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ISSN1100-1607

Control Lyapunov Functions:

A Control Strategy for Damping of Power

Oscillations in Large Power Systems

Mehrdad Ghandhari

Stockholm2000

DoctoralDissertation

Royal Institute of Technology

Dept. of Electric PowerEngineering

Electric Power Systems

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In thepresent climate of deregulation and privatisation, the utilitiesare

oftenseparatedintogeneration, transmissionanddistributioncompanies

so as to help promote economic eÆciency and encourage competition.

Also, environmental concerns, right-of-way and cost problems have de-

layedtheconstruction of bothgenerationfacilitiesand new transmission

lines whilethe demand for electric power has continued to grow, which

mustbemetbyincreasedloadingofavailablelines. Aconsequenceisthat

power system damping is often reduced which leads to a poordamping

of electromechanical power oscillations and/or impairment of transient

stability.

The aim of this thesis is to examine the ability of Controllable Series

Devices (CSDs),such as

 Uni edPower FlowController(UPFC)

 ControllableSeries Capacitor(CSC)

 QuadratureBoosting Transformer (QBT)

forimprovingtransient stabilityand dampingofelectromechanical oscil-

lationsina powersystem.

Forthesedevices, ageneralmodelisusedinpowersystemanalysis. This

model is referred to as injection model which is valid for load ow and

angle stabilityanalysis. The model isalso helpfulfor understandingthe

impact ofthe CSDson powersystem stability.

A control strategy for damping of electromechanical power oscillations

is also derived based on Lyapunov theory. Lyapunov theory deals with

dynamical systems without input. For this reason, it has traditionally

been applied only to closed{loop control systems, that is, systems for

which the input has been eliminated through the substitution of a pre-

determined feedbackcontrol. However, inthisthesis,Lyapunov function

candidates are used in feedback design itself by making the Lyapunov

derivative negative when choosing the control. This control strategy is

calledControlLyapunovFunction(CLF) forsystems withcontrolinput.

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Keywords: Controllable Series Devices (CSDs), Uni ed Power Flow

Controller (UPFC), Quadrature Boosting Transformer (QBT), Control-

lableSeriesCapacitor(CSC),Lyapunovfunction,ControlLyapunovFunc-

tion (CLF),SIngle Machine Equivalent(SIME), VariableStructureCon-

trol(VSC).

TRITA-EES{0004ISSN1100-1607

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First of all, I would like to express my deepest gratitude and apprecia-

tion to my supervisor, Professor Goran Andersson, for his support and

guidancethroughout thisproject.

I would like to extend my warmest thanks to Dr. Ian A. Hiskens for

his constant support, inspiringdiscussions and valuable suggestions, es-

peciallyduringmyvisitat theUniversityof Newcastle, Australia.

I gratefully acknowledge numerous useful comments by the members of

the project steering committee, namely, Mojtaba Noroozian, Lennart



Angquist, Bertil Berggren of ABB and Magnus Danielsson of Svenska

Kraftnat. Also, nancialsupportfromthesecompaniesthroughtheElek-

traprogram is gratefullyacknowledged.

Manythanks to thesta of ElectricPowerSystems forproviding stimu-

latingandfriendlyatmosphereforstudyandresearchandhelpindi erent

aspects. Myspecialthanksto Mrs. LillemorHyllengrenforallher assis-

tance.

A specialthanksto Lars Lindkvistforhis assistance withSIMPOW.

Many thanks to Professor Mania Pavella and Damien Ernstfor helping

mewith SIMEduringmy visitat theUniversityof Liege, Belgium.

Finally,Iwouldliketo extendmydeepestgratitudeand personalthanks

to those closest to me. In particular, I would like to thank my dear

mother for teaching me the value of education and my lovely Karin for

hersupportand encouragementduringthisperiodoflate workinghours.

Mehrdad Ghandhari

Stockholm

September2000

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Acronym Description

AC Alternating Current

AVR Automatic Voltage Regulator

BT Boosting Transformer

CLF ControlLyapunov Function

CSC ControllableSeries Capacitor

CSDs ControllableSeries Devices

DAE Di erential{Algebraic Equations

DC Direct Current

ET Excitation Transformer

FACTS FlexibleAC TransmissionSystems

GOMIB Generalized One{Machine In niteBus

OMIB One{Machine In niteBus

PSS PowerSystem Stabilizer

QBT Quadrature BoostingTransformer

RNM Reduced Network Model

s.e.p StableEquilibriumPoint

SIME SIngle MachineEquivalent

SPM Structure PreservingModel

TCSC ThyristorControlledSeriesCapacitors

TSSC ThyristorSwitchedSeriesCapacitors

UPFC Uni edPowerFlowController

VSC Variable Structure Control

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Abstract iii

Acknowledgments v

1 Introduction 1

1.1 Backgroundand Motivationof Project . . . 1

1.2 Aims ofthePerformed Work . . . 2

1.3 Outlineof theThesis . . . 5

1.4 Listof Publications. . . 6

2 Power SystemOscillations 9 2.1 Sourcesof Mitigating PowerSystem Oscillations . . . 10

2.2 Summary . . . 12

3 Modeling of Power Systems 13 3.1 Reduced Network Model . . . 15

3.2 StructurePreservingModel . . . 19

3.3 Summary . . . 21

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4 Modeling of Controllable Series Devices 23

4.1 OperatingPrinciple of Controllable SeriesDevices . . . . 23

4.1.1 Uni edPowerFlowController . . . 23

4.1.2 QuadratureBoosting Transformer . . . 24

4.1.3 ControllableSeries Capacitor . . . 24

4.2 InjectionModel . . . 25

4.2.1 InjectionModelof UPFC . . . 26

4.2.2 InjectionModelof QBT . . . 29

4.2.3 InjectionModelof CSC . . . 30

4.3 Summary . . . 31

5 Lyapunov Stability 33 5.1 Mathematical Preliminaries . . . 33

5.2 LyapunovFunction . . . 38

5.3 Total Stability . . . 46

5.4 Applicationof LyapunovFunctionto PowerSystems . . . 48

5.4.1 EnergyFunction forReducedNetwork Model . . . 48

5.4.2 EnergyFunction forStructure PreservingModel . 49 5.5 Summary . . . 54

6 Control Lyapunov Function 55 6.1 GeneralFramework. . . 55

6.2 Applicationof CLFto theStructure PreservingModel . . 68

6.3 Summary . . . 71

7 Numerical Example 73 7.1 Two{Area Test System. . . 74

7.2 IEEE 9-BusTest System . . . 79

7.3 Nordic32A Test System . . . 81

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8 Single Machine Equivalent 85

8.1 Foundations . . . 85

8.2 ControlLawBased on SIME . . . 87

8.3 Numerical Examples . . . 88

8.4 Selectionof theGains ofControlLaws . . . 102

8.5 Summary . . . 103

9 Variable Structure Control with Sliding Modes 105 9.1 Background . . . 105

9.2 Methodof EquivalentControl . . . 110

9.3 Summary . . . 117

10 Closure 119 10.1 ContributionsoftheThesis . . . 119

10.2 Conclusions . . . 120

10.3 Discussions and Future Work . . . 121

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3.1 A multi{machinepowersystem. . . 13

