MONITORING AND CONTROL OF HYDRO POWER PLANT

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    MONITORING AND CONTROL OF HYDRO POWER PLANT

    Matei Vinatoru

    University of Craiova, Faculty of Automation, Computers and Electronics

    Str. A. I. Cuza Nr. 13, Craiova, RO 200396

    Abstract: In hydro power plants from Romania, there is a major interest for theimplementation of digital systems for monitoring and control replacing the conventional

    control systems for power, frequency and voltage. Therefore is necessary to develop

    mathematical models capable to accurately describe both dynamic and stationarybehaviour of the hydro units, in order to be able to implement digital control algorithms.

    Moreover, it is necessary to implement systems for monitoring and control of hydro

    power plants in a cascade system along a river, in order to optimize the use of the river

    resources. This paper presents the possibilities of modelling and simulation of the hydro

    power plants and performs an analysis of different control structures and algorithms.

    Keywords: Hydro power plant, Control system, Digital Control Algorithms.

    1. INTRODUCTION

    This paper discusses the aspects of modelling and

    design of hydro power plants and control of hydro

    power groups. There are presented computing

    methods for pressure losses on the water intake pipesfrom the reservoir to the turbine, aspects regarding

    the energy transformations for different turbine types

    (Pelton, Francis, and Kaplan) in order to determinethe net hydraulic power of the plant and to determine

    the control options for the turbines.

    Also, are presented different control structures for

    the power groups and hydro power plants. In this

    case, are analyzed different SCADA monitoring and

    control systems, for an assemble of hydro power

    plants on the same water stream as well as SCADAsystem for high-energy power plants with Kaplan

    turbines, and the case studies for the modelling,

    design and study of the power groups, with andwithout water towers.

    This paper will present several possibilities for the

    modelling of the hydraulic systems and the design of

    the control system.

    2. THE DESIGN OF CONTROL SYSTEMS FORKAPLAN HYDRAULIC TURBINES

    2.1.Introduction

    Different construction of hydropower systems and

    different operating principles of hydraulic turbines

    make difficult to develop mathematical models fordynamic regime, in order to design the automatic

    control systems. Also, there are major differences in

    the structure of these models. Moreover, there aremajor differences due to the storage capacity of the

    reservoir and the water supply system from the

    reservoir to the turbine (with or without surgechamber). The dynamic model of the plants with

    penstock and surge chamber is more complicated

    than the run-of-the-river plants, since the water feed

    system is a distributed parameters system.

    2.2. Modelling of the hydraulic system for run-of-the-river hydropower plants

    These types of hydropower plants have a low water

    storage capacity in the reservoir; therefore the plant

    operation requires a permanent balance between thewater flow through turbines and the river flow in

    IFAC Workshop ICPS'07

    2007, July 09-11

    Cluj-Napoca, Romania

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    order to maximize the water level in the reservoir for

    a maximum efficiency of water use. Next, we willdetermine the mathematical model for each

    component of the hydropower system.

    A. Hydraulic turbine. The hydraulic turbine can be

    considered as an element without memory since thetime constants of the turbine are less smaller than the

    time constants of the reservoir, penstock, and surge

    chamber, if exists, which are series connectedelements in the system.

    As parameters describing the mass transfer andenergy transfer in the turbine we will consider the

    water flow through the turbine Q and the moment M

    generated by the turbine and that is transmitted to the

    electrical generator. These variables can be

    expressed as non-linear functions of the turbinerotational speed N, the turbine gate position Z, and

    the net head H of the hydro system.

    Q = Q(H, N, Z) (1)

    M = M(H, N, Z) (2)

    Through linearization of the equations (1) and (2)around the steady state values, we obtain:

    zanahaq

    ZZ

    QN

    N

    QH

    H

    QQ

    ... 131211 ++=

    +

    +

    = (3)

    zanaham

    ZZ

    MN

    N

    MH

    H

    MM

    ... 232221 ++=

    +

    +

    = (4)

    where the following notations were used:0Q

    Q=q ,

    0N

    N=n ,

    0M

    M=m ,

    0H

    H=h ,

    0Z

    Z=z which

    represent the non-dimensional variations of the

    parameters around the steady state values.

    B. The hydraulic feed system. The hydraulic feedsystem has a complex geometrical configuration,

    consisting of pipes or canals with different shapesand cross-sections. Therefore, the feed system will

    be considered as a pipe with a constant cross-section

    and the length equal with real length of the studied

    system. In order to consider this, it is necessary thatthe real system and the equivalent system to contain

    the same water mass. Let consider m1, m2... mn thewater masses in the pipe zones having the lengths l1,

    l2,...,lnand cross-sectionsA1, A2,...,Anof the real feed

    system. The equivalent system will have the lengthL=l1+l2+...+ln and cross-section A, convenientlychosen. In this case, the mass conservation law in

    both systems will lead to the equation:

    ==

    =n

    iii

    n

    ii AllA

    11

    . (5)

    Since the water can be considered incompressible,

    the flow Qi through each pipe segment with cross-

    section Ai is identical and equal with the flow Qthrough the equivalent pipe

    Q=v.A=Qi=vi.Ai for i=1, 2,...,n (6)

    Where v is the water speed in the equivalent pipe,

    and viis the speed in each segment of the real pipe.From the mass conservation law it results:

    QAl

    l

    Al

    lQ

    A

    Qv

    ii

    i

    ii

    ii ...

