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    Warsaw University of Technology

    Faculty of Electrical EngineeringInstitute of Control and Industrial Electronics

    Ph.D. Thesis

    M. Sc. Mariusz Cichowlas

    ! ! ! !

    Thesis supervisor

    Prof. Dr Sc. Marian P. Kamierkowski

    Warsaw, Poland 2004

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    The work presented in this thesis was carried out during my Ph.D. studies at the Institute of

    Control and Industrial Electronics at the Warsaw University of Technology. Some parts of the

    work were realized in cooperation with University of Aalborg, Denmark (International

    Danfoss Professor Programme Prof. Frede Blaabjerg),

    First of all, I would like to thank Prof. Marian P. Kamierkowski for continuous support, help

    and friendly atmosphere. His precious advice and numerous discussions enhanced my

    knowledge and scientific inspiration.

    I am grateful to Prof. Stanisaw Pirg from the AGH University of Science and Technology,

    Cracow and Prof. Wodzimierz Koczara from the Warsaw University of Technology for their

    interest in this work and holding the post of referee.

    Furthermore, I thank my colleagues from the Intelligent Control Group in Power Electronics

    for their support and friendly atmosphere. Specially, to Dr. D.L. Sobczuk and Dr. M.

    Malinowski for his support for my education.

    Finally, I would like to thank my whole family, particularly my wife Kinga and son Kuba for

    theirs love and patience.

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    Table of Contents

    1. Introduction 7

    2. Front-end Rectifiers for Adjustable Speed AC Drives 14

    2.1 Introduction 14

    2.2 Adjustable Speed AC Drives 14

    2.3 Drive System Configurations 15

    2.4 Diode rectifiers 16

    2.5 Harmonic Limitations 24

    2.6 Conclusions 27

    3. Basic Theory of PWM Rectifier 28

    3.1 Operation of the PWM Rectifier 28

    3.2 Mathematical description of PWM Rectifier 33

    3.3 Block diagram of PWM rectifier 35

    3.4 Operating limits 37

    4. Introduction to Active Filtering 39

    4.1 Basic configuration 40

    4.2 Control of Shunt Active Filters 40

    4.3 Types of Harmonic Sources 42

    4.4 Analysis of Shunt Active Filter (SAF) Operation with Different Harmonic

    Sources44

    4.5 Conclusions 47

    5. PWM Rectifier with Active Filtering Function 49

    5.1. Introduction 49

    5.2. Control Methods of PWM Rectifier 50

    6. Dimensioning of Power Converters 646.1 PWM Rectifier rating 65

    6.2. Shunt Active Power Filter (SAF) Rating 68

    6.3. PWM Rectifier with Active Filtering Function Rating 71

    6.4 Design of Passive Components 73

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    6.5 Conclusions 78

    7. Simulation and Experimental Results 79

    7.1 Voltage Oriented Control (VOC) 81

    7.2 Virtual Flux Based Direct Power Control (VF-DPC SVM) 86

    7.3 Summary and Comparison of Compensating Results 90

    7.4 Rectifying and Regenerative Mode of PWM Rectifier Operation 92

    7.5 Typical Grid Voltage Distortion 95

    7.6 Influence of Passive Components, DC-link Voltage and Converter Power

    Variations100

    7.7 Discussion on Digital Signal Processor Implementation 102

    7.8 Conclusions 104

    8. Summary and Closing Remarks 107

    Appendix 109

    A.1 Harmonics 143

    A.2 Basic Harmonic Distortion in Power System 108

    A.3 Instantaneous decomposition of powers 110

    A.4 Simulations and Experimental environments 115

    A.5 Review and design of Current and Power Controllers 120

    References 147

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    List of symbols

    Symbols

    - phase angle of reference vector

    - power factor

    - phase angle of current

    - angular frequency

    - phase angle

    - control phase angle

    cos- fundamental power factor

    f frequency

    i(t), i instantaneous current

    kP, kI proportional control part, integral control part

    t instantaneous time

    v(t), v- instantaneous voltage

    S virtual line flux vector

    S virtual line flux vector components in the stationary , coordinates

    S virtual line flux vector components in the stationary , coordinates

    Sd virtual line flux vector components in the synchronous d, q coordinates

    Sq virtual line flux vector components in the synchronous d, q coordinates

    uS line voltage vector

    uS line voltage vector components in the stationary , coordinates

    uS line voltage vector components in the stationary , coordinates

    uSd line voltage vector components in the synchronous d, q coordinates

    uSq line voltage vector components in the synchronous d, q coordinates

    iS line current vector

    iS line current vector components in the stationary , coordinates

    iS line current vector components in the stationary , coordinates

    iSd line current vector components in the synchronous d, q coordinates

    iSq line current vector components in the synchronous d, q coordinates

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    uC converter voltage vector

