represented as

    L

    = wlLs

    + w2LG+ w3LIM, ith C

    w

    = 1

    (2.1)

    The values of wl ,

    w

    and w vary for different load buses

    depending on their load compositions. For a load with

    high concentration of industrial components, for example,

    a larger value of w may be assigned.

    Here we describe the loads and their aggregated

    characteristics that significantly present voltage

    sensibility. Details of the load m odeling are as follows,

    (1) The static load is modeled as an exponential function

    of voltage V

    Pd = POCf Qd = QO ( f

    (2.2)

    where Po, Qo are static load consumptions at the rated

    voltage

    Vo.

    The indices

    a

    and p are the parameters

    chosen to best represent the voltage dependence of the

    aggregate load, and normally have a range of a = 0.5 -

    1.8,

    p

    =1.5 - 6 according to Kundur [8]. Xu et al.

    Proposed

    a =

    0.31 - 1.50, p = 2.22 - 4.18 based on the

    field test in [8]. The general trend is that, high

    concentration of residential load exhibits larger

    a

    and

    smaller

    p;

    while high concentration of commercial /

    industrial loads exhibits smalle r and larger

    p

    [8] and [9].

    For

    example, their values can be chosen as a = 0.8 - 1.5,

    p = 2.0

    - 4.0 for

    each bus depending on the load

    composition. However these static load models neglect

    the critical important dynamic behavior exhibited by

    many loads.

    (2) A number of generic dynamic load models have been

    proposed recently in the literature for voltage stability

    studies, see

    -

    [SI, [6], [lo] and [SI.

    A

    first-order dynamic

    recovery model proposed by Hill and Karlsson in [SI and

    [6]

    will be used to illustrate the impact of load modeling

    on

    system stability. This model captures the load

    restoration characteristics with an exponential recovery

    process. Figure 2. shows the typical power response of

    aggregate loads to a voltage step and its exponential

    approximation. Some examples of this response are

    provided in [Il l .

    Mathematically, this model can be

    expressed in state space form as,

    x p = P , ( V ) - P ,

    (2.3)

    xq = Qs (U

    Qd (2.4)

    Pd = * x p

    + p , ( V ) (2.5)

    Qd = t x q +Q,W (2.6)

    where

    Pd

    and

    Qd

    are the load real and reactive powers,

    xp and xy are the corresponding load states,

    Tp

    and

    Tq

    are

    the load recovery time constants.

    Qs,

    ,

    nd

    Qt,

    Pl

    are the

    steady state and transient load characteristics respectively.

    Normally they are expressed as a function of node

    voltage V ither exponential as

    (2.7)

    =

    QO

    kp Q =

    QO gp

    or a polynomial function, such as a quadratic function;

    Recovery time constants

    Tp

    and T, range from 60s

    to

    150s. The values for a; and p, will take the same values

    as a nd p i n the static component, while

    a

    2.0 h;. .5

    [61.

    1.1,

    Figure 2. Typical power response of aggrega te loads to

    a voltage step

    (3) A steady-state equivalent circuit of Induction Motor

    as Figure 3 shows can be used [8]. When we neglect the

    stator transients, the aggregate IM is represented by its

    first order model,

    (2.9)

    Where s s the motor slip; H s moment of inertia; T, and

    T,,, are the electromagnetic and mechanical torques

    respectively;

    T,a

    P&,

    V) in per unit if neglecting effects

    of R, and T isassumed to be constant. Parameters for IM

    can be taken from [8].

    s = & T

    s)

    - T

    (3,

    U1

    T f S

    Figure

    3.

    IM steady-state equivalent circuit

    These models will be used in load modeling and study of

    modeling impact on system stability in the following

    sections.

    111. GA/EP

    LOAD

    DENTIFICATION

    In this section, we propose the algorithm for load

    identification. System identification and EP fitness

    function for the specific purpose of load modeling

    identification.

    [

    121

    Genetic Algorithms (GAS) are heuristic algorithms,

    which can locate the global optimal solution. The G A

    optimization mechanism is developed from the concept of

    natural evolution, where the strongest individuals survive

    and the weaker ones die off during the evolution process.

    Part of the work is to develop an effective modification of

    14

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    a genetic algorithm to optimally determine the load

    model parameters w ith system identification algorithms.

    For better GA performance, adaptively adjusted mutation

    probability can be used [13], [14], [15], [16], and [17]. In

    this paper

    two

    parallel processes are used for mutation

    probability control, as follows,

    P,(i,y) = P, *exp(-+i/nl)*exp(-y/n2)

    (4. I )

    where P, is the mutation probability, which takes the

    initial value of P, , i is the fitness of the i-th individual,

    y is the generation numbe r, nl an d n2 are ad justing factors

    controlling the decre asing rate of P, taking into

    consideration of fitness and generation number

    respectively.