    === (7)

    The dynamic pressure loss can be computedconsidering the inertia force of the water exerted on

    the cross-section of the pipe:

    dt

    dv

    g

    LAaALamFi .

    ..... ===

    (8)

    Where L is the length of the penstock or the feed

    canal, A is the cross-section of the penstock, is thespecific gravity of water (1000Kgf/m

    3), a is the water

    acceleration in the equivalent pipe, and g=9,81 m/s2

    is the gravitational acceleration.

    The dynamic pressure loss can be expressed as:

    dt

    dQ

    Al

    l

    g

    L

    dt

    dv

    g

    L

    A

    FH

    ii

    iid

    ===.

    .. (9)

    Using non-dimensional variations, from (9) it results:

    dt

    Q

    Qd

    Al

    lL

    H

    Q

    H

    H

    ii

    i

    dd

    d

    =

    0

    0

    0

    0

    (10)

    Or in non-dimensional form:

    dt

    dqTh wd = (11)

    Where TW is the integration constant of the

    hydropower system and the variables have the

    following meaning:

    ===ii

    i

    d

    w

    d

    dd

    Al

    lL

    H

    QT

    Q

    Qq

    H

    Hh

    0

    0

    00

    ,, (12)

    It must be noted that this is a simplified method to

    compute the hydraulic pressure loss, which can be

    used for run-of-the-river hydropower plants, withsmall water head. If an exact value of the dynamic

    pressure is required, then the formulas presented in

    [8], sub-chapter 8.4 The calculation of hydro energypotential shall be used.

    Using the Laplace transform in relation (11), it

    results:

    hd(s) = - sTw.q(s), and, )(1

    )( shsT

    sq dw

    = (13)

    Replacing (13) in (3) and (4) and doing some simple

    calculations, we obtain:

    )(1

    )(1

    )(11

    13

    11

    12 szsTa

    asn

    sTa

    asq

    ww ++

    += (14)

    )(1

    )(1

    )(11

    13

    11

    12 szsTa

    sTasn

    sTa

    sTash

    w

    w

    w

    wd +

    +

    =

    (15)

    )(1

    )(1

    )(11

    1323

    11

    1221 sz

    sTa

    sTaasn

    sTa

    sTaasm

    w

    w

    w

    w

    ++

    +=

    (16)

    The mechanical power generated by the turbine can

    be calculated with the relation P=..Q.H (see [8]sub-chapter 8.5 Hydraulic turbines), which can be

    used to obtain the linearized relations for variations

    of these values around the steady state values:

    p = .g.Qo.h + .g.Ho.q (17)

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    Where is the turbine efficiency, and , Q, and Hwere defined previously.

    On the other hand, the mechanical power can be

    determined using the relation P=M.=2.M.N,which can be used to obtain the linearized relationsfor variations of these values around the steady state

    values:

    ( )m

    P

    Np

    P

    Nn

    o

    o

    o

    o222

    = (18)

    Where P0=M0.0is the steady state power generatedby the turbine for a given steady state flow Q0and a

    steady state head H0, and N0 is the steady state

    rotational speed.Using these relations, the block diagram of the

    hydraulic turbine, for small variation operation

    around the steady state point, can be determined andis presented in figure 1, where the transfer functions

    for different modules are given by the following

    relation:

    +=

    +=

    +=

    +=

    +=

    +=

    sTa

    sTaasH

    sTa

    sTaasH

    sTa

    sTaH

    sTa

    sTasH

    sTa

    asH

    sTa

    asH

    w

    wmz

    w

    wmn

    w

    whz

    w

    whn

    wqz

    wqn

    11

    1323

    11

    1221

    11

    13

    11

    12

    11

    13

    11

    12

    1)(,

    1)(,

    1

    ,1

    )(,1

    )(,1

    )(

    (19)

    For an ideal turbine, without losses, the coefficients

    aij resulted from the partial derivatives in equations(12 - 16) have the following values: a11=0,5;

    a12=a13=1; a21=1,5; a23=1. In this case, the transfer

    functions in the block diagram are given by thefollowing relation:

    sT.,

    sTH,

    sT.,HH

    w

    whn

    wqzqn

    501501

    1

    +=

    +== (20)

    +=

    +=

    sT.,

    sT,H,

    sT.,

    sTH

    w

    wmn

    w

    whz

    50151

    501(21)

    sT.,

    sT..

    sT.,

    sT)s(H

    w

    w

    w

    wmz

    501

    501

    5011

    +

    =

    += (46)

    2.3. Simulation results

    Example. Let consider a hydroelectric power systemwith the following parameters:

    -Water flow (turbines): Q(5001000) m3/s, QN=725m3/s;

    -Water level in the reservoir: H(1738) m, HN=30m;

    -The equivalent cross-section of the penstockA=60m2;

    -Nominal power of the turbine

    PN=178MW=178.000kW;

    -Turbine efficiency =0,94;-Nominal rotational speed of the turbine N=71,43

    rot/min;

    -The length of the penstock l=li=20m;

    It shall be determined the variation of the timeconstant TWfor the hydro power system.

    For the nominal regime, using relation (12), where

    li=20m, the time constant of the system is:sTw 82,0

    6081,9

    20

    30

    725=

    = (47)

    Next we will study the variation of the time constant

    due to the variation of the water flow through theturbine for a constant water level in the reservoir,

    H=30m, as well as the variation due to the variable

    water level in the reservoir for a constant flowQ=725 m

    3/s.