4.1 Basic circuitarrangement of aUPFC. . . 24

4.2 Basic circuitarrangement of aQBT. . . 25

4.3 Basic circuitarrangement of aCSC. . . 25

4.4 Equivalent circuitdiagramof a CSD. . . 26

4.5 Vector diagram ofthe equivalentcircuitdiagram. . . 26

4.6 Representationof theseriesconnectedvoltage source. . . 27

4.7 Replacementoftheseriesvoltagesourcebyacurrentsource. 27 4.8 Injection modelof theseriespartof theUPFC. . . 28

4.9 Injection modelof theUPFC. . . 28

4.10 CSClocatedina losslesstransmissionline. . . 30

5.1 Stabilityboundary(dottedlines)and stabilityregionof x s . 38 5.2 Estimate ofthe stabilityregionof x s .. . . 42

5.3 The OMIB system. . . 43

5.4 Phase portraitof theOMIB system. . . 44

6.1 The OMIB systemwitha CSD. . . 60

6.2 Phase portraitof theOMIB systemduringthefault. . . . 63

6.3 Phase portraitof theOMIB systemafter thefault. . . 64

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6.4 The2{machine in nitebustest system. . . 65

6.5 Variationoftherotor angles. . . 67

6.6 Variationoftheenergy function. . . 68

7.1 Thetwo{area testsystem. . . 74

7.2 VariationofP vs timeforthe systemmodel1. . . 75

7.3 VariationofP vs timeforthe systemmodel2. . . 76

7.4 VariationofP vs timeforthe systemmodel3. . . 77

7.5 VariationofP vs timeforthe systemmodel4. . . 78

7.6 TheIEEE 9{bus test system. . . 79

7.7 VariationofP vs timeinthe IEEE9{bus test system. . . 80

7.8 VariationofP vstimewithCSDsintheIEEE9{bussystem. 81 7.9 TheNordic32A test systemproposedbyCIGRE. . . 82

7.10 VariationofP vstimeintheNordic32Atestsystem,LF32{ 028. . . 83

7.11 VariationofP vstimeintheNordic32Atestsystem,LF32{ 029. . . 84

8.1 Two{area powersystem. . . 87

8.2 Case1: VariationofP vs. timeinthetwo{areatestsystem and phaseportrait ofthecorresponding GOMIBsystem.. 90

8.3 Case2: VariationofP vs. timeinthetwo{areatestsystem and phaseportrait ofthecorresponding GOMIBsystem.. 91

8.4 Case3: VariationofP vs. timeinthetwo{area testsystem. 92 8.5 VariationofP vs timeinthe IEEE9{bus system. . . 93

8.6 VariationofP vs timeinthe Nordic32Atest system. . . . 94

8.7 TheBrazilianNorth{South interconnection system.. . . . 95

8.8 Case 1: Variation of P vs. time in the Brazilian North{

Southinterconnectionsystemandphaseportraitofthecor-

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8.9 Case 2: Variation of P vs. time in the Brazilian North{

Southinterconnectionsystemandphaseportraitofthecor-

responding GOMIBsystem. . . 98

8.10 Case 3: Variation of P vs. time in the Brazilian North{

Southinterconnectionsystemandphaseportraitofthecor-

responding GOMIBsystem. . . 99

8.11 Case 4: Variation of P vs. time in the Brazilian North{

Southinterconnectionsystemandphaseportraitofthecor-

responding GOMIBsystem. . . 100

8.12 Case 5: Variation of P vs. time in the Brazilian North{

South interconnection system. . . 101

8.13 Phase portraitof theGOMIB systemof thetest system. . 102

9.1 Phase portrait ofthe systemfork = 3(dotted line)and

k = 2 (dashed line, and also solid lines which are indeed

the eigenvectors). . . 106

9.2 Phase portraitof thesystemcontrolledbyVSC,c

1

=

1

. 107

9.3 Phase portrait of the system when g

1

< 

1 and g

1

> 

1 ,

respectively. . . 108

9.4 Phase portrait of the OMIB system after the fault, when

CSC is controlled by CLF and VSC with sliding mode,

respectively. . . 114

9.5 Phase portrait of the OMIB system after the fault, when

an energy function(dottedline) and a Lyapunov function

(solidline)areusedforderivingthecontrollaw,respectively. 116

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Introduction

1.1 Background and Motivation of Project

Historically,power systems were designed and operated with large mar-

gins. Itwascomparativelyeasytomatchloadgrowthwithnewgeneration

and transmission equipment. So, systems normallyoperated ina region

where behavior was fairly linear. Only occasionally would systems be

forced to extremes wherenonlinearitiescould begin to have some signi -

cant e ect. However, because of politicaland environmentalissues, such

as thebuilding and the locations of new generation and impedimentsof

thebuildingtransmissionfacilities,there isagreaterneedtomake maxi-

mumuseof existingfacilities. Asaconsequence, some transmissionlines

becomemoreloadedthanwasplanned(whentheywerebuilt)whichleads

toreducedpowersystemdampingofoscillationsandtodecreasedsystem

stabilitymargins. Also,astheelectricityindustrymovestowardanopen

access market, operating strategies will become much less predictable.

Hence,therelianceonnearly linearbehavior(whichwasadequateinthe

past)mustgivewaytoanacceptancethatnonlinearitiesaregoingtoplay

an increasinglyimportant role inpower systemoperation. Itis therefore

vital that analysis tools perform accurately and reliablyin the presence

of nonlinearities[1 ].

Development of devicesforincreasing the transmissioncapacity of lines,

and controlling thepower owin transmissionsystemgoeson presently.

Manyofthesenewapparatusescan bematerializedonlydueto thelatest

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development in high{power electronics to be used in the main circuits 1

combined withcontrolstrategies thatrelyon themoderncontrolsystem

software and hardware.

ByusingpowerelectronicscontrollersaFlexibleACTransmissionSystem

(FACTS) can be produced which o ers greater control of power ow,

secure loading and dampingof powersystem oscillations[2 ]. The device

conceptscanbeclassi edintothoseoperatinginshuntwiththepowerline

in which cases the injected currents are controlled, and those operating

in series with the power line in which cases the inserted voltages are

controlled. The rst category includes system components, such as the

Static Var Compensator (SVC),and thelatter category includessystem

components, such as

 Uni edPowerFlowController(UPFC)

 Controllable SeriesCapacitor (CSC)

 Quadrature BoostingTransformer(QBT)

which all henceforth will be called Controllable Series Devices (CSDs).

Application of these devicesto power ow control and damping control

in electricpowersystems isdescribedin[3 ].

Generally, in the modeling of such devices for studies of power system

behavior,thefastswitchingactioninherentinpowerelectronicsisignored.

Instead,thedevicesarerepresentedbyapproximatemodelswhichexhibit

continuousbehavior. Theaimistoensurethattheexactandapproximate

representations have asimilar\average" e ect on thesystem. Ofcourse,

anyphysicallimitationsintheactualdevicemustbeaccurately re ected

in theapproximatemodel[1 ].

1.2 Aims of the Performed Work

Modern power systems are large scale and complex. Disturbances typ-

ically change the network topology and result in nonlinear system re-

sponse. Also, because of deregulation the con guration of the intercon-

nected grid will routinely be in a state of change. Therefore, the tradi-

tionalcontrollawsbasedonlinearizedsystemmodelsareoftenof limited

1

Thecircuitsofthedevicewherethepoweris owingareusuallyreferredtoasmain

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value. Thus, a control strategy that will counteract a wide variety of

disturbancesthatmayoccur inthepowersystemis attractive.

The aim of this project is to investigate and evaluate the enhancement

of the performance of the control laws which are derived for nonlinear

systems. Also,aquestionofgreatimportanceistheselectionoftheinput

signalsfortheCSDsinordertodamppoweroscillationsinane ectiveand

robust manner. For a CSD controller sited in the transmission system,

it is attractive to extract an input signal from the locally measurable

quantitiesat thecontrollerlocation.

In the rstpart of theproject,two controlstrategies, namely:

 Variable StructureControl

 EnergyFunction Method

were studied and the results were reported in [4]{[6]. It was concluded

that the Energy Function Method was more suitable than the Variable

Structure Control for controlling CSDs in a multi{machine power sys-

tem. Therefore, furtherresearch regarding EnergyFunctionMethodwas

motivated.