    uC converter voltage vector components in the stationary , coordinates

    uC converter voltage vector components in the stationary , coordinates

    uCd converter voltage vector components in the synchronous d, q coordinates

    uCq converter voltage vector components in the synchronous d, q coordinates

    iC converter current vector

    iC converter current vector components in the stationary , coordinates

    iC converter current vector components in the stationary , coordinates

    iCd converter current vector components in the synchronous d, q coordinates

    iCq converter current vector components in the synchronous d, q coordinates

    iL nonlinear load current vector

    iL nonlinear load current vector components in the stationary , coordinates

    iL nonlinear load current vector components in the stationary , coordinates

    iLd nonlinear load current vector components in the synchronous d, q coordinates

    iLq nonlinear load current vector components in the synchronous d, q coordinates

    udc DC link voltage

    idc DC link current

    Ldc- DC link inductor

    Sa, Sb, Sc switching state of the converter

    C capacitance

    I root mean square value of current

    L inductance

    R resistance

    S apparent power

    T time period

    P active power

    Q reactive power

    Z- impedance

    p,q- instantaneous active and reactive power

    pref, qref - reference values of instantaneous active and reactive powers

    pA, qA- nonlinear load instantaneous active and reactive powers

    pA, qA- alternated values of instantaneous active and reactive power

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    Subscripts

    ..a, ..b, ..c- phases of three-phase system

    ..d, ..q - direct and quadrature component

    ..+, -, 0 - positive, negative and zero sequence component

    .., .., ..0 alpha, beta components and zero sequence component

    ..h harmonic order of current and voltage, harmonic component

    ..n harmonic order

    ..max - maximum

    ..min - minimum

    ..LL - line to line

    ..Load - load

    ..ref - reference

    ..m - amplitude

    ..rms - root mean square value

    Abbreviations

    APF Active Power Filter

    AFF Active Filtering Function

    ANN Artificial Neural Network

    ASD Adjustable Speed Drives

    DPC Direct Power Control

    DSP Digital Signal Processor

    HPF High Pass Filter

    LPF Low Pass Filter

    EMI Electro-Magnetic Interference

    IGBT Insulated Gate Bipolar Transistor

    PCC Point Of Common Coupling

    PFC Power Factor Correction

    PI Proportional Integral (Controller)

    PLL Phase Locked Loop

    PWM Pulse-Width Modulation

    REC Rectifier

    SVM Space Vector Modulation

    THD Total Harmonic Distortion

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    UPF Unity Power Factor

    VF Virtual Flux

    VF-DPC Virtual Flux Based Direct Power Control

    VSI Voltage Source Inverter

    Basic Definitions

    Harmonic Distortion

    %100

    1X

    nX

    HD=

    X1 RMS value of first harmonic of voltage or current

    Xn RMS value of n harmonic of voltage or current

    Total Harmonic Distortion

    2

    1100%

    1

    Xn

    nTHD

    X

    >=

    X1 RMS value of first harmonic of voltage or current

    Xn RMS value of n harmonic of voltage or current

    Power Factor

    1 cosI

    PF I =

    Partial Weighted Harmonic Distortion

    2

    14

    1

    100%

    h

    h

    hI

    PWHDI

    ==

    Harmonic Constant

    2 2

    2

    1

    100%

    h

    h

    h I

    HCI

    ==

    Remark: Please note that literature is numbered using [x,y] nomenclature, where x denotes a

    topic and y number of paper

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    1. Introduction

    Modern electric devices are usually fed by diode or thyristors front-ends. Such equipment

    generates higher harmonics into a grid. Nowdays those problems are going more and more

    serious. Grids disturbances may result in malfunction or damage of electrical devices.

    Therefore, currently many methods for elimination of harmonic pollution in the power system

    are developed and investigated.

    Restrictions on current and voltage harmonics maintained in many countries through IEEE

    519-1992 in the USA and IEC 61000-3-2/IEC 61000-3-4 in Europe standards, are associated

    with the popular idea of clean power.

    Harmonic reduction techniques can be divided as shown in Fig. 1.1, where two main groups

    can be seen:

    - devices for cancellation of existing harmonics,

    - grid friendly devices, which do not generate (or generate limited number) harmonics.

    Fig. 1.1 Most popular current harmonic reduction techniques in three-phase networks

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    The classical method of current harmonic reduction uses passive LC filters (Fig.1.2) [7, 10.5,

    10.7]. They are usually constructed as capacitors and inductors series or parallel-connected to

    the grid. Each harmonic (5th

    , 7th

    , 11th

    , 13th

    ) requires its own passive filter (see Fig. 1.2). This

    means that filters can not be designed in a general way but must be designed according to

    each application. Such a solution has advantages of simplicity and low cost. However, among

    disadvantages are:

    A passive filters are designed for a particular application (size and placement of the

    filters elements, risk of resonance problems),

    high power losses as a result of high fundamental current,

    passive filters are heavy and bulky.

    5th 7th 11th 13th

    Fig. 1.2. LC passive filters

    The simpler way to harmonic reduction of diode rectifier currents are additional series

    inductors used in the input or output of rectifier (typical per unit value is 1-5%) (see Chapter

    2).

    Other technique, based on mixing single and three-phase (Fig. 1.3a) non-linear loads [7.7,

    10.2], gives a reduced THD because the 5th

    and 7th

    harmonic current of a single-phase diode

    rectifier often are in counter-phase with the 5th

    and 7th

    harmonic current of a three-phase diode

    rectifier. Simulated input current waveform is presented in Fig. 1.3 b.

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    Fig. 1.3. Mixed single and three-phase nonlinear loads and typical line current waveforms

    The multipulse rectifier [3] gives another possibility to decrease current harmonics content.

    Although it is easy to implement, it possess several disadvantages such as: bulky and heavy

    transformer, higher voltage drop, and higher harmonic currents at non-symmetrical load or

    line voltage conditions.

    Y Y

    12-pulse rectifier6-pulse rectifier

    YY

    YY

    24-pulse rectifier

    Y Y

    Fig. 1.4. Basic schemes and typical line current waveforms of multipulse rectifiers

    A modern alternative to the passive filter is application of the Shunt Active Filters (SAF) [5,

    7, 8], which, thanks to used closed feedback loops, gives better dynamics and control of

    harmonic as well as fundamental currents. Active filters are generally divided into two

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    groups: the active shunt filter (current filtering) (Fig. 1.5) and the active series filter (voltage

    filtering).