    In table I, column 3 and figure 2 a) are presented the

    values and the graphical variation of the timeconstant TW for the variation of the water flow

    between 500 m3/s and 110 m

    3/s, for a constant water

    level in the reservoir, H=30m. In table 8.12 column 4

    and figure 2 b) are presented the values and thegraphical variation of the time constant TW for the

    variation of the water level in the reservoir, for aconstant water flow, Q=725m3/s.

    It can be seen from the table or from the graphs that

    the time constant changes more than 50% for the

    entire operational range of the water flow through theturbine or if the water level in the reservoir varies.

    These variations will create huge problems during

    the design of the control system for the turbine, androbust control algorithms are recommended.

    gQo

    gHo

    Hqn(s)

    Hqz(s)

    Hhn(s)

    Hhz(s)

    Hmn(s)

    Hmz(s)

    2No/Po

    (2No)2/Po

    p

    np

    n

    n

    n

    z

    z

    z

    z

    m

    h

    q

    +

    Fig. 1. The block diagram of the hydraulic turbine.

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    Table I. Variations of the time constant of the hydro

    system

    H Q Tw(H=30m) Tw(Q=725mc/s

    17 1135,46 1,286065 1,449101

    20 965,14 1,093155 1,23173623 839,25 0,950569 1,071075

    26 742,42 0,8408882 0,947489

    29 665,62 0,7538998 0,849473

    32 603,21 0,6832217 0,769835

    35 551,51 0,6246598 0,703849

    38 507,97 0,5753446 0,648282

    In figure 3 is presented the block diagram of theturbines power control system, using a secondary

    feedback from the rotational speed of the turbine. Itcan be seen from this figure that a dead-zone element

    was inserted in series with the rotational speed sensor

    in order to eliminate the feedback for 0,5%variation of the rotational speed around thesynchronous value.

    The constants of the transfer functions had been

    computed for a nominal regime TW=0,8s. Theoptimal parameters for a PI controller are: KR=10,

    TI=0,02s. The results of the turbine simulation fordifferent operational regimes are presented in figure

    4, for a control system using feedbacks from theturbine power and rotational speed, with a dead-zone

    on the rotational speed channel for 0,5% variation

    of the rotational speed around the synchronous value(a) Power variation with 10% around nominal value,

    b) Rotational speed variation for power control).

    Figure 3. Block Diagram of the control system for hydraulic turbines

    np

    0.0389

    0.0016

    s4,01

    1

    +

    0.0025

    1.1305

    p

    n

    n

    n

    z

    z

    z

    z

    m

    h

    q

    +

    s4,01

    1

    +

    s

    s

    4,01

    8,0

    +

    s

    s

    4,01

    2,05,1

    +

    s

    s

    4,01

    8,01

    +

    s

    s

    4,01

    8,0

    +

    +

    sTK

    IR

    11

    --

    +

    P*

    0,6

    0,7

    0,8

    0,9

    1

    1,1

    1,2

    1,3

    1,4

    1,5

    15 20 25 30 35 40

    [s]

    [m]

    H

    Tw

    b)

    0,5

    0,6

    0,7

    0,8

    0,9

    1

    1,1

    1,2

    1,3

    1,4

    500 600 700 800 900 1000 1100 1200

    Tw

    Q

    [s]

    [mc/s]a)

    Figure 2 Variation of the integral time constant TW: a) by the flow Q, b) by the water level H

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    Fig. 4. Turbine Control simulations with feedbacksfrom turbine power and rotational speed

    Fig. 5 Control structure with only power feedback,

    a) Power variation with 10% around nominal value,

    b) Rotational speed variation for power control

    In figure 5 are presented the variations of the turbine

    power (graph a) and rotational speed (graph b) forthe control system using a feedback from the turbine

    power but no feedback from the rotational speed .

    This oscillation has no significant influence on the

    performance of the system but would have lead topermanent perturbation of the command sent to theturbine gate.

    2.4. Conclusions

    The possibility of implementation of digital systems

    for monitoring and control for power, frequency andvoltage in the cascade hydro power plant was

    discussed. The simplified mathematical models,

    capable to accurately describe dynamic andstationary behaviour of the hydro units have been

    developed and simulated. These aspects are

    compared with experimental results. Finally, a

    practical example was used to illustrate the design ofcontroller and to study the system stability.

    3. IMPLEMENTATION OF DIGITAL SYSTEMS

    FOR MONITORING AND CONTROL IN

    CASCADE POWER PLANTS

    3.1. Introduction

    A series of hydro power plant systems in Romania

    are capturing the river water in a geographical area

    and store it in reservoirs connected through transport

    pipes. Every lake has its own hydro power plant and

    the water used through the turbines of one plant issent to the next reservoir, thus using the entire

    hydraulic potential offered by the geographical area.A similar hydro power system is built in the north-

    west part of Oltenia region, in the south-west part of

    Romania. The hydraulic profile of this cascadesystem is presented in figure 6.

    As it can be seen in this figure, there are two hydropower plants, CH1 and CH2, with reservoirs and

    surge tanks and one run-of-the-river power plant, CH

    3, with a reservoir providing only a net head.

    In this type of hydropower systems, provided with

    small power units connected to the grid, the dynamicof the hydraulic system has a great importance in thestability of the system. The dynamics of the turbine

    and electric generator have a very small influence

    since the power grid has a great influence and willmaintain the generator rotational speed at a value

    synchronized with the electrical frequency of the grid

    and the generated power is dependent of the existingunbalance. Therefore, this paper will try to study the

    stability of the hydraulic system of the hydropower

    system and the achievement of a maximum

    efficiency of the water usage in the system.