It shouldbe noted that Energy Function Method will henceforth be re-

named to ControlLyapunovFunction(CLF).

The overall aim of the research of this part of the project is to try to

resolve some issuesregardingCLFand verifyits applicabilityto realistic

powersystems. The followingtopicsareplannedto be addressed:

 In uence oflosses.

 In uence ofmore detailedmodels.

 Use oflocal inputsignalsand coordinationof di erentcontrollers.

These itemswillbeelaborated below.

SofarControlLyapunovFunction(CLF) isprovento workinpowersys-

temswithoutlosses. Oneissue istheunavailabilityof CLFto e ectively

handle power system losses, where the losses are either from transmis-

sion systems or from the transfer conductances in the reduced system

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theoretical problem. Thisproblemisalso validwhenvoltage dependence

of realloadsandmore detailedmodelsofsynchronousmachinesincluded

AutomaticVoltageregulator(AVR)andturbineregulatorareconsidered.

Oneoftheaimsoftheproposedprojectistostudythee ectsthatcanbe

expectedwhencontrollawsfortheCSDs(whicharebaseduponsimpli ed

system models)are appliedto realisticsystems.

In the somewhat simpli edmodelused to derive theCLF based control

law, it can be veri edthat localinputsignals, e.g. power ows on lines,

can successfully be usedto damp power oscillations. However, there are

twoissuesthatwillbeinvestigatedfurtherinthisprojecttogainabetter

basis andunderstanding,namely:

 ArelocalsignalssuÆcientalsowhenmorecomplicatedandrealistic

modelsofthepowersystemcomponentsare used?

 Even ifit can be proven thatlocalsignalscan stabilizethesystem,

a remote input signal may be more e ective for this purpose. A

pertinent questionis forwhich power systemconditions thisis the

case.

Arelatedquestion(atleastfromatheoreticalpointofview)concernsthe

coordination ofseveral CSD controller. A relevant questionis then:

 Do CSDswithCLFcontroladverselya ect each other?

Theaimoftheprojectistoanswertheabovequestionsthroughanalytical

work andsimulationsof realisticpowersystems.

The project can be seen asa very natural extensionand continuationof

theworkdoneatthedepartmentandreportedin[7 ]. Theemphasisin[7]

wason (steady{state)power owcontrolandonlinearanalysisofpower

systems with CSDs, butsome possibilitiesof nonlinearcontrolwere also

brie y investigated.

TheprojectwasalsocoordinatedwithaprojectbytheNUTEKREGINA

projectonCoordinatedandRobust ControlofPowerSystemswhichwas

reportedin[8 ]. Themainissuesof[8 ]involvethedesignofcontrolstrate-

gies ofpowersystemsforthecasewhenseveralinteractingcontrollersare

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the project reported in [8 ] have some points of interactions which were

coordinated,anditisbelievedthatthesetwoprojectshavebene tedfrom

each other infruitfulway.

Another project was dealing with damping of power oscillations by use

of High Voltage Direct Current (HVDC) systems and was reported in

[9]. Many of the questions and problems of the proposed project are

similarto thoseof[9 ],butthestudiedsolutionsareofcoursedi erent. A

fruitfulinteractiontookalsoplaceinthiscase. Allthedescribedprojects

together are part of long term plan of the department to develop and

investigate the possibilities and virtues of controllable devices in power

systems. Thisplanincludesalsothedevelopmentofrelevantanalysisand

simulation tools.

1.3 Outline of the Thesis

Chapter 2 brie y explains the e ects and consequence of power system

oscillationsinapowersystem. Thischapter alsooutlineshowthese oscil-

lationsaremitigatedinapowersystem. Discussioninthischapterlargely

follows thatin[10 ] and referencestherein.

Chapter3presentsthemathematicalmodelsforapowersystemrequired

in formulating the stability problem. Both Reduced Network Model

(RNM) and Structure Preserving Model (SPM) are presented in this

chapter. Discussion inthis chapter largely follows that in [11 ], [12 ] and

referencestherein.

Chapter 4 explains the operating principles of the Uni ed Power Flow

Controller (UPFC), the Quadrature Boosting Transformer (QBT) and

ControllableSeries Capacitor(CSC). A generalmodelisalso derived for

thesedevices. Thismodelwhichisreferredtoasinjectionmodel,ishelpful

forunderstandingthe impactof these componentson power systems.

Chapter 5starts byreviewingsome relevant conceptsfromnonlineardy-

namicalsystems theory. Then,this chapter analyzesstabilityof equilib-

riumpointsbyapplyingLyapunovtheorems. Formechanicalandelectri-

calsystems,thephysicalenergy(orenergy{like)functionsareoftenused

as Lyapunov function candidates. The time derivatives of these energy

functionsarehowevernegativesemide nite,andtherefore,thesefunctions

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applyingtheLaSalle'sinvarianceprincipleandthetheoremofBarbashin

and Krasovskii,theasymptoticstabilityofan equilibriumpointcan also

be justi ed by the energy functions. Discussion in this chapter largely

follows that in[13 ]{[16].

Chapter 6 introducesthe concept ofControlLyapunovFunctionfor sys-

tems withcontrolinput. Theso{called aÆnesystems arestudied inthis

chapter. Discussion inthischapter largely follows thatin[17 ] and refer-

ences therein.

Chapter 7 provides the results of numerical examples. In this chapter,

thecontrollaws derivedinChapter6areappliedto varioustest systems.

Chapter 8 introduces theconcept of SIngle Machine Equivalent (SIME).

SIMEisahybriddirect-temporaltransientstabilitymethod,whichtrans-

formsthetrajectoriesofamulti{machinepowersystemintothetrajectory

of a Generalized One{Machine In niteBus (GOMIB)system. Basically,

SIMEdealswiththepost-faultcon gurationofapowersystemsubjected

to a disturbance which presumably drives it to instability. Under such

condition,SIMEusesatime{domainsimulationprograminordertoiden-

tifythemode ofseparationofits machinesintotwo groups,namely,crit-

ical and non-critical machines which are replaced by successivelya two{

machine equivalent. Then,this two{machine equivalent is replaced bya

GOMIB system. Discussioninthischapter largely followsthat in[12 ].

Chapter 9 introduces the concept of Variable Structure Control (VSC)

and VSC with sliding mode. With VSC, dynamical systems are con-

trolledwithdiscontinuousfeedbackcontrollers. VSC hasbeendeveloped

duringthelastfourdecades,andischaracterizedbyacontrollawwhichis

designed todrivethesystemtrajectoriesonto aspeci edline(orsurface)

in the state space. The slidingmode describesthe particular case when

the system trajectories are constrained to lie upon a line (or surface).

Discussion inthischapter largelyfollowsthat in[44 ] and[48 ].

Finally,inChapter 10,weprovidethe conclusionsand alsosome sugges-

tions forfutureworkare given.

1.4 List of Publications

Work performed duringthis projecthas beenpublished inthe following

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1. M. Norrozian,L.



Angquist,M.GhandhariandG. Andersson, \Use

of UPFC for Optimal Power Flow Control", Proceedings of Stock-

holm Power Tech., pp. 506{511, June1995.

2. M.Norrozian,L.



Angquist,M.GhandhariandG.Andersson,\Series{

Connected FACTS Devices Control Strategy for Damping of Elec-

tromechanical Oscillations", Proceedings of 12 th

PSCC, pp. 1090{

1096, August 1996.

3. M. Norrozian,L.



Angquist,M. GhandhariandG. Andersson, \Use

ofUPFCforOptimalPowerFlowControl", IEEETrans. onPower

Delivery, Vol. 12, No. 4,pp. 1629{1635, October1997.