    Non-linear

    load

    iC

    iL

    iS

    L

    APF

    uS

    Fig. 1.5. Three-phase shunt active filter together with non-linear load

    The three-phase (two-level) shunt SAF consists of voltage source bridge converter. This

    topology is identical to the PWM inverter. SAF represents a controlled current source iC

    which added to the load current iLyields sinusoidal line current iSand provide:

    harmonic compensation (much effectives than passive filters).

    compensation of fundamental reactive components of load current,

    load symetrization (from grid point of view),

    Parallely to excellent performance, SAF possess few disadvantages as: complex control

    strategy, switching losses and EMC problems. Therefore, inclusion of a small LC or LCL

    passive filter between the grid and theSAF

    is necessary.

    Load

    uS

    Fig.1.6 PWM Rectifier

    The other possible reduction technique of current harmonic is application of PWMRectifier

    (Fig. 1.6). Two types of PWMconverters, with a voltage source output [4] (Fig. 1.7a) and a

    current source output (Fig. 1.7b) can be used. First of them called a boostrectifier (increases

    the voltage) operates at fixed DC voltage polarity, and the second, called a buck rectifier

    (reduces the voltage) operates with fixed DC current flow.

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    a) b)

    C

    Udc

    iload

    ia

    ib

    ic

    3xL

    uLa

    uLb

    uLc

    Ui

    3xL

    uLa

    uLb

    uLc

    ia

    ib

    ic

    iload

    Ldc

    Udc

    3xC

    Fig. 1.7 Basic topology of PWM rectifier a) boostwith voltage output, b) buck with current output

    Among the main features of PWM rectifiers are:

    bi-directional power flow,

    nearly sinusoidal input current, regulation of input power factor to unity,

    low harmonic distortion of line current (THDbelow 5%),

    adjustment and stabilization of DC-link voltage (or current),

    reduced capacitor (or inductor) size due to the continues current.

    Furthermore, it can be properly operated under line voltage distortion and notching, and line

    voltage frequency variations.

    This thesis is devoted to investigation of two different control strategies for boost type of

    three-phase bridge PWM rectifiers. A well-known method based on current vector orientation

    with respect to the line voltage vector (Voltage Oriented Control - VOC) is compared with

    control strategy based on instantaneous direct active and reactive power control based on

    virtual flux estimation called Virtual Flux based Direct Power Control (VF-DPC).

    Additionally, in both control strategies an Active Filtering Function is applied.

    Therefore, the following thesis can be formulated:

    Application of Active Filtering Function to PWM Rectifier control strategy provides

    more efficient utilization of power electronics equipment and leads to neutralization of

    harmonics generated by other nonlinear loads. Thus, it improves the line current and

    voltage at the point of common coupling (PCC).

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    In order to prove the above thesis, the author used an analytical and simulation based

    approach, as well as experimental verification on the laboratory setup with a 5kVA IGBT

    converter. In the analytical approach mathematical description based on space vector are

    applied. The following simplifications were assumed when formulated simulation models:

    power transistors were considered as ideal switches, however, the voltage drop has

    been taken into account,

    power diodes were idealized,

    models of passive components included inductance with resistance and capacitance

    with resistance.

    The thesis deals with analysis and comparative study of different control strategies for PWM

    Rectifiers having Active Filtering Function (AFF). At legating a general information

    regarding diode rectifiers, to well understand and recognition of harmonics problems

    generated by them are presented and discussed. Two different control schemes for PWM

    Rectifiers and three different methods for elimination of current harmonics are presented.

    Additionally, information concerning design of current and power controllers, selection of

    passive components and power converter rating calculation are considered. The PhD thesis

    consists of 8 chapters

    The first Chapter Introduction gives short overview of harmonic reduction techniques and

    formulates main goals of the thesis. The second one Front-end Rectifiers for Adjustable

    Speed Drivesdeals with requirements for diode rectifier, which are most common used in

    inverter fed adjustable speed drives. Several models of diode rectifiers with different AC and

    DC side filters are presented, as well as information about current harmonics generated by

    such a rectifiers. Additionally, requirements for passive elements of diode rectifiers are

    presented. Finally, international norms devoted to harmonics pollution in the grid are

    included. The third chapter titled Basic Theory of PWM Rectifier consists of theoretical

    information, mathematical models, basic requirements and limitations for PWM rectifiers.

    The fourth chapter Introduction to Active Filtering describes basic principles of parallel

    active power filters, principles of shunt active filters for current and voltage harmonics

    sources. The fifth chapter PWM Rectifier with Active Filtering Function presents and

    investigates, an interesting opportunity for PWM rectifier filtering function. It is a result of

    conjunction a PWM rectifier and Active Power Filter. Both of them has the same power

    circuit, as well as a control strategies are very similar, therefore such equipment can be

    interesting alternative for expensive active filtering units. Two different control strategies are

    described: VOC (Voltage Oriented Control) with two different methods of compensation