    0 0.5 1 1.5 2 2.5 3-0.02

    0

    0.02

    0.04

    0.06

    0.08

    0.1

    0.12

    0 0.5 1 1.5 2 2.5 3-2

    -1

    0

    1

    2

    3

    4

    5

    P[%]

    a)

    b)

    t [s]

    t [s]

    0 0.5 1 1.5 2 2.5 3-0.04

    -0.02

    0

    0.02

    0.04

    0.06

    0.08

    0.1

    0.12

    0.14

    P[%]

    0 0.5 1 1.5 2 2.5 3-4

    -2

    0

    2

    4

    6

    8

    10

    12

    t [s]

    t [s]

    a)

    b)

    n[%]

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    3.2. The design of control systems for hydro power

    plants with reservoir and surge tank.

    Different construction of hydropower systems and

    different operating principles of hydraulic turbinesmake difficult to develop mathematical models for

    dynamic regime, in order to design the automaticcontrol systems [1,2,5,6]. Also, there are major

    differences in the structure of these models.

    Moreover, there are major differences due to thestorage capacity of the reservoir and the water supply

    system from the reservoir to the turbine (with orwithout surge tank). The dynamic model of the

    plants with penstock and surge tank is more

    complicated than the run-of-the-river plants, sincethe water feed system is a distributed parameters

    system. This paper presents a solution for the

    modelling of the hydraulic systems and the design ofthe control system.

    As it is know, the hydraulic power available at theturbine is a function of the water flow trough the

    turbine Qtand the net head Hn.

    Ph= QtHn (25)

    In the long run operation of the hydro power plants

    with reservoir and surge tank, it results from the

    relation (25) that the power generated by the turbine

    is maximum when the head Hn is maintained at

    maximum value, for variations of the river flow dueto meteorological conditions. In this case, the power

    generated by the turbine will be only a function of

    the water flow trough the turbine. In this case, thecontroller is controlling the flow Qt in order to

    maintain constant the water level in the reservoir,

    thus the main feedback will be from the reservoirswater level sensors.

    There are cases when the hydro power plants with

    high capacity reservoirs are used as peak load plants.In these cases, the power dispatcher will impose the

    plant generating power and the plant dispatcher or

    the automatic control system will distribute therequired load over the operational power units and

    the water level in the reservoir can vary between the

    admissible maximum and minimum limits with anadmissible rate of variation. The set-point for the

    water level controller is generated by the monitoring

    system, has a certain variation profile and is a

    function of the required power:

    t

    nn

    Q

    PH

    ** = (26)

    In figure 7 is presented the simplified hydraulicdiagram of a hydropower plant with reservoir and

    surge tank. Using this structure, a case study is

    presented, regarding the modelling, simulation and

    the stability of the of the control structure.

    3.2.1 Mathematical modelling of the control system

    This control system is opening and closing thecontrol gates for the turbines in order to assure an

    optimal operation and in the same time to maintain a

    constant water level in the reservoir. In a similarmode, a control system may be used for two plants in

    a cascade system to maintain the water flows

    between the plants.

    In order to design the control system, there is

    necessary to obtain a mathematical model of theplant, which contains the water tunnel between the

    reservoir and the surge tank, the surge tank itself, the

    penstock and the hydraulic turbine[4,5,6]. We willanalyze every component of the plant in order to

    determine the model, using the energy balance

    equations and the continuity equations for the waterflows, in dynamic regime.

    For the hydropower plant we will consider the

    simplified diagram in figure 7.

    a) The continuity equation for the water in thereservoir

    wtrB

    L QQQdt

    dHA = (27)

    Where: -ALis the area of the horizontal surface of theequivalent reservoir considered as having a constant

    depth HL. HL.AL=Vreal, Qris the water flow entering

    the reservoir, QW is the discharging water flow(through the emptying channel or overspill).

    b) The energy balance equation for the water tunnelbetween the reservoir and the surge tank:

    Surge Tank

    Penstok Generator

    Water tunnel

    Overspill

    Figure 7. Simplified model of the hydropower plant

    Turbine

    ControllerHn

    *

    Level

    transducer

    t

    Echivalent

    reservoir

    HBHC

    Qcf

    QB

    Lt

    Qe

    Qr

    c

    TurbineGate

    HL

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    cHBHcQcQCctQtQtCdt

    tdQ

    gA

    L

    t

    t =++ (28)

    Where: -Lt is the length of the tunnel between thereservoir and the surge tank, At is the cross-section

    of the tunnel, Qtis the water flow in the tunnel, Qcisthe water flow entering the surge tank, HB is the

    water height in the reservoir, HCis the water heightin the surge tank,

    dt

    dv

    g

    L

    dt

    AQd

    g

    L

    dt

    dQ

    gA

    L tttttt

    t

    t ==)/(

    is the

    inertial force of the water mass in the tunnelexpressed in hydrostatic units (meters of water

    column), Ct/Qt/Qt is the hydraulic pressure loss due

    to friction with the tunnel walls; the flow Qt is

    considered positive if the water flows from the

    reservoir to the surge tank and the loss coefficient Ctwill be positive in this case, Ct/Qc/Qcis the hydraulic

    pressure loss due to the cross-section reduction at the

    entrance in the surge tank installed to avoid thepressure shocks, -HB-HC is the driving force that

    moves the water in the tunnel and the surge tank.

    c) The continuity equation for the surge tank

    cftcc QQQdt

    dHcA == (29)

    Where: ACis the cross-section of the surge tank, QC

    is the water flow at the entrance of the surge tank

    (we assume that there is no water flow through thetop of the surge tank), Qcfis the water flow through

    the penstock.

    d) The energy balance equation for the penstock and

    the turbine

    Considering the low water volume existing in thesetwo elements we can neglect the water mass

    accumulation (water is considered incompressible).