4. M. Norrozian,L.



Angquist,M. GhandhariandG.Andersson, \Im-

provingPowerSystem Dynamics bySeries{Connected FACTS De-

vices", IEEE Trans. on Power Delivery, Vol. 12, No. 4, pp.

1636{1642, October1997.

5. M.Ghandhari,G.Andersson,M.NorrozianandL.



Angquist,\Non-

linearControlofControllableSeriesDevices(CSD)",Proceedingsof

the 29 th

North American Power Symposium (NAPS), pp. 398{403,

October1997.

6. M. Ghandhari, Control ofPowerOscillations inTransmission Sys-

tems Using Controllable Series Devices, Licentiate Thesis, Royal

Institute of Technology, TRITA{EES{9705, ISSN1100{1607, 1997.

7. M. Ghandhariand G. Andersson, \Two Various ControlLaws for

Controllable Series Capacitor (CSC)", Power Tech. Budapest 99,

September1999.

8. M. Ghandhari and G. Andersson, \A Damping Control Strategy

for Controllable Series Capacitor (CSC)", Proceedings of the 31 th

NorthAmerican PowerSymposium (NAPS), pp. 398{403,October

1999.

9. M.Ghandhari,G.AnderssonandI.A.Hiskens, \ControlLyapunov

Functions for Controllable Series Devices", SEPOPE, Brazil, (in-

vited paper), May2000.

10. M. Ghandhari, G. Andersson and I. A. Hiskens, \Control Lya-

punov Functions for Controllable Series Devices", Submitted to

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11. M.Ghandhari,G.Andersson,D.ErnstandM. Pavella, \AControl

Strategy for Controllable Series Capacitor in Electric power Sys-

tems", Submitted to Automatica.

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Power System Oscillations

Anelectricalpowersystemconsistsofmanyindividualelementsconnected

together to form a large, complex system capable of generating, trans-

mittingand distributing electricalenergy over a largegeographical area.

Because of this interconnection of elements, a large variety of dynamic

interactionsarepossible,someof whichwillonlya ectsome ofelements,

otherswilla ect partsof thesystem, whileothers maya ect thesystem

asa whole.

Ingeneral, powersystemstabilitycanbedividedinto(rotor)anglestabil-

ityand voltage stability. In thisthesis, the angle stabilityis considered.

Power system stability is a term applied to alternating current electric

power systems, denoting a condition in which the various synchronous

machinesofthe systemremain \insynchronism", or\instep" with each

other. Conversely,instabilitydenotes a conditioninvolving \lossof syn-

chronism", or falling \out of step" [19 ]. The stability problem involves

thestudyoftheelectromechanicaloscillationsinherentinpowersystems.

Power systems exhibit various modes of oscillation due to interactions

among system components. Many of the oscillations are due to syn-

chronousgeneratorrotorsswingingrelativetoeachother. Theelectrome-

chanical modes involving these masses usually occur in the frequency

range of 0.1 to 2 Hz. Particularly troublesome are the interarea oscil-

lations, which typically are in the frequency range of 0.1 to 1 Hz. The

interarea modesareusuallyassociatedwithgroupsof machinesswinging

relative to other groupsacross a relativelyweak transmissionpath. The

higher frequency electromechanical modes (1 to 2 Hz) typically involve

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one or two generators swinging against the rest of the power system or

electrically close machinesswinging against each other (called also local

modes). Inmanysystems,thedampingofthese electromechanical swing

modesis acritical factor foroperating ina securemanner.

Becauseofpoliticalandenvironmentalissues,suchasthebuildingandthe

locationsofnewgenerationandimpedimentsofthebuildingtransmission

facilities,there is agreater needto make maximumuseof existingfacili-

ties. Asaconsequence,sometransmissionlinesbecomemoreloadedthan

was plannedwhen they were built. In particular, heavy power transfers

can create interareadamping problemsthat constrain systemoperation.

The oscillationsthemselves maybe triggeredthroughsome event ordis-

turbance on the power system orbyshiftingthe system operatingpoint

across some steady-state stability boundary where oscillations may be

spontaneously created. Controller proliferation makes such boundaries

increasingly diÆcult to anticipate. Once started, undamped oscillations

oftengrowinmagnitudeoverthespanofmanyseconds. Theseoscillations

maypersistformanyminutesandbelimitedinamplitudeonlybysystem

nonlinearities. In some cases, large generator groups loose synchronism

and part orall of the electrical network is lost. The same e ect can be

reachedthrough slow cascading outages when theoscillationsare strong

and persistent enough to cause uncoordinated automatic disconnection

of key generators or loads. Sustained oscillationscan disrupt the power

systeminotherways,evenwhentheydonotproducenetworkseparation

orlossof resources. Forexample, powerswingsthatarenottroublesome

inthemselvesmayhaveassociatedvoltageorfrequencyswings,whichare

unacceptable. Such considerations can limit power transfers even when

stabilityis notadirect concern.

2.1 Sources of Mitigating Power System

Oscillations

The torqueswhichin uencethemachineoscillationscanbeconceptually

split into synchronizing and damping components of torque. The syn-

chronizingcomponent\holds"themachinestogetherandisimportantfor

system transient stabilityfollowing largedisturbances. For smalldistur-

bances, thesynchronizingcomponent oftorquedeterminesthefrequency

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The damping component determinesthe decay of oscillationsand isim-

portant for system stability following recovery from the initial swing.

Damping is in uenced by many system parameters. It is usually small

and can sometimes become negative in the presence of controls, which

arepracticallytheonly\source"ofnegative damping. Negativedamping

can lead to spontaneous growth of oscillations until relays begin to trip

systemelements.

Much history existsin thepowersystem literatureon the application of

supplemental modulation controls to existing regulators in order to aid

dampingofpowerswings. Whenadevice,itsregulatorandsupplemental

controlareaddedtothepowersystem,theymustoperatesatisfactorilyin

thepresenceofmultiplepowerswingmodesoverawiderangeofoperating

conditions.

Conventionally,thedampingofpowersystemoscillationsisperformedby

Power System Stabilizer (PSS) which is an added device to Automatic

VoltageRegulator(AVR)ofthegenerator. ThebasicfunctionofthePSS

isto extendstabilitylimitsbymodulatinggenerator voltage throughthe

exciter to provide positive damping torque to power swing modes. By

modulatingtheterminalvoltage thePSSa ectsthepower owfromthe

generator,whicheÆcientlydampslocalmodes. PSShasthedisadvantage

of working through the same element that had resulted in the negative

damping originally. Also, the achievable damping of interarea modes is

lessthanthatoflocalmodes. Sincesystemdampingissmallatbest,itis

reasonable to use new devicesfor more damping. For e ective damping

withoutdisturbingthenetworksynchronizingtorques,itisessentialthat

the damping device generate a torque whose phase is precisely de ned

andcanoperatecontinuously. Thesesrequirementsseembestsatis edby

thefast responseand staticcharacter of powerelectronicsdevices.

In recent years, the fast progress in the eld of power electronics has

opened new opportunities for the power industry via utilization of the

FACTS deviceswhich o er an alternative means to mitigate power sys-

tem oscillations. Theyareoperated synchronouslywiththetransmission

lineand maybeconnectedeitherinparallelproducingcontrollableshunt

reactive current forvoltage regulation,or inserieswith theline forcon-

trollingpower owon thetransmissionline.

Unlike PSS control at a generator location, the speed deviations of the

machinesofinterestusedasinputsignals(measurements)arenotreadily

(28)

since the usualintent is to damp interarea modes, which involve a large

number of generators, speed signals themselves are not necessarily the

best choice for an input signal for devices in the transmission line. For

the FACTS devices, it is typically desirable to extract an input signal

from locally measurable quantities. Selectingappropriate measurements

is usuallya very mostimportant aspect ofcontroldesign.