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    higher current harmonics and VF-DPC (Virtual Flux based Direct Power Control). Very

    important chapter sixth Dimensioning of Power Converters deals with dimensioning of

    power converter, taking into account a parameters like: demanded active power of DC load,

    input filter inductance, reactive and harmonics power intended to compensation. Additionally,

    requirements for passive elements of power converters are presented. The chapter sevenths

    entitled Simulation and Experimental Results presents simulation models developed in

    thesis and selected waveforms which show operation of investigated control algorithms. Also,

    comparative study of Voltage Oriented Control (VOC) versus Direct Power Control (DPC) is

    presented. The last chapter eight Summary and Closing Conclusions gives general

    overview and final conclusions on discussed topic. Several information, devoted to harmonic

    distortion in power system, instantaneous decomposition of powers according to different

    authors like: Peng, Akagi, etc. are presented in Appendix A.2. Additionally, general

    information concerning simulation models, used simulation packages (SABER,

    MATLAB/SIMULINK, PLECS) and laboratory setup are given in Appendix A.4. Also,

    Appendix A.5 presents design algorithms for current (for VOC) and power (for VF-DPC), PI

    type regulators. An Artificial Neural Network based, resonant current controllers as well as

    delta modulation and hysteresies controllers are presented.

    In the authors opinion the following parts of the thesis represent his original

    contributions:

    elaboration of Virtual Flux based Direct Power Control for PWM rectifiers with Active

    Filtering Function control strategy (Chapter 5),

    elaboration of methodology for converter power ratio calculations depending on

    application PWM Rectifier, Active Power Filter, PWM Rectifier with Active Filtering

    Function (Chapter 6),

    development of two simulation algorithms in Matlab/Simulink and SABER with control

    algorithm in C language for investigation of proposed solutions (Appendix A.4),

    implementation and investigation of various closed-loop control strategies for PWM

    rectifiers: Virtual Flux Based Direct Power Control (VF -DPC), Voltage Oriented

    Control (VOC), as well as open loop and closed loop control strategies for PWM Rectifier

    with Active Filtering Function ,

    practical verification on the experimental setup based on a mixed RISC/DSP (PowerPC

    604/TMS320F240) digital controller.

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    2. Front-end Rectifiers for Adjustable Speed AC Drives

    2.1 Introduction

    Voltage source inverters (VSI) fed adjustable speed drives (ASD) are frequently used in

    industry, especially in energy saving applications. In the conventional solution the inverter is

    fed by a diode or thyristor rectifier [7.8] with a large DC link capacitor. Such a rectifier takes

    a high distorted AC-grid current. Frequent use of such rectifiers as ASD front-ends has

    resulted in serious utility problems like current and voltage harmonics, reactive power,

    voltage notches, etc. Voltage harmonics due to current harmonics becomes the main problem

    for utility.

    A usual way to reduce high current harmonics is application of a DC or AC-side inductors.

    Compared to DC-sided smoothing inductor, an AC-side inductor creates an electrical distance

    between grid and a drive. However, the AC-inductor is a source of additional losses, has a

    meaningful dimension and determines an additional cost. Fig. 2.1 shows scheme of utility

    interface for converter-fed drives [7.1]. These solutions do not provide recommended IEEE

    519 harmonic standards, which require voltage distortion limitation at utility-customer point

    of common coupling (PCC). IEEE 519 is a justification for using of power quality

    compensators.

    VS

    Motor

    AC side filter DC side filterDiode rectifier InverterPCC

    Fig. 2. 1 Converter-Fed adjustable drives utility interface typical scheme

    2.2 Adjustable Speed AC Drives

    The ASDs input current characteristics depend on: drive type, its load, and the characteristics

    of the supplying system [7.4, 7.5]. The input currents harmonic distortion can vary over a

    wide range. However, for purposes of analysis it is possible to identify two basic waveform

    types as bellow [11].

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    TYPE 1: Discontinuous mode - High Distortion Current Waveform.

    This is a representation of all ASDs that have voltage source inverters without an additional

    inductor for current smoothing (Fig. 2.3a). The total harmonic current distortion can be over

    80%. Actually, it can be higher for small drives but waveform of Fig. 2.3b is a good

    representation for larger drives or groups of smaller drives.

    TYPE 2: Continuous mode - Low Distortion Current Waveform.

    This mode represents behavior of DC drives, large AC drives with current source inverters,

    and smaller AC drives with voltage source inverters and added inductor for current smoothing

    (Fig. 2.4a). The typical waveform of Fig. 2.4b has a THD level of 30%, which is obtained for

    an AC drive with a 5% inductor.

    The significant harmonic reduction is obtained for ASDs just by adding an inductor at the

    rectifier input. Fig. 2.5 illustrates the effect of AC-side inductance size on input currentdistortion. It is possible to include this inductance in the DC link of the drive, providing the

    same harmonic current reduction benefit.

    2.3 Drive system configurations

    "#$#% &'"#$#% &'"#$#% &'"#$#% &'((((

    A DC-side inductor can be added to a three-phase rectifier (Fig. 2.2) for harmonic reduction.

    With the dc inductor of a sufficient amount, the input current becomes a square waveform. By

    adding an infinite dc inductor, a perfect square waveform can be obtained. However, a perfect

    square waveform will have difficulties to meet the individual limits for higher order

    harmonics.

    Motor

    VS

    Fig. 2.2. Diode rectifier with DC side capacitor and inductor.

    Input current THD=60%-130%

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    "#$#" &' '"#$#" &' '"#$#" &' '"#$#" &' '((((

    Another solution is to add a series AC-side inductor or passive filter to remove individual

    harmonics. Fig. 2.3 shows the circuit arrangement with a LC filter in front of the rectifier

    together with a DC-side inductor.Generally, such a LC filter can be tuned to the 5th

    or 7th

    harmonic because they are most important. Once the 5

    th harmonic is cancelled, rest of

    harmonics can also be reduced significantly in the same way.