    Therefore, from the energy balance equation, thebehaviour of the penstock and the turbine can be

    described by the water flow computed from the

    following relation:

    o

    ccccov

    H

    QQCHQxQ

    += , (30)

    Where: H0is the water level in the surge tank when

    the gate is completely open, Q0is the water flow for

    a completely open gate and -0 x 1 is the openingfactor for the gate.

    We choose this form of the expression in order to usenon-dimensional values for the gate opening and to

    avoid some very complex equations describing the

    water flow through the gate. Therefore are necessarysome experiments to measure the values of H0 and

    Q0. The gate is open completely and the flow Q0 in

    steady conditions is measured. After the flow

    stabilizes, the water height in the surge tank, H0, ismeasured. It must be mentioned that in steady state

    conditions (HL=constant, HC=constant,

    Qcf=constant), the water flow into the surge tank

    QC=0.

    e) The equation of the controller

    The control system structure for the water level in thereservoir is presented in figure 7. It is recommended

    to use a PI controller if the gate servomotor is a

    system with its own position controller (proportionalactuator) or a PD controller if the actuator is of the

    integrating type (without its own position controller).In our case we will use a PI controller.

    In this control system, the water level in the reservoiris compared with a set-point determined by the

    operational conditions. If the level is different than

    the set-point, the error is processed by the turbine

    controller which will open or close the gates in orderto maintain the water level at the prescribed value.

    The equation of the PI controller can be written in

    differential form:

    dt

    HHdKHH

    T

    K

    dt

    dx reffRreff

    i

    R)(

    )(

    += (31)

    Where: Hrefis the set-point level, Hfis the water level

    in the reservoir, KR, T iare the proportional constantand the integral constant of the PI controller.

    This equation is not considering some factors suchas: delays due to the servomotor and the controller,

    and minimum and maximum variation rates for the

    gates.

    3.2.2 Stability analysis

    The equations (27)-(31), which describe the dynamic

    behaviour of the control system for the hydropower

    unit, are strongly non-linear. Moreover, some

    parameters such as loss coefficients Ct and Cc canchange due to different flow regimes and due to

    building parameters of the feeding system. Thereforeis necessary to study the system stability in theoperation point (small stability in Lyapunov way)

    and to determine the stability domain in the

    operational parameters plane.

    a) Small stability of the control system

    Equations (27)-(31) will be linearized around the

    operation point. For simplicity, it is preferable to usenon-dimensional variables as follows: qt is the

    relative variation of the flow through the penstock, hB

    is the relative variation of the water level in thereservoir, hcis the relative variation of the water level

    in the surge tank, is the relative variation of thecontroller output and qris the relative variation of theriver flow around the steady state value for constant

    water level (Qr0=Qt0).

    0

    0

    0

    0

    0

    0

    0

    0

    0

    0

    r

    rrr

    c

    ccc

    B

    BBB

    t

    ttt

    Q

    QQq;

    x

    xx;

    H

    HHh

    ;H

    HHh;

    Q

    QQq

    =

    =

    =

    =

    =

    (32)

    We will introduce the following supplementary

    reference parameters,0

    200 ;

    c

    tt

    ref

    i

    H

    QCp

    H

    Tx== ,

    where characterize the statism of the integral

    -50-

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    controller (the slope of the controller output for a

    step variation of the error) and p characterize the

    ratio between the losses on the feeding pipes and thehydraulic pressure at the base of the surge tank.

    In steady state regime, HB=const., Hc=const.,

    Qt0=Qcf=const. and from equations (27)-(31) itresults that:

    02000 )1( cttcrefB HpCHHH Q +=+==

    0

    0

    0

    00

    c

    t

    H

    H

    Q

    Qx = .

    According with the previous relations and

    considering that the spillover flow is zero (QB=0),following linearization of equations (27)-(31), the

    linear state equations, expressed with non-

    dimensional variables defined in (32), can be writtenas:

    -from (27) it results:

    rtB

    t

    refLqq

    dt

    dh

    Q

    HA+=

    0 (33)

    -from (28) it results:

    cBc

    refc

    c

    cc

    tc

    ttt

    ct

    tt

    hhH

    Hq

    H

    C

    qH

    C

    dt

    dq

    HgA

    LQ

    Q

    Q

    =+

    ++

    00

    20

    0

    20

    0

    0

    2

    2

    (34)

    It can be considered that the level control system

    works with a zero steady state error, HB0=Href and

    Qc0=0 and from equation (28), written for steadystate, it results:

    110

    20

    0

    00020

    +=+=

    ==

    pH

    C

    H

    Hor

    HHHHC

    c

    tt

    c

    ref

    crefcBtt

    Q

    Q

    In this case, equation (34) becomes:

    cBtt

    ct

    tt hhpqpdt

    dq

    HgA

    LQ++= )1(2

    0

    0 (35)

    From the linearization of equation (29) it results:

    00

    0

    t

    cft

    c

    t

    cc

    Q

    Qq

    dt

    dh

    Q

    HA = (36)