2.2 Summary

Power systems exhibit various modes of oscillation due to interactions

among system components. Particularly troublesome are the interarea

oscillations, which typically are in the frequency range of 0.1 to 1 Hz.

Conventionally,thedampingofpowersystemoscillationsisperformedby

Power System Stabilizer(PSS).However, dueto the fastprogress inthe

eld of power electronics, the FACTS deviceso er an alternative means

to mitigatepowersystemoscillations.

(29)

Modeling of Power Systems

In thischapter, themathematical modelsforapowersystemrequired in

formulating thestabilityproblem willbe presented. Both Reduced Net-

workModel(RNM)andStructurePreservingModel(SPM)arepresented

inthischapter.

Figure3.1showsamulti{machinepowersystemwhichhasatotalofn+N

nodesof whichthe rst nare internalmachine nodes and theremaining

N areloadbuses, thatis,networknodes.

Transmission Network GEN 1

1 1

n n

V + Ð G +

2 2

n n

V + Ð G +

2 n 2 n

V Ð G

1 1

E @ ¢Ð

2 2

E @ ¢Ð

n n

E @ ¢Ð

1

jx¢ d

2

jx¢ d

jx¢ dn

2 1 n 2 1 n

V + Ð G +

2 2 n 2 2 n

V + Ð G +

n N n N

V + Ð G +

GEN 2

GEN n

Figure3.1. Amulti{machinepowersystem.

In Figure 3.1,



E 0

k

=E 0

k

6

Æ

k

(k =1n) is the internal machine voltage

phasorbehind the transient reactance x 0

dk

which includesthe reactance

(30)

of transformer. E 0

k

is themagnitudeof theinternal machine voltage and

Æ

k

is the internal machine angle of the k{th machine. All the angles

are measured with respect to a synchronously rotating reference in the

system.



V

k

=V

k

6



k

(k=n+1n+N) is theload busvoltage phasor

with magnitudeV

k

and phase angle

k .

Historically, loads are presented by the following three types or models

in terms of their load voltage characteristics (also called \static loads"),

namely:

 Constant power

 Constant current

 Constant impedance

They form fundamental basis in modeling a majority of loads with the

exceptionofsomemotorloadsrequiringspecialconsiderationduringlarge

disturbances. Astatic load isdescribedby

P

L

=P

Lo (

V

V

o )

mp

Q

L

=Q

Lo (

V

V

o )

mq

(3.1)

where P

Lo

and Q

Lo

are the active and reactive powers at the nominal

voltage V

o

, respectively. mp and mq are the voltage exponents of the

activepowerandthereactive powerwhichcanassumeanyvalueranging

from 0to 3 basedon thenature ofthecompositeloadcharacteristic ata

given bus. V is thecurrent voltage.

Having mp =mq =0, the active and reactive components of the static

load have constant power characteristics. For mp = mq = 1 and mp =

mq =2,the active and reactive componentsof the static load have con-

stant current and constant impedancecharacteristics, respectively.

Afrequentlyusedrepresentationofthestaticloadsasfunctionsofvoltage

and frequencydeviationsmay be writtenas(also calledZIPmodel)

P

L

=P

Lo (a

0 V

0

+a

1 V

1

+a

2 V

2

)(1+k

P

f)

Q

L

=Q

Lo (b

0 V

0

+b

1 V

1

+b

2 V

2

)(1+k

Q

f)

(3.2)

wherea

i ,b

i ,k

P andk

Q

aretherespectivevoltageandfrequencysensitivity

(31)

3.1 Reduced Network Model

The Reduced Network Model (RNM) is based on the following assump-

tions:

 The various network components are assumed to be insensitive to

changes infrequency.

 Each synchronousmachine isrepresented bya voltage phasorwith

constant magnitudeE 0

behind itstransientreactance.

 Themechanicalangle ofthesynchronousmachinerotor isassumed

to coincide with the electrical phase angle of the voltage phasor

behindthetransient reactance.

 Loads are represented asconstant impedances, i.e. mp= mq = 2

in(3.1).

 Mechanical powerinputto generatorsis assumedconstant.

 Saliencyis neglected,i.e. x 0

d

=x 0

q .

 Stator resistance isneglected.

This is the simplest power system model used in stabilitystudies. It is

usuallylimited to analysisof rst{swingtransients.

Power systems are most naturally described by Di erential{Algebraic

Equations(DAE).Anadvantageoftheassumptionofconstantimpedance

loads is that it is possible to eliminate the network nodes to obtain an

equivalent systemwhichonlyconsistsof nonlineardi erentialequations.

Thisis achieved bythefollowingsteps:

1. Performa pre{fault load owcalculation. Calculate theequivalent

steady{state impedance loadsin theform ofadmittances as

 y

Lk

= P

Lk jQ

Lk

V 2

k

; k =n+1n+N

foreach loadbus, and add theseelementsto the



Y matrix.

(32)

2. Calculatetheinternalmachinevoltagesbehindtransientreactances

as



E 0

k

=



V

n+k +jx

0

dk P

Gk jQ

Gk



V



n+k

; k=1n

foreach of thenmachines.

3. Augmentthe



Y

bus

matrixbyadmittances corresponding tothema-

chine transient reactances as

 y

k

= 1

jx 0

dk

; k=1n

to create theninternal machine nodes.

4. Thisaugmentedadmittancematrixcansymbolicallybepartitioned

as

n N

^



Y

BUS

=





Y

A



Y

B



Y

C



Y

D



n

N

The relation between injected currents and node voltages is now

given by





I

G

0



=





Y

A



Y

B



Y

C



Y

D

 



E

G



V

L



where



E

G

isthevector of theinternalmachinevoltages behindthetran-

sient reactances and



V

L

isthe vector of loadbus voltages. Since there is

no injectedcurrentsinthenetwork nodes,thissystemcan bereducedto

internalmachinenodesas



I

G

=(



Y

A



Y

B



Y 1

D



Y

C )



E

G

=



Y

int



E

G

The powerinjectedintheinternalmachinenodek can nowbecalculated

by

P

Gk

=R ef



E 0

k



I



Gk g

=E 0

k 2

G

kk +

n

X

l=1

l6=k E

0

k E

0

l (B

kl sin(Æ

kl )+G

kl cos(Æ

kl ))

(3.3)

(33)

Æ

kl

k Æ

l

G

kk

isthe short-circuitconductanceof thek{thmachine.

G

kl

isthe transferconductance in



Y

int

,k6=l.

B

kl

isthetransfer susceptancein



Y

int

,k 6=l.

Let

C

kl

=E 0

k E

0

l B

kl

F

kl

=E 0

k E

0

l G

kl

(3.4)

Now, themotion ofthek{thmachine isgiven by (k =1n)

_

Æ

k

=!

k

M

k _

!

k

=P

mk D

k

!

k P

Gk

(3.5)

or

_

Æ

k

=!

k

M

k _

!

k

=P

k D

k

!

k n

X

l=1

l6=k (C

kl sin(Æ

kl )+F

kl cos (Æ

kl ))

(3.6)

where

P

k

=P

mk E

0

k 2

G

kk

P

mk

isthe mechanical power inputto thek{thmachine.

D

k

>0 isthedamping constant ofthe k{thmachine.

M

k

>0is themoment of inertiaconstant of thek{thmachine.

!

k

is the rotor speed deviation of the machine k with respect to a syn-

chronouslyrotating reference.

Intheanalysisofanglestability,thefocusofattention isonthebehavior

of the machine angles with respect to each other. In order to clearly

distinguishbetweentheforcesthatacceleratethewholesystemandthose

(34)

are transformed into the Center Of Inertia (COI) reference frame. The

positionofthe COIisde nedby

Æ

COI

= 1

M

T n

X

k=1 M

k Æ

k

; M

T

= n

X

k=1 M

k

(3.7)

Next, thestate variablesÆ

k and !

k

aretransformedto theCOIvariables

as

~

Æ

k

= Æ

k Æ

COI

~

!

k

= !

k

!