    Motor

    VS

    Fig. 2.3. Diode rectifier with DC side capacitor and inductor filter and AC side inductor. Input currentTHD=30%-40%

    Fig. 2.4 compares harmonic contents for different DC-side inductors.The three-phase diode

    rectifier generates about 70-percent 5th harmonic. After adding 1% and 5% DC-side inductor,

    the 5th harmonic content is reduced to 35% and 25%, respectively.Therefore, an individual

    harmonic filter in addition to the DC-side inductor is necessary to meet IEC 1000-3-4

    standards.

    5 7 9 1 1 1 3 1 5 1 7 1 9

    0

    2 0

    4 0

    6 0

    8 0

    HD[%]

    H a r m o n i c n u m b e r

    T h r e e p h a s e r e c t if ie r

    1 % D C i n d u c to r

    5 % D C i n d u c to r

    I E C 1 0 0 0 - 3 - 4 S t a n d a r d

    Fig. 2.4. Comparison between different three-phase built-in passive compensation results and IEEE

    standard

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    2.4 Diode rectifiers

    "#)#%# * &'"#)#%# * &'"#)#%# * &'"#)#%# * &'((((

    The idealized model of three-phase diode rectifier with infinite DC-side inductor is presented

    in Fig. 2.5a.a) b)

    L

    o

    a

    d

    LDC

    uA

    uB

    uC

    iA

    1/6 5/6 2

    Fig. 2.5 Ideal three phase rectifier with infinite DC-side inductor Ldcand no grid impedance (a),

    Voltages and currents of idealized three phase rectifier (b).

    The idealized rectifiers current assumed to be smooth on the DC-side (infinite LDC) and, for

    neglected commutation effects (LS=0), occurs an ideal square. As shown o Fig. 2.5b the

    current changes instantaneously from zero to a finite value. Every phase is conducting only

    during 2/3 of the period. The input diode rectifier current can be described in following form:

    0

    0

    50 6

    5 1

    6 6

    1 1( ) 0

    6 6

    1 5

    6 6

    50

    6

    sa

    t

    I t

    i t t

    I t

    t

    < <

    < <

    = <

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    can be used to determine the order and magnitude of the harmonic currents drawn by a six-

    pulse diode rectifier:

    16 = kh k = 1, 2, 3. (2.3a)

    h

    I

    Ih /1

    1

    = (2.3b)

    Thus, the higher harmonic orders are: 5th

    , 7th

    , 11th

    , 13th

    etc., with a 50 Hz fundamental

    frequency, that corresponds to 250, 350, 550 and 650 Hz, respectively. The per unit

    magnitude of the harmonics of the fundamental is the reciprocal of the harmonic order: 20%

    for the 5th

    , 14,3% for the 7th

    , etc. Eqs. (2.1)-(2.2) are calculated from the Fourier series for

    ideal square wave current (critical assumption for infinite inductance on the input of the

    converter). Equation (2.1) is fairly good description of the harmonic orders generally

    encountered. The magnitude of actual harmonic currents often differs from the relationship

    described in (2.2). The shape of theACcurrent depends on the input inductance of converter.

    The ripple current is proportional to 1/L times the integral of the DC ripple voltage and

    inverse proportional to LDCinductance.

    1ripple DC

    i U dt L

    = (2.4)

    "#)#" * &'"#)#" * &'"#)#" * &'"#)#" * &'((((

    A diode rectifier with DC-side smoothing capacitor is common used front-end rectifier in

    industry. Its construction is very cheap and compact, however from the grid point of view it

    has the worst behavior.

    L

    o

    a

    d

    Fig. 2. 6. Three-phase rectifier with smoothing DC side capacitor a) circuit, b) typical waveforms

    b)a)

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    The idealized model of three-phase diode rectifier with DC-side capacitor is presented in Fig.

    2.6a. Typical input current waveform presents Fig. 2.6b, and as shown it contains high

    number of higher harmonics and the THD is over 80%.

    "#)#$ * '"#)#$ * '"#)#$ * '"#)#$ * '(((( &' &' &' &'((((

    The idealized model of three-phase diode rectifier with AC-side inductor and DC-side

    capacitor is presented in Fig. 2.7a [10.5, 10.6, 10.8]. Typical input current waveforms are

    presented in Fig. 2.7b and 2.7c with 1% and 5% AC-side inductor, respectively. It can be seen

    that, an input current of Fig. 2.7c consists less higher harmonics and has lower THD

    compared with current of Fig. 2.7b.

    Fig. 2.7. Diode rectifier with AC-side inductors (a) and typical for 1% and 5% inductor (b).

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    0 1 2 3 4 5

    30

    40

    50

    60

    70

    80

    Input

    currentTHD[%]

    Choke inductance [%]

    Fig. 2.8. Effect of input inductance on ASDs input current distortion

    Fig. 2.8 presents effect of input inductor on input current THD. The input current THD

    decrease with increasing value of input inductance. Therefore, such a solution partially solves

    a harmonic problem. However, application of input inductance generates some additional

    problems. One of them is the phase shift between fundamental harmonics of gridvoltage and

    input current, which is very important parameter determining the reactive power level. Fig.

    2.9 shows that it strongly depends and increases in case of increasing input inductance or load

    power.

    0 4 8 12 16 20

    -25

    -20

    -15

    -10

    input inductance [mH ]

    iDC

    [A]Phaseshiftbetwee

    nfirstharmonics

    oflinevoltageandinputcurrent[deg]

    Fig. 2.9. Phase shift between first harmonics of grid voltage and input current versus AC-side

    inductance or load power.