    In our algorithm, the production mutation occurs when a

    Gauss-distribution random vector is added into the parent

    generation. The basic algorithm adopted in this paper is

    as follows,

    1. Problem Formulation: The solution

    X

    of the

    optimization problem is represented by a d-

    dimensional vectorX = [x x2 .

    ,

    d 1 and uJ

    < xJ

    V j

    = 1,2,-.-,

    (4.3)

    Where N ( O , P , + z , ) is the mutation

    operation vector, and the PJ + Z J s the

    determination variable based on the value of

    mutation probability Z

    5.

    Tournament: The competence of tournament is

    calculated by each individual's tournament penalty

    weighting factor, weighf( i ) .This factor is calculated

    by comparing with other randomly selected

    individuals.

    emax

    e

    emax

    m

    weight(i)

    =

    c w ,

    / = I

    (4.4)

    WJ;l ..l.Jc

    0

    Where ,U',, is a random vector between (0, l) , e is

    the advantage.

    6. Selection: According to the value of weight, all

    individual (2n) are arranged

    in

    sequence. The first n

    individuals selected as the next g eneration.

    Return to 4 until the convergence condition is

    satisfied.

    7.

    I v .

    POWER SYSTEM MO EL ANALYSIS

    In this section, we test out algorithm with som e real field

    test data to identify load models for further stability

    analysis. The data is from the field measurement from

    Tong Liao Power Plant and the'neighboring area of the

    North East China grid. The one line diagram of the test

    system is given in Figure 4. Tong Liao Power Plant

    locates in the eastern part of Inner Mongolia. The

    electricity is transmitted to North East China Grid via

    three 220KV transmission lines over a distance of more

    than 200

    km

    7s

    jdw

    rhu ngli o

    tongliao

    tcngbian

    176, 177

    Figure 4. Power System Around Tong Liao Power Plant

    1V.I. Load Model Identification

    We take the population size n = 50, the number of each

    individual competing with others

    m

    = 30. The Elite

    percentage, which decides the percentage of reserved

    individuals in each generation be lo , so Elite =

    n*10

    =

    5 ;

    mutation probability

    z

    =

    0.001

    and scale factor B

    =

    , where

    step-num

    is the total number of

    iterations. The limits of variables to be identified are

    given in Table

    1.

    e-O.OS*step-num

    Table

    1.

    Variables range

    of

    solution vector

    Lowerlimit

    0

    I -1

    I

    -3

    0 -1

    I -30

    15

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    These limits are used only during the initial population is

    being produced. Now we give so me detailed case studies

    from field test and com puter identification simulation.

    Error

    2.42 16307e -002

    2.42 1666

    1

    -002

    Example 1. Static load model

    The active power P and reactive power Q are identified

    respectively. The identification process terminates after

    100

    generations. The results a re shown in Table 2.

    X1 x2

    0.68979 14.05219

    0.68653 1427952

    Table 2. The identification resu lts of static load model

    Active Dower

    A

    parameter

    =

    0.001 and

    f l

    =

    e-0~08 step-num

    In our

    algorithm, we consider

    two

    aspects of modeling: (1)

    order of model, A4 is often set to be 1 or 2, and (2)

    linearity of the model, is Boolean variable, and

    = 0

    stands for linear model, = 1 for nonlinear model.

    We used dynamic load model to fit the test data with

    iteration number of 3000. Both first-order linear model

    and se cond-order nonlinear model are identified. Figure 6

    shows the simulated results of active and reactive powers.

    Identification error and modeling param eters are given in

    Table3 .

    ~~

    2.42 16854e-002 0.68764 1425461

    2.42 16894e-002

    0.68925 1437090

    2.42 17 187e-002 0.69oOo

    1430551

    Reactive Dower

    x3

    -13.95077

    -14.16945

    Therefore, the identification gives the static load m odel

    as:

    x4 X5

    -7.87665 9.16634

    -822913 9.47256

    P

    =

    0.454084V1.405687

    Q = 0.179435V3.206189

    -14.14562

    -1426829

    -1420455

    In our identification process, PO,

    l

    Qo bl are very closed

    after only one identification, and all solution individuals

    converged close to their final solution point very quickly.

    Since the frequency f hanged very small in field tests,

    the impa ct of frequency variation is ignored and the static

    load model is used. The identified and measured real data

    of the reactive and reactive powers are shown as Figure 5 .

    ~~~~

    -8.05477

    921439

    -820608 930574

    -829263 9.42222

    0.48

    0.46

    0 45

    Error

    6.85621-

    6.8737617MKl3

    0.W 1.00 1.01 1.02 1

    I3

    X I x2

    0.95424 535434

    0.95633 5.40915

    Figure

    5.