COI

These COIvariablesareconstrainedby

n

X

k=1 M

k

~

Æ

k

=0

n

X

k=1 M

k

~

!

k

=0

(3.8)

Swing equations (3.6) can now be rewritten in the COIreference frame

as (k=1n)

_

~

Æ

k

=!~

k

_

~

!

k

= 1

M

k [P

k n

X

l=1

l6=k C

kl sin(Æ

kl )+

M

k

M

T P

COI D

k

~

!

k ]

1

M

k n

X

l=1

l6=k F

kl cos (Æ

kl )

=f

k +p

k

(3.9)

where

P

COI

= n

X

k=1 (P

mk P

Gk )

f

k

= 1

M

k [P

k n

X

l=1

l6=k C

kl sin(Æ

kl )+

M

k

M

T P

COI D

k

~

!

k ]

p

k

= 1

M

k n

X

l=1 F

kl cos (Æ

kl )

(3.10)

(35)

Note that

~

Æ

kl

=

~

Æ

k

~

Æ

l

kl

and uniformdampingis considered.

System (3.9) can indeedbe consideredasanOrdinaryDi erentialEqua-

tion (ODE)of theform

_

x=F(x)=f

o

(x)+p(x) (3.11)

wherex=[

~

Æ !~] T

is thevector of thestate variables. In (3.11)

f

o

(x)=[!~ [f

1

f

n ]]

T

; p(x)=[0 [p

1

 p

n ]]

T

and

~

Æ=[

~

Æ

1



~

Æ

n

] ; !~ =[!~

1

 !~

n ]

3.2 Structure Preserving Model

It is known that load characteristics have a signi cant e ect on system

dynamics. Inaccurateloadmodelingmayleadto apowersystemoperat-

ing in modes that result inactual system collapse or separation. In the

Reduced Network Model (RNM), impedance loads are assumed. Hence,

inthe context of systemmodeling,RNM precludesconsiderationof load

behaviors (i.e. voltage and frequencyvariations) at load buses. Further-

more, in the context of physical explanation of results, reduction of the

transmissionnetworkleadsto lossof network topology.

Structure Preserving Model (SPM) have beenproposed( rst in [20 ]) to

overcomesomeoftheshortcomingsoftheRNM,andtoimprovethemod-

elingofgeneratorsandloadrepresentations. An advantageof usingSPM

isthatfromamodelingviewpoint,itallowsmorerealisticrepresentations

of powersystem components,especiallyload behaviors.

Consider again themulti{machine powersystem shownin Figure3.1. It

is assumed that the mechanical power input is constant and the stator

resistance is neglected. The one{axis generator model is used for the

generators. This model includesone circuit for the eld winding of the

rotor, i.e. thismodel considers thee ects of eld ux decay. Note that

in theone{axis generator model, thevoltage behindthe direct transient

reactance is no longer a constant. The loads are modeled by equation

(3.1) withmp=0 andarbitrary mq. Thetransmissionlinesaregiven by

(36)

loads and the d{axis transient reactances x 0

d

. The kl{th element of the

admittance matrixis de ned by



Y

kl

=G

kl +jB

kl

, whereG

kl

represents

solely the resistances of the respective transmission lines. In general,

because ofthehigh ratioof reactance toresistance, thetransmissionline

resistances can be neglected. Thus,



Y

kl

=jB

kl .

The dynamics of the k{th generator are described by the following dif-

ferentialequationswithrespectto theCOIreference frame. Notethatin

the followingequations

~

Æ

k

~



l

k



l and

~



k

~



l

=

k



l

. Thus, for

k =1n

_

~

Æ

k

=!~

k

M

k _

~

!

k

=P

mk P

Gk D

k

~

!

k M

k

M

T P

COI

T 0

dok _

E 0

qk

= x

dk x

0

dk

x 0

dk V

n+k cos (Æ

k



n+k )

+E

fdk x

dk

x 0

dk E

0

qk

(3.12)

where

P

Gk

= 1

x 0

dk E

0

qk V

n+k sin(Æ

k



n+k )

x 0

dk x

qk

2x 0

dk x

qk V

2

n+k

sin(2(Æ

k



n+k ))

(3.13)

P

COI

isgiven by (3.10).

x

dk ,x

qk

arethed{axisandtheq{axissynchronousreactances ofthek{th

machine.

E 0

qk

istheq-axisvoltage behindtransientreactanceof thek{thmachine.

T 0

dok

is the d{axis transient open{circuit time constant of the k{th ma-

chine.

E

fdk

istheexcitervoltageofthek{thmachinewhichisassumedconstant.

E

fd

can be either constant ( xed excitation) or can vary due to Auto-

matic Voltage Regulator (AVR) action. When theexciter controlaction

is included in the generator model, due to AVR modeling, at least one

(37)

For the lossless system the following equations can be written at bus k

whereP

k

istherealpowerandQ

k

isthereactive powerinjected intothe

systemfrom busk.

For k=(n+1)2n

P

k

= n+N

X

l =n+1 B

kl V

k V

l sin(

k



l )+

E 0

q(k n) V

k sin(

k Æ

k n )

x 0

d(k n)

+ x

0

d(k n) x

q(k n)

2x 0

d(k n) x

q(k n) V

2

k

sin(2(

k Æ

k n ))

Q

k

=

n+N

X

l =n+1 B

kl V

k V

l cos(

k



l )+

V 2

k E

0

q(k n) V

k cos (

k Æ

k n )

x 0

d(k n)

x 0

d(k n) x

q(k n)

2x 0

d(k n) x

q(k n) V

2

k

[cos (2(

k Æ

k n )) 1]

and fork =(2n+1)(n+N)

P

k

=

n+N

X

l =n+1 B

kl V

k V

l sin(

k



l )

Q

k

=

n+N

X

l =n+1 B

kl V

k V

l cos (

k



l )

Therefore, for k = (n+1)(n+N) the power ow equations can be

writtenas

P

k +P

Lk

= 0

Q

k +Q

Lk

= 0

(3.14)

3.3 Summary

Dynamicsofmulti{machinepowersystems aredescribedbytheReduced

Network Model ortheStructure PreservingModel. IntheReduced Net-

workModelimpedanceloadsareassumed. Thus,itispossibletoeliminate

(38)

nonlinear di erential equations. However, in thecontext of physicalex-

planation of results, reduction of the transmission network leads to loss

of networktopology.

In the Structure Preserving Model, dynamics of multi{machine power

systems are described by Di erential{Algebraic Equations. Thus, from

a modeling viewpoint, it allows more realistic representations of power

system components,especiallyload behaviors.

(39)

Modeling of Controllable

Series Devices

In this chapter, the operating principles of a Uni ed Power Flow Con-

troller (UPFC), a Quadrature Boosting Transformer (QBT) and a Con-

trollable Series Capacitor (CSC) are described. Also, a general model

is derived for these devices. The models are derived in a single{phase

positive{sequencephasorframe. Thismodelwhichisreferredto asinjec-

tion model,is helpfulfor understandingthe impact ofthese components

on power systems. Furthermore, this model can easily be implemented

intoexistent powersystemanalysis programs.

4.1 Operating Principle of Controllable Series

Devices

4.1.1 Uni ed Power Flow Controller

A uni edpower ow controller consists of two voltage source converters

[21 ]. Theseconverters areoperated froma commonDC linkprovidedby

a DC capacitor, see Figure 4.1. Converter 2 provides the main function

oftheUPFCbyinjectinganACvoltagewithcontrollablemagnitudeand

phase angle in serieswith the transmissionline via a seriestransformer.