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    Fig. 2.10 presents simulated waveforms for diode rectifier with AC-side inductance and DC-

    side capacitance for two different load conditions. The decreasing amplitude and phase shift is

    present in case of increasing load conditions. That gives an additional reactive power taken by

    the converter.

    Fig. 2.10. Typical input current waveforms for two different DC-side currents: Idc=3A (blue),

    Idc=15A (green)

    Applied input inductance value has an additional effect on a diode rectifier operation [9].

    Adoption of it, besides of decreasing of harmonic distortion and increasing of reactive power

    determine of decreasing ofi

    t

    parameter.

    Fig. 2.11.i

    t

    parameter of diode rectifier input current versus input inductance value

    a) LL=10mH, b) LL=1mH

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    As shown in Fig. 2.11 an input inductance value has a great influence oni

    t

    parameter of

    diode rectifier grid current. A large value of input inductance decrease significantly ofi

    t

    parameter.

    Additional input inductance is the simplest method to reduce grid current harmonics

    generated by diode rectifiers feded adjustable speed drives (ASD) converters.

    Summarizing, the input inductor has following impact on diode rectifier operation:

    Significantly reduce a grid current THD,

    Decrease ai

    t

    parameter,

    Increase reactive power value taken by the converter,

    A source of additional voltage drop.

    "#)#) "#)#) "#)#) "#)#)

    Diode rectifier with DC-side capacitance

    0 200 400 600 800 1000

    80

    100

    120

    140

    160

    180

    GridcurrentTHD[%]

    DC-link capacitance [uF]

    Fig. 2.12. Grid current THD versus DC-link capacitance

    Fig. 2.12 shows the grid current THD versus DC-link capacitance. A large value of

    capacitance provide more smooth shape of DC-link voltage, however a grid current will have

    higher amplitude. That significantly increase a grid current THD.

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    Diode rectifier with DC-side capacitance and inductance

    0 200 400 600 800 1000

    37

    38

    39

    40

    41

    42

    43

    LinecurrentT

    HD[%]

    DC-link capacitance [uF]

    10 20 30 40 50

    30

    32

    34

    36

    38

    GridcurrentT

    HD[%]

    DC-link inductance [mH]

    Fig. 2.13. a) Grid current THD versus DC-link capacitance, b) Grid current THD versus DC-link

    inductance

    In this situation a DC-link inductance provide a continuous mode of diode rectifier operation.

    Therefore, both a large value of a DC-link capacitance and inductance provide decreasing of

    input current THD. However, there are the maximal values for capacitance and inductance

    (500uF and 30mH, respectively), above which increasing of those parameters is not

    profitable, because the grid current THD do not decrease enough.

    Diode rectifier with AC-side inductance and DC-side capacitance

    0 200 400 600 800 1000

    31,5

    32,0

    32,5

    33,0

    33,5

    34,0

    GridcurrentTHD[%]

    DC-link capacitance [uF]

    0 5 10 15 20 25

    20

    40

    60

    80

    100

    GridcurrentTHD[%]

    AC-side inductance [mH]

    Fig. 2.14. a) Grid current THD versus DC-link capacitance, b) Grid current THD versus AC-side

    inductance

    Here, for a grid current smoothing the AC-side inductor is applied. Similar, like in previous

    situation both a large value of a AC-side inductance and DC-link capacitance provide

    decreasing of input current THD. Moreover, there are also the maximal values for capacitance

    a) b)

    a) b)

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    2.5 Harmonic Limitations

    Severe current or voltage harmonics may damage or malfunction various electronic

    equipment supplied from the grid. However, a level of grid distortion where those problems

    can occur is not precisely defined. The main reason of harmonics in power system is

    electronic equipment mainly a diode rectifiers, mostly spread power electronic AC/DC

    converters. The reason of diode rectifier popularity is very simple, it is cheap, robust,

    efficient, reliable and has a small size. However, a diode rectifier has one big disadvantage

    significantly distorted input current. Therefore, problems related to harmonics produced in the

    grid by diode rectifiers, caused necessity of define and arrange requirements for nonlinear

    electronic equipment. International norm precisely define maximal harmonic content in a grid

    voltage as well as in the current taken by electronic equipment. Norms divide electronic

    devices depending on maximum permissible current and force an application of equipment

    like passive and active filters or PWM Rectifiers.

    "#+#% *,,, +%-"#+#% *,,, +%-"#+#% *,,, +%-"#+#% *,,, +%-((((%--"%--"%--"%--"

    This standard sets limits for harmonic voltage and currents at the Point of Common Coupling

    (PCC), therefore the focus is only on the power system. It places responsibility on large

    commercial and industrial consumers.

    Voltage Distortion Limits

    Bus Voltage at PCC Individual voltage distortion [%]* Total voltage distortion [%]

    below 69kV 3.0 5.0

    69kV to 138kV 1.5 2.5

    Above 138kV 1.0 1.5

    * maximum for individual harmonic

    Current Distortion Limits

    Maximum odd harmonic current distortion in percent of ILfor general distribution systems (1.120V 69kV)

    ISC/IL

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    IL- fundamental of the average (over 12 months) maximum monthly demand load current at

    PCC

    TDD total demand distortion, harmonic current distortion in % of maximum demand load

    current (15 or 30 minute demand)

    "#+#" *,' .%///"#+#" *,' .%///"#+#" *,' .%///"#+#" *,' .%///(((($$$$((((" 0*,' %///" 0*,' %///" 0*,' %///" 0*,' %///(((($$$$(((("1"1"1"1

    The European standard IEC 61000 defines the current distortion limits for equipment

    connected to the public supply system. The objective is to limit the voltage distortion and is

    addressed to small customer equipment. Emphasis onpublic, low-voltage and household.