    Where the variation of the water flow through the

    penstock Qcfcan be obtain from the linearization ofthe equation (30) around the steady state values:

    ct

    t

    ccc

    cf

    hQ

    Q

    hH

    HQx

    H

    HQxQ

    +=

    =+=

    2

    2

    00

    0

    000

    0

    000

    In this case, equation (29) becomes:

    = ctc

    t

    cc

    hqdt

    dh

    Q

    HA

    2

    1

    0

    0

    (37)

    The equation system (33 -37) can be expressed in

    canonical matrix-vectorial form:

    BuAxdt

    dx+= or BuAxx +=

    Where the following notations were used:

    00

    0

    0

    0 ,,t

    LrefL

    t

    ccc

    ts

    ttt

    Q

    AHT

    Q

    AHT

    AHg

    QLT

    =

    =

    =

    .

    And

    =

    c

    B

    t

    h

    h

    q

    x ;

    =

    1

    10

    LTB ;

    +

    =

    cc

    f

    www

    TT

    T

    TT

    p

    T

    p

    2

    10

    1

    001

    112

    A ; [ ]rq0=u .

    (39)

    The block diagram of the installation is presented in

    figure 8.

    For the controller, from (7) and noting:

    HH

    HHh

    ref

    refrefr

    0

    0= ,

    0

    0

    xT

    HKK

    i

    refRI= , (integral

    constant of the controller

    rationalized),0

    0

    x

    HKK

    refRP= , the proportional

    constant (rationalized) and e(t)=(hr-hBT), we obtain:

    dt

    tdeKteK

    dt

    dPI

    )()( +=

    (40)

    Adding equations (33), (35), and (37) and using thenotations from (14), we obtain the complete equation

    system for the controller in figure 7:

    HR(s) HIT(s)

    Hp(s)

    hB* hB(s)(s)e(s)

    qr(s)

    qt(s)

    -

    +

    +-

    Figure 8. The block diagram of level controller

    Notes: HR(s)-controller transfer function;

    HIT(s)-the transfer function on the direct channel

    HP(s)-transfer function on the perturbation channel

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    rL

    tL

    B qT

    qTdt

    dh+=

    11 (41)

    ct

    Bt

    tt

    t hT

    hT

    pq

    T

    p

    dt

    dq

    ++=

    112 (42)

    =c

    cc

    tc

    c

    Th

    Tq

    Tdt

    dh 1

    2

    11 (43)

    Using Laplace transform, for zero initial conditions,from equations (40) to (43) it results:

    )s(hsT

    )s(hsT

    p)s(q

    sT

    p)s(q

    );s(qsT

    )s(qsT

    )s(h

    ct

    Bt

    tt

    t

    rL

    tL

    B

    ++=

    +=

    112

    11

    (44)

    )s(eK)s(es

    K)s(

    )s(sT

    )s(hsT

    )s(qsT

    )s(h

    PI

    cc

    ct

    cc

    +=

    =1

    2

    11

    (46)

    These equations can be processed to obtain the

    transfer functions on the direct channel and on the

    perturbation channel. From (45), the flow qt can beexpressed as:

    )(2

    1)(

    2

    )1()( sh

    psTsh

    psT

    psq c

    tB

    tt +

    ++

    = (48)

    This will be used in equation (46):

    )s()s(h)s(h

    psT

    )s(hpsT

    )p()s(hsT

    cc

    t

    Bt

    cc

    +

    +

    +=

    2

    1

    2

    1

    2

    1

    (49)

    And the variation of the water level in the surge tank

    can be determined as:

    )s()p(s)TpT(sTT

    psT

    )s(h)p(s)TpT(sTT

    )p()s(h

    tctc

    t

    B

    tctc

    c

    ++++

    +

    ++++

    +=

    1242

    2

    1242

    1

    2

    2

    (50)

    Let note Hn(s)=2TcTts+(4pTc+Tt)s+2(p+1) to

    simplify the calculations and let use (50) in (48) todetermine the water flow through the penstock,

    which is equal with the flow through turbine.

    1242:where

    1

    2

    1

    2 ++++=

    ++

    +=

    ps)TpT(sTT)s(H

    ),s()s(H

    )s(h)s(H

    )s(H

    psT

    )p()s(q

    tctcm

    nB

    n

    m

    tt

    (51)

    And after simple processing from (51) and (44) it

    results:

    ( ))(

    )(

    )(2)(

    )(

    2)( sq

    sP

    sHpsTs

    sP

    psTsh r

    nttB

    ++

    +=

    (52)Where the characteristic polynomial of the open-loop

    system is:

    ( )

    [ ][ ] )pp(sT)p()TT)(p(p

    sTT)p(TT)p(TTp

    sTpTTTsTT)s(P

    tcL

    tctLLc

    tctLtcL T

    132114

    121228

    82

    2

    22

    342

    ++++++++

    +++++

    +++=

    (53)

    From (52), the two transfer functions in the block

    diagram of the control system presented in figure 2can be calculated:

    )(

    2)(

    sP

    psTsH tIT

    += and

    ( ))(

    )(2)(

    sP

    sHpsTsH ntP

    +=

    (54)

    From (47), using the Laplace transform, we get:

    )()()( shs

    sKK

    shs

    sKK

    s BTRI

    rRI

    +

    +

    = (55)

    Replacing (55) in (52), after several simpletransforms, it results:

    )s(q)sKK)(psT()s(Ps

    )s(H)psT(s

    )s(h)sKK)(psT()s(Ps

    )sKK)(psT()s(h

    rRIt

    nt

    rRIt

    RItB

    +++

    ++

    ++++

    ++=

    2

    2

    2

    2

    (56)

    Where the characteristic polynomial of the closed-

    loop system is:

    ( )

    [ ][ ]

    IRIt

    RttcL

    tctLLc

    tctL

    tcLRIt

    pKs)pppKKT(

    sKTT)p()TT)(p(p

    sTT)p(TT)p(TTp

    sTpTTT

    sTT)sKK)(psT()s(Ps)s(L T

    21322

    114

    121228

    8

    22

    2

    2

    32

    4

    52

    ++++++

    +++++++

    ++++++

    +++

    +=+++=

    For an exact analysis of the hydropower unit

    dynamic behaviour it can be considered the exampleof a hydropower plant with reservoir and surge tank

    having a low installed power but a high storage

    capacity in the reservoir.

    Experiment. It is considered a hydropower systemwith the following parameters:

    The water volume in the reservoir VL=4,8.106m3;

    -The equivalent depth of the reservoir (considered

    constant) HL=60m; The equivalent reservoir surface

    area is AL4,8.106/60=8.10

    4m

    2; The length of the pipe

    between the reservoir and the surge tank Lt=9650m,

    the diameter of the pipe Dt=3,6m and the cross-

    section At=10m2; The surge tank has a diameter

    Dc=5,4m with a cross-section Ac=23m2; The gross

    nominal head HB=260m, HBmax=266m, HBmin=245m;

    The gross nominal head at the surge tank Hc0=230m;

    The nominal flow through the penstock Qt0=36m3

    /s;The length of the penstock Lcf=205m.

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    Using the previous data, the time constants andequations coefficients can be determined using

    relation (14):

    s..

    T

    ;.

    T;,

    T

    L

    ct

    5106

    36

    80000260

    15036

    2323415

    10230819

    369560

    ==

    ===

    =

    02303636

    230130

    130230

    230260

    20

    0

    0

    0

    0

    2

    ,.

    .,pHC

    ;,H

    HH

    H

    Cp

    Q

    Q

    t

    ct

    c

    cref

    c

    tt

    ==

    =

    =

    ==

    (56)

    342230

    36

    0

    0

    0

    00

    0

    00000 ,

    cH

    tQ

    H

    Qx;

    H

    cHQxtQvQ =====

    The steady state value for the controller output x0is

    determined using the maximum flow through the

    penstock Qvmax=56m3/s and is obtained for x0=1:

    73640

    3742iar640

    56

    36

    0

    00 ,

    ,

    ,;,x

    H

    Q====

    Replacing these values in equations (48) and (50),we obtain the operational expressions for the flow q t

    and the level in the surge tank:

    )s(h

    s

    ,)s(h

    s

    .)s(q

    )s(qs

    .,)s(q

    s

    .,)s(h

    cBt

    rtB

    158

    921

    158

    354

    10166010166055

    +

    +

    =

    +=

    (57)

    )s(ss

    )s(,

    )s(hss

    ,)s(h Bc

    ++

    +

    ++

    =

    1411991

    158260

    1411991

    50

    2

    2 (58)

    ( )

    [ ][ ]

    IRIt

    RttcL

    tctLLc

    tctLtcL

    RIt

    pKs)pppKKT(

    sKTT)p()TT)(p(p

    sTT)p(TT)p(TTp

    sTpTTTsTT

    )sKK)(psT()s(Ps)s(L

    T

    21322

    114

    121228

    82

    2

    2

    2

    32

    452

    ++++++

    +++++++

    ++++++

    +++=

    =+++=

    L(s) = 405.108. s

    5 + 153.10

    7.s

    4 + 348,53.10

    5.s

    3 +

    (35,27.104 +15.KR).s

    2 + (15.KI+0,26.KR+4238).s +

    0,26.KI (59)

    Using the stability criteria Routh-Hurwitz for the

    characteristic polynomial (59) we obtain a series of

    inequalities for the tuning parameters Ki and KR asfollows:

    -from the block diagram of the control system

    presented in figure 8, it can be seen that the transfercoefficient on the direct channel is negative,

    therefore the controller shall have inverse output and

    therefore KR0 it results that the

    integral parameter shall be positive;-from the Hurwitz determinant of second order

    results:

    a0. a

    1 = 0,26 K

    I .( 15 K

    I + 0,26 K

    R + 4238) > 0

    1630069,57 +

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    This diagram was preferred for simulation since itallows highlighting the variation of some specific

    parameters of the system, such as the level in the

    surge tank and the flow variation in the penstock Q t.

    The simulation results are represented in the figures10 and 11.

    In figure 10 is presented the system output for a 10%

    variation of the set-point for the reservoir waterlevel, with no limitation on the flow control channel.

    Oscillations of the flow can be observed, due to the

    big differences between the time constants in thesimulation scheme.

    To avoid these flow oscillations, the variation of theflow control output is limited in order to avoid big

    differences between the subsequent commands sent

    to the gate. The simulation results are presented in

    figure 11.

    3.3. Conclusions

    Specifically, a hydropower plant may be composed

    of several turbine-generator units, referred to in this

    paper as groups. Each hydropower plant must becontrolled by a local SCADA system that will be

    connected at the Central SCADA system, which

    performs the control of the plants from the hydro-

    valley, for optimal generation scheduling and controlfor the reservoir stream-flows.