The basic function of converter 1 is to supply or absorb the real power

demand by converter 2 at the common DC link. Converter 1 can also

(40)

generate or absorb controllable reactive power ifit is desired. This con-

vertercan thereby provideindependent shunt reactive compensation for

the line. Converter 2 supplies or absorbs locally the required reactive

power, and exchanges the active power asa result of the seriesinjection

voltage.

Converter 1

Converter 2

Series transformer Shunt

transformer

V i V j

ij ij

P + jQ

ji ji

P + jQ V se

Figure4.1. BasiccircuitarrangementofaUPFC.

4.1.2 Quadrature Boosting Transformer

Based on feasible semiconductor switches and converter topologies for

high{powerapplications,di erentPhase ShiftingTransformer(PST)cir-

cuitcon gurationsareidenti ed. Inthisthesis,theso{calledQuadrature

Boosting Transformer (QBT) (i.e. the injected voltage is perpendicular

to the inputterminal voltage) is considered. Figure 4.2 shows the basic

circuit of a Quadrature Boosting Transformer (QBT). The phase angle

di erencebetweentheQBTterminalvoltages isachievedbyseriallycon-

necting a Boosting Transformer (BT) into the transmission line. The

powerwhichisinjectedinto thetransmissionlinebythisboostingtrans-

former must be taken from the network by the Excitation Transformer

(ET). Theconvertercontrolsthemagnitudeandthephase angleof



V

se .

4.1.3 Controllable Series Capacitor

A Controllable SeriesCapacitor (CSC)can bematerialized byThyristor

(41)

Converter

BT ET

V i V j

ij ij

P + jQ

ji ji

P + jQ V se

Figure4.2. BasiccircuitarrangementofaQBT.

pacitors (TSSC), as shown in Figure 4.3. In a simpli ed study, a CSC

can be consideredasa continuouslycontrollable reactance (normallyca-

pacitive) whichis connectedinserieswiththetransmissionline.

TSSC TCSC

Figure4.3. Basiccircuitarrangement ofaCSC.

4.2 Injection Model

Figure4.4showstheequivalentcircuitdiagramofaCSDwhichislocated

between buses i and j in a transmission system. A UPFC and a QBT

inject a voltage



V

se

in serieswith the transmission line througha series

transformer, see Section4.1. The active power P

se

involved inthe series

injection is taken from the transmission line (i.e. P ) through a shunt

(42)

transformer. TheUPFC generates orabsorbs theneeded reactive power

(i.e. Q

se

and Q

sh

) locally by the switching operation of its converters,

whilethereactive powerQ

se

injectedinserieswiththetransmissionline

by the QBT, is taken from the transmission line (i.e. Q

sh

). In Figure

4.4, x

s

isthee ectivereactanceoftheUPFC(ortheQBT)seenfromthe

transmissionlinesideof theseriestransformer.

V i V j

jx s

V '

V se

se , se

P Q

sh sh

P Q I sh

I se

Figure 4.4. EquivalentcircuitdiagramofaCSD.

Figure 4.5 shows thevector diagramof the equivalentcircuit diagramof

a CSD.

γ

I se

V '

V se

V i

β

Figure 4.5. Vectordiagramoftheequivalentcircuitdiagram.

4.2.1 Injection Model of UPFC

ToobtainaninjectionmodelforaUPFC,we rstconsidertheseriespart

(43)

V se

V i V j

jx s

I se

V '

Figure4.6. Representationoftheseriesconnectedvoltagesource.

The seriesconnected voltage sourceismodeledbyanideal seriesvoltage



V

se

which is controllable in magnitude and phase, that is,



V

se

= r



V

i e

j

where0r r

max

and 0 2.

Theinjectionmodelisobtained(asshowninFigure4.7)byreplacingthe

voltage source



V

se

bya currentsource



I

inj

= jb

s



V

se

inparallelwith x

s .

Note thatb

s

=1=x

s .

i i i

V V G = Ð V V G j = Ð j j

jx s

I inj

Figure4.7. Replacementoftheseriesvoltagesourcebyacurrentsource.

The current source



I

inj

correspondsto injectionpowers



S

i and



S

j which

arede ned by



S

i

=



V

i (



I

inj )



= rb

s V

2

i

sin( ) jrb

s V

2

i

cos ( )



S

j

=



V

j (



I

inj )



=rb

s V

i V

j sin(

ij

)+jrb

s V

i V

j cos (

ij )

where

ij

=

i



j .

Figure4.8showstheinjectionmodeloftheseriespartoftheUPFC,where

P

i

= real(



S

i

) ; Q

i

= imag(



S

i )

P = real(



S ) ; Q = imag(



S )

(4.1)

(44)

i i i

V V G = Ð V V G j = Ð j j

jx s

i i

P jQ + P j + jQ j

Figure 4.8. InjectionmodeloftheseriespartoftheUPFC.

The apparent power supplied by the series voltage source is calculated

from



S

se

=



V

se



I



se

=re j



V

i (



V 0



V

j

jx

s )



Active and reactive powers suppliedbytheseriesvoltage sourceare dis-

tinguished as:

P

se

= rb

s V

i V

j sin(

ij

+ ) rb

s V

2

i

sin( )

Q

se

= rb

s V

i V

j cos (

ij

+ )+rb

s V

2

i

cos ( )+r 2

b

s V

2

i

AssuminganidealUPFC(i.e. lossesareneglectedintheUPFC),wehave

then P

sh

= P

se

. For the UPFC, Q

sh

is independently controllable, and

we assumethat Q

sh

=0. Note thatQ

sh

can alsohave a nonzero value.

TheinjectionmodeloftheUPFCisconstructedfromtheseriesconnected

voltage sourcemodelshown inFigure4.8byaddingP

sh +jQ

sh

to busi.

Figure 4.9 shows theinjectionmodelof theUPFC.

i i i

V V G = Ð V V G j = Ð j j

jx s

si si

P + jQ P sj + jQ sj

Figure4.9. InjectionmodeloftheUPFC.

(45)

In Figure4.9

P

si

=rb

s V

i V

j sin(

ij + )

P

sj

= P

si

Q

si

=rb

s V

2

i

cos ( )

Q

sj

= rb

s V

i V

j cos (

ij + )

(4.2)

wherer and are thecontrolvariablesofthe UPFC.

ForthepurposeofdevelopingacontrolstrategyfortheUPFC,itisuseful

to applythefollowingcontrolvariables.

Since

rsin(

ij

+ )=rcos( )sin(

ij

)+rsin( )cos(

ij )

rcos (

ij

+ )=rcos( )cos(

ij

) rsin( )sin(

ij )

(4.3)

let

u

up1

=rcos( ) ; u

up2

=rsin( ) (4.4)

Substituting(4.3) and (4.4) into (4.2),thefollowingis obtained.

P

si

=b

s V

i V

j (u

up1 sin(

ij )+u

up2 cos(

ij ))

P

sj

= P

si

Q

si

=u

up1 b

s V

2

i

Q

sj

= b

s V

i V

j (u

up1 cos(

ij ) u

up2 sin(

ij ))

(4.5)

Note that

r = q

u 2

up1 +u

2

up2

; =arctan(

u

up2

u

up1 )

4.2.2 Injection Model of QBT

The argument given in Subsection4.2.1 is also validfor constructing an

injection model for a QBT. For this device, the injected voltage



V

se is

perpendicular to the input terminal voltage



V

i

. Thus, = =2, see

Figure 4.5.

Assuming an ideal QBT (i.e. losses are neglected in theQBT), we have

then P =P

se

. Forthe QBT,the reactive powerinjected inserieswith

(46)

thetransmissionlineistakenfromtheshuntpartoftheQBT.Therefore,

Q

sh

=Q

se .