    IEC 1000-3-2 Limits for Class D Equipment

    Harmonic order Maximum permissible

    harmonic current per watt

    Maximum permissible

    harmonic current

    N mA/W A

    3 3.4 2.3

    5 1.9 1.14

    7 1.0 0.77

    9 0.5 0.40

    11 0.35 0.33

    13

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    2.6 Conclusions

    International standards impose voltage and current harmonic limits.Many solutions has been

    designed to deal with these standards.

    The simplest compensation method is to use an AC-side inductor or an AC-side LC filters.

    However, when using these passive compensation methods some problems can occur:

    - Rectifier input voltage distortion and output DC link voltage reduction by AC-side

    induction.

    - Rectifier input current augmentation by parallel connected filters.

    The active compensation is therefore preferred in case of performance basis, but its cost and

    complexity is a main problem.

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    3. Basic Theory of PWM Rectifier

    As shown in Chapter 2, diode rectifiers are most frequently applied converters in

    AC/DC power conversion. However, because of significantly distorted input current, which is

    not acceptable in respect to international standards, diode rectifiers should be replaced be

    other, not polluting and line power friendly equipment. Therefore, converters which present a

    low interaction on the grid are going more interested. The three phase VSC (Voltage Source

    Converter) applied as a grid interface stage called Boost active rectifier, can take near

    sinusoidal input current with a near unity power factor but also it can work in both rectifying

    and regenerative modes. From the reliability and efficiency point of view a PWM Rectifiers

    are very promise solutions [1, 4, 6.2, and 6.4].

    The PWM Rectifier, by many is considered as most obvious alternative to conventional diode

    rectifier. This chapter introduces and presents basics of operation of PWM Rectifier and

    operation limitations. Also, mathematical models in different reference frames are presented.

    The basic requirements of a PWM Rectifier can be defined as follows:

    bi-directional power flow,

    low harmonic distortion of line current,

    regulation of input power factor to unity,

    adjustment and stabilization of DC-link voltage, reduced DC filter capacitor size.

    3.1 Operation of the PWM Rectifier

    Fig. 3.1b shows a single-phase representation of the PWM boost Rectifier circuit presented in

    Fig. 3.1a. The L and R represent the line inductor. uSis the line voltage and uC is the bridge

    converter voltage controllable from the DC-side. Magnitude of uCdepends on the modulation

    index of the VSC and DC voltage level.

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    a)

    b)

    uS

    uc

    iCL R

    RiCjLiC

    Fig. 3.1. Simplified representation of three-phase PWM rectifier for bi-directional power flow

    a) Main circuit b) single-phase representation of the rectifier circuit

    d

    q

    (a) (b)

    Su

    jL Ci

    R Ci

    Cid

    q

    Su

    jL Ci

    R Ci

    Ci

    Cu

    Cu

    Fig. 3.2. Phasor diagram for the PWM rectifier a) rectification at unity power factor b) inversion at

    unity power factor

    Inductors L connected a input of PWM converter with a grid are integral part of the rectifier

    circuit. It brings current source character of input circuit and provide boost feature of

    converter. The line current iC is controlled by the voltage drop across the inductance L

    interconnecting two voltage sources (grid and PWM converter). It means that the inductance

    voltage uI equals the difference between the line voltages uS and the converter voltage uC.

    When a phase angle and amplitude of converter voltage uC is controlled, indirectly phase

    and amplitude of line current is controlled. In this way average value and sign of DC current

    is controlled and is proportional to active power flowing through converter. The reactive

    power can be controlled independently with shift of fundamental harmonic current iC in

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    respect to voltage uS. Fig. 3.2 presents general phasor diagram for both rectification and

    regeneration modes when unity power factor is required. The figure shows that the voltage

    vector uC is higher during regeneration (up to 3%) then rectifier mode [6.6]. Thus, PWM

    Rectifier has two operation modes:

    Rectifying mode, Regenerating mode.

    Naturally, in a real system the power losses are present because of:

    Power transistors switching losses,

    AC-side inductor losses,

    Heating losses and others.

    Load

    VS

    Plosses

    Rectifying mode Pgrid

    = Pload

    + Plosses

    Regenerating mode Pgrid

    = Pload

    - Plosses

    Fig. 3.3. Power flow in active PWM rectifier

    A three-phase symmetric system represented in a natural coordinate system by phase

    quantities like for example voltages (Fig. 3.4), can be replaced by one resultant space vector.

    22( ) ( ) ( )

    3A B Ck k t k t k t = + + 1 a a (3.1)

    Where: ( ), ( ), ( )A B Ck t k t k t - denote arbitrary phase quantities in a system of natural

    coordinates (A, B, C) satisfying the condition ( ) ( ) ( ) 0A B Ck t k t k t + + =

    2, ,1 a a - Complex unit vectors,

    2

    3- Normalization factor

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    Fig. 3.4. Configuration of space vector

    Main circuit of bridge converter (Fig. 3.1a) consists of three legs with IGBT transistor or, in

    case of high power, GTO thyristors. The bridge converter voltage can be represented with

    eight possible switching states (six-active and two-zero) described by equation 3.2.