    4. MONITORING SYSTEM FOR CASCADEHYDRO POWER PLANTS.

    The optimal generation scheduling is an important

    daily activity for hydroelectric power generationcompanies. The goals are to determine which

    hydropower groups are to be used in order to

    generate enough power to satisfy demand

    requirements, with various technological constraintsand with minimum operating cost. In the same time

    hydropower systems must consider the stream-flow

    equations for reservoirs that couple all reservoirsalong a hydro-valley, because the amount of outflow

    water released by one of hydropower plant affects

    water volumes in all the plants downstream.Furthermore, other conditions must be imposed as:

    water travel times, alternative uses (irrigation, flood

    control, navigation). To solve the optimal scheduling

    of hydropower plants, a highly sophisticatedmodelling for the operation is required.

    In the figure 12 is presented the SCADA systemarchitecture for monitoring and control of hydro

    power plants in a cascade system along a river,

    implemented in order to optimize the use of the riverresources [7]. This structure is implemented at the

    central dispatcher. At the level of hydro power plant

    there is a local monitoring and control system,

    interconnected with central dispatcher via modemsand radio communication buses.

    0 2000 4000 6000 8000 10000-2.5

    -2

    -1.5

    -1

    -0.5

    0

    0. 5

    1

    0 2 0 0 0 4 0 0 0 6 0 0 0 8 0 0 0 1 0 0 0 0- 0 . 0 2

    0

    0 . 0 2

    0 . 0 4

    0 . 0 6

    0 . 0 8

    0 .1

    0 . 1 2

    0 . 1 4

    t [s]

    hB[%]

    Figure 10. The response of the control system for a 10% variation of the set-point

    t [s]

    qt [%]

    0 2000 4000 6000 8000 10000-0.02

    0

    0.02

    0.04

    0.06

    0.08

    0.1

    0.12

    0.14

    0.16

    0.18

    Figure 11. The response of the control system with flow limitation

    0 2000 4000 6000 8000 10000

    -0.6

    -0.4

    -0.2

    0

    0.2

    0.4

    0.6

    tt

    hB[%] qt

    -54-

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    The monitoring system presented above is

    performing the following functions:

    -Data acquisition from the local monitoring systemsinstalled in each power plant, using routers

    connected to telephone lines or radio

    communications; the data is sent tot the SCADA

    server for processing, monitoring and optimization;

    -The optimal load distribution between theoperational units in the power plants, depending of

    the available water flow, in order to ensure an

    efficient usage of the water for the required systempower;

    -Monitoring of the water levels in the reservoirs and

    water flow control in order to maintain the maximumwater level in the reservoirs;

    -In the case of extreme rain conditions, control the

    water flows in order to avoid flooding of the areasneighbouring the plants.

    5. CONCLUSIONS

    The possibility of implementation of digital systemsfor monitoring and control for power, frequency and

    voltage in the cascade hydro power plant was

    discussed. The simplified mathematical models,

    capable to accurately describe dynamic and

    stationary behaviour of the hydro units weredeveloped and simulated and these results were

    compared with the experimental results. Finally, a

    practical example was used to illustrate the design ofcontroller and to study the system stability.

    REFERENCES

    [1] G., D Ferrari-Trecate, Mignone, D. Castagnoli, M.Morari, Hybrid Modeling and Control of a

    Hydroelectric Power Plant, CH 0802, Institut furAutomatik, ETH- Zurich, (2003).

    [2] C. Henderson, Yue Yang Power Station TheImplementation of the Distributed Control System,GEC Alsthom Technical Review, Nr. 10, 1992.

    [3] G. I. Krivchenko, Hydraulic machines: Turbine andPumps,2nd ed. ISBN 1-56670-001-9, CRC Press,London (1994).

    [4] M. Vntoru, E. Iancu, C. Vntoru, Control,Monitoring and Protection of the Turbine andGenerator System, International Symposium on SystemTheory, Robotics, Computers and Process Informatics,

    SINTES 9, Craiova , (1998).

    [5] O. F. Jimenez, M. H. Chaudhry Water level Control in

    Hydropower Plants, Journal of Energy Engineering,Vol118, No. 3 Dec. 1992.

    [6] H. Weber, V. Fustik, F. Prillwitz, A. Iliev, Practically

    oriented simulation model for the Hydro Power Plant

    Vrutok in Macedonia, Balkan Power Conference, 19.

    21.06.2002, Belgrade

    [7] I.C.E Felix -Bucharest S.A, Arhitectura sistemului decontrol supervizor i achiziie de date (SCADA) alcascadei de hidrocentrale de pe Oltul Mijlociu, http://www.felix.ro/apl.html.

    [8] M. Vinatoru, Conducerea automata a proceselor

    industriale, vol. II, Editura Universitaria Craiova, 2005.

    To CHE

    System

    ER

    RadioEngineering

    Pules Message NMEA

    Sincron

    mGPS

    Local Sincron

    Server

    Ethernet Switch

    Pulse Message NMEA

    Operator 1 Operator 2

    EngineeringServer

    SCADA 1

    Server

    SCADA 2

    Hist. Date

    Server

    Ethernet Bus

    Ethernet Switch

    Simulator CHE

    Router

    Asyncron 2

    Router

    Asyncron 1

    - - - - - -Modem 10 Modem 1

    Ethernet Bus

    Sever Radio

    comunication

    Fig. 12. SCADA system architecture - Dispatcher

    Hydro power plants

    Wall Display (4 modules)

    -55-