The injectionmodeloftheQBTisconstructedfromtheseriesconnected

voltage sourcemodelshown inFigure4.8byaddingP

sh +jQ

sh

to busi.

Thus, Figure4.9also showstheinjectionmodelof theQBT,where

P

si

=u

q b

s V

i V

j cos (

ij )

P

sj

= P

si

Q

si

=u

q b

s V

2

i +u

q b

s V

i V

j sin(

ij )

Q

sj

=u

q b

s V

i V

j sin(

ij )

(4.6)

In (4.6),u

q

=rsin( ) and r

max

u

q

r

max

since ==2.

Note that

r=ju

q

j ; =sgn(u

q )



2

where sgn(:)is thesign function.

4.2.3 Injection Model of CSC

SupposeaCSCisislocatedbetweenbusesiandjinalosslesstransmission

lineas showninFigure 4.10.

i i i

V V G = Ð V V G j = Ð j j

jx L - jx c I se

Figure4.10. CSClocatedinalosslesstransmissionline.

For studies involving load ow and angle stability analysis, the CSC is

modeled as a variable reactance, i.e x

c

in Figure 4.10. However, for the

purposeofdevelopinga controlstrategyandhavingsame modelsforthe

(47)

Figure 4.4 is also valid for the CSC if



I

sh

is set to zero and x

s is the

transmissionlinereactance, i.e. x

s

=x

L

. Furthermore, ==2inFigure

4.5. Thus,Figure 4.10 can bereplaced by Figure4.4 wherex

s

=x

L and



I

sh

=0. From Figure 4.10, we have



I

se

=



V

i



V

j

j(x

L x

c )

In Figure4.4,



V

se

= jx

c



I

se

and inFigure 4.7, we have



I

inj

=



V

se

jx

L

= jx

c



I

se

jx

L

= x

c

x

L



I

se

TheinjectionmodeloftheCSCisthenobtainedby(4.1). Notethatsince



I

sh

= 0, we have P

sh

=Q

sh

= 0. Thus, Figure 4.9 is also validfor the

CSC, where

P

si

=u

c b

s V

i V

j sin(

ij )

P

sj

= P

si

Q

si

=u

c b

s (V

2

i V

i V

j cos(

ij ))

Q

sj

=u

c b

s (V

2

j V

i V

j cos(

ij ))

(4.7)

and

u

c

= x

c

x

L x

c

(4.8)

4.3 Summary

The injection models of the Controllable Series Devices are derived in

a single{phase positive{sequence phasor frame. The injection model is

helpful for understanding the impact of the Controllable Series Devices

on power systems. This model can easily be used for the purpose of

developing control laws. Furthermore, this model can be implemented

intoexistent powersystemanalysis programs.

(48)
(49)

Lyapunov Stability

This chapter starts by reviewing some relevant concepts from nonlinear

dynamical systems theory. Stabilityofequilibriumpointsin thesenseof

Lyapunov is also presented. Lyapunov stabilitytheorems give suÆcient

conditionsforstability. Theydonotsaywhether thegivenconditionsare

necessary. There arehowevertheorems which establish(at least concep-

tually)thatformanyofLyapunovstabilitytheoremsthegivenconditions

areindeednecessary. SuchtheoremsareusuallycalledconverseLyapunov

theorems. Thesetheoremshavebeenabasisfortheintroductionof Con-

trolLyapunovFunctionforsystems withcontrolinput.

5.1 Mathematical Preliminaries

Considerthe nonlinearsystem

_ x=f

o

(x) (5.1)

wherexisthen{dimensionalstate vectorwhichbelongstotheEuclidean

spaceR n

. Thesystemisspeci edbythevector eldfunctionf

o

:D!R n

whichiscontinuousandhascontinuous rst-orderpartialderivativeswith

respect to x on a domain D  R n

into R n

. System (5.1) is also called

(50)

autonomous since timedoesnotappearexplicitlyinf

o

. Letthesolution

to (5.1) be given by

x(t)=(t t

o

;x

o )

where x

o

is the initial conditions and t

o

is the initial time which is ar-

bitrary. Since the dependence of the solution on the initial time is not

essential, wecan assume withoutlossof generalitythat t

o

=0. Thus,

x(t)=(t;x

o )

Since f

o

(x) is continuous, and has continuous rst-order partial deriva-

tiveswithrespecttox,asolutionto(5.1)(satisfyingtheinitialconditions

x(0) = (0;x

o ) =x

o

) exists on some time interval a<t <b containing

0, and that the time interval can be extended at both ends as long as

kf

o

[x(t)]kremainsbounded. Furthermore,thesolutionisuniqueand dif-

ferentiable inbotht and x

o .

One of themost important geometric properties of autonomous systems

of theform (5.1)is thatthere isonlyone solutionx(t)=(t;x

o

) passing

throughanygiveninitialstatex(0)=(0;x

o )=x

o

. Hence,trajectoriesin

statespacecanneverintersecteachother. Incontrast,fornonautonomous

systems, thesolution x(t)= (t;t

o

;x

o

) depends on the startingtime t

o ,

so that the solution from x

o at t

o

=0 will generally not be thesame as

the solutionstartingfromx

o

at some other initialtimet

o 6=0.

An equilibriumpoint x

e

for(5.1) is de ned byf

o (x

e

)=0. The point x

e

is Lyapunovstable (or stablein thesenseof Lyapunov) ifsolutions that

start nearx

e

remain nearx

e

forall t0. More precisely,anequilibrium

pointx

e

isLyapunovstableif forany >0 (nomatter howsmall)there

exists aÆ =Æ()>0 such thatforeveryx(0) inwhich

kx(0) x

e k<Æ

the solutionx(t)satis es

kx(t) x

e

k< ; 8t>0

If, inaddition,

kx(t) x

e

k!0 as t!1

then x

e

is asymptotically stable. An equilibrium point x

e

that is not

(51)

Lyapunov stability of a solution to a system of nonlinear equations (at

least locally) can be de ned by examining the linearized equations of

motion. ThisapproachisknownasLyapunov's rst(orindirect)method.

Linearizingthenonlinearsystem(5.1)aroundanequilibriumpointx

e ,we

obtain

x_ =Ax

where

A=



@f

o (x)

@x



x=x

e

= 2

6

6

4

@f

1 (x)

@x

1



@f

1 (x)

@xn

.

.

. .

.

. .

.

.

@f

n (x)

@x

1



@f

n (x)

@x

n 3

7

7

5

x=x

e

whichisalsocalledtheJacobianmatrixat x

e

. We sayx

e

ishyperbolicif

Ahasnoeigenvalues()withzerorealpart. MatrixAiscalledastability

matrixora Hurwitzmatrixif alleigenvaluesof AsatisfyR e

i

<0.

Theorem 5.1. Let x

e

be an equilibrium point for the nonlinear system

(5.1) . Then,

1. x

e

isasymptotically stableif A is a Hurwitz matrix.

2. x

e

isexponentially stable if andonly if A is a Hurwitzmatrix.

3. x

e

isunstable if R e

i

>0 for one or more of the eigenvalues of A.

The proof can be foundin[13 ].

Anasymptoticallyorexponentiallystableequilibriumpointishenceforth

denoted by x

s

. A few topological concepts of R n

are reviewed in the

following. Thestabilityregionofx

s

(denotedbyS(x

s

))isaregioninthe

state space from whichall trajectoriesconverge to x

s

. Moreprecisely,

S(x

s

)=fx: lim

t!1

(t;x

o )=x

s g

A subset S  R n

is said to be open, if for every vector x 2 S, one can

ndan {neighborhoodof x

N(x;)=fz2R n

:kz xk<g

such that N(x;) 2 S. A set S is bounded if there is r > 0 such that

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