    The curves

    of

    static loads between identified

    and real measured data

    6.8765852dH3

    6.877633W3

    6 . m 3

    Example 2. Dyna mic load model

    Let the population size

    n

    = 200, the number

    of

    each

    individual competing with others

    m

    =

    80.

    One generation

    is left by IO , i.e.,

    Elite = n*10 =

    20, mutation

    0.95445

    5.46509

    0.95560 539985

    0.95516

    m

    Table 3. The identification resu lts

    of

    the dynamic load

    ~

    Y

    x3

    -522094

    -52848

    -533203

    -52'7143

    -539731

    X$

    4

    4 m 82027

    -5.73658 7.88834

    -5.75931 7.79500

    -5.97893

    8.031%

    -5.98805

    8.08046

    i n

    n

    qn

    r n

    cn cm

    i n n

    r?n

    Figure 6. The comparison curve s of reactive power:

    identified and real measured

    Based from the results obtained, we can conc lude-that,

    16

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    1.The results are satisfactory for the requirement of

    system security analysis from field test. We also

    performed Least Square identification, and it can be

    seen that our G A E P based algorithm gives better

    performance over the LS approach. The algorithm is

    robust with different orders of linear model.

    2. The initial generation of solutions can be produced by

    random m odels or combining some consideration of

    the actua l plant to be identified.

    onstant Eq' Mod el and Constant resistance

    .

    Classic Eq Mod el and Constant resistance

    Online Eq Model and Exponential unction

    IV.11. Load Modeling and System Stability

    described before. As we can see, the simulation results

    fits very closely to the real field tests. This demonstrated

    Based on the load identification results, simulation

    of

    the

    power grid is carried out. The results are given in Figures

    7 - 10. In the simulation, it is assumed that all

    4

    generators in Tong Liao Power Plant have the same

    -Constan t Eq' Model and Constant resistance

    .

    Classic Eq Model and Constant resistance

    Online Eq Model and Exponential function

    2.44

    ,

    , ,

    ,

    , t ~ s )

    0.4

    0.2

    0

    2

    4 6 8 10

    Figure

    7.

    P at 1 Diantong transmission line after a phase

    dinrnnnertinn

    generation level, the network operation condition is

    during later peak hours, and system loads are taken the

    classical loading levels under normal operation

    conditions. The system faults include: (i) disconnection

    of the three phase m ain transmission line, (ii)

    disconnection of the three phas e main transmission line at

    -Constant Eq' Model and Constant resistance

    . Classic Eq Model and Constant resistance

    1 4

    ..

    10

    0 t(s)

    2 4 6 8 10

    Figure

    9.

    Power plant angle stability after Dianju

    trrnsmiwinn line nn

    lnnd

    disrnnnertinn.

    -Constant Eq' Model and Constant resistance

    . Classic Eq Model and Constant resistance

    Online Eq Model and Exponential unction

    I I

    1P

    Ac

    iv 3.5 1

    tfs)

    .51

    4 .

    . . . . . . . . . . .

    ,

    0

    2

    i

    6

    10

    Figure 10. #2 Generator active power behavior after Dianju line

    nn-lnad 3 nhrne dismnnertinn.

    In Figures

    7

    -

    10

    the solid lines in each figure stand for

    constant Eq' model, dashed lines stand for Eq classical

    model, and the short dashed lines stand for performances

    follow ing field test for the Eq model. The load models

    These stability simulations under various system

    operation and loading conditions are very useful for

    future

    operation planning of Tong Liao Power Plant.

    Algorithms used here can certainly be applied to other

    systems to investigate the system load modeling and

    stability conditions in a very practical and less risky way.

    0 5

    t(s) V. CONCLUSIONS

    2

    4 6 8 10

    Genetic Algorithms and Evolutionary Programming

    based identification is used in the paper to identify the

    power system load parameters based on data from field

    the terminal out of the power plant, (iii) main measurement. Several load models are used to simulate

    transmission line two phase short circuit at Ju Feng the identification process. Improvements over the basic

    terminal side.

    genetic algorithms a re proposed including considerations

    Figure

    8.

    Active power tra nsients of Dianling line after

    3

    phase

    dinrnnnrrtinn nf nian tnne line.

    17

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    on m utation probability control, fitness formulation and a

    progressive concept for search and optimization. Both

    theoretical analytical simulation and field tests are carried

    to validate the effective of the algorithm for load models

    and their impact on system stability. It can be seen from

    these simulations and tests the algorithms proposed in the

    paper gives satisfactory results of identification for

    further stability analysis. Further researches are being

    carried out to develop a more comprehensive general load

    model suitable for measurement based model

    identification and system stability analysis.

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