    Fig. 3.5a presents converter structures for eight different switching states.

    A B C

    +

    -

    UDC

    U1k = 0

    Sa

    =1

    Sb

    =0

    Sc

    =0

    A B C

    +

    -

    UDC

    U2k = 1

    Sa

    =1

    Sb

    =1

    Sc

    =0

    A B C

    +

    -

    UDC

    U3k = 2

    Sa

    =0

    Sb

    =1

    Sc

    =0

    A B C

    +

    -

    UDC

    U4k = 3

    Sa

    =0

    Sb

    =1

    Sc

    =1

    A B C

    +

    -

    UDC

    U5k = 4

    Sa

    =0

    Sb

    =0

    Sc

    =1

    A B C

    +

    -

    UDC

    U6k = 5

    Sa

    =1

    Sb

    =0

    Sc

    =1

    A B C

    +

    -

    UDC

    U7

    Sa

    =1

    Sb

    =1

    Sc

    =1

    A B C

    +

    -

    UDC

    U0

    Sa

    =0

    Sb

    =0

    Sc

    =0

    Fig. 3.5a Possible switching states (Sa, Sb, Sc) of PWM bridge converter

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    ( 1) / 32

    3

    0

    j k

    DCk

    U eu

    =

    1...6

    0,7

    k

    k

    =

    =

    (3.2)

    As mentioned in Fig. 3.5a eight possible states of the converter can be presented in vector

    representation (Fig. 3.5b). Therefore, demanded command vector, will be constructed using

    the nearest accessible vectors [2.1, 2.2].

    Fig. 3.5b Representation of input voltage as a space vector

    Fig. 3.5b presents of input voltage as a space vector as was mentioned in Fig. 3.5a.

    Only one switch in the leg of converter (Fig. 3.1a) can be turn on in one time, if two of them

    will be turn on, the short circuit of DC-link will happen. To protect the converter, a delay time

    (dead time) in transistor switching signals must be applied [2.3]. The dead time effect

    produces a nonlinear distortion of the average voltage trajectory. Therefore, for the proper

    operation a compensation of dead time is required.

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    3.2 Mathematical description of PWM Rectifier

    2

    3 DC

    U

    2

    DCU

    2

    DCU

    2

    DCU

    2

    DCU

    2

    3 DC

    U

    2

    DCU

    2DCU

    2

    DCU

    2

    DCU

    DCU

    DCU

    Fig. 3.6 Representation of converter output voltages: a) equivalent scheme of the converter, b)

    output voltages

    $#$#% 2 $#$#% 2 $#$#% 2 $#$#% 2

    Three phase grid voltage and the fundamental line current are described as:

    sinAN mu E t= (3.3a)

    2sin( )

    3BN m

    u E t

    = + (3.3b)

    2sin( )

    3CN m

    u E t

    = (3.3c)

    sin( )AN mi I t = + (3.4a)

    2sin( )

    3BN mi I t

    = + + (3.4b)

    2sin( )3

    CN mi I t = + (3.4c)

    where Em (Im) and are amplitude of the phase voltage (current) and angular frequency,

    respectively.

    With assumption

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    0AN BN CNi i i+ + (3.5)

    we can transform equations (3.3) to a stationary - system and the input voltage in -

    frame are expressed by:

    3

    sin( )2S mu E t = (3.6)

    3cos( )

    2S m

    u E t = (3.7)

    Similarly, the input voltages in the synchronous d-q coordinates are expressed by:

    2 23

    200

    Sd S Sm

    Sq

    u u uE

    u

    + = =

    (3.8)

    $#$#" * $#$#" * $#$#" * $#$#" *

    Line to line input voltages of PWM rectifier can be described as:

    ( )AB A B DCu S S u= (3.9a)

    ( )BC B C DC

    u S S u= (3.9b)

    ( )CA C A DC

    u S S u= (3.9c)

    and phase voltages are equal:

    AN a DCu f u= (3.10a)

    BN b DCu f u= (3.10b)

    CN c DC u f u= (3.10c)

    where:

    2 ( )

    3

    A B Ca

    S S Sf

    += (3.11a)

    2 ( )

    3

    B A Cb

    S S Sf

    += (3.11b)

    2 ( )

    3

    C A Bc

    S S Sf

    += (3.11c)

    Thefa, fb, fcare assume 0, 1/3 and 2/3.

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    3.3 Block diagram of PWM rectifier

    $#)#% $#)#% $#)#% $#)#% ((((

    The voltage equations for balanced three-phase system without the neutral connection (Fig.

    3.1) can be written as:

    S I Cu u u= + (3.12)

    C

    S C C

    diu Ri L u

    dt= + + (3.13)

    Sa Ca Ca Ca

    Sb Cb Cb Cb

    Sc Cc Cc Cc

    u i i ud

    u R i L i udt

    u i i u

    = + +

    (3.14)

    and additionally for currents

    dca Ca b Cb c Cc dc

    duC S i S i S i idt

    = + + (3.15)

    A block diagram of PWM rectifier corresponding to Eqs(3.13-14) is shown in Fig. 3.7.

    sLR+

    1

    sLR+1

    sLR+

    1

    3

    1

    sC

    1+

    +

    +

    +

    +

    +

    +

    ++

    +

    ++

    +

    -

    -

    -

    -

    -

    -

    - udc

    idc

    uSa

    uSb

    uSc

    Sa

    Sb

    Sc

    iCa

    iCb

    iCc

    fa

    fb

    fc

    uS

    a

    uS

    b

    uSc

    Fig. 3.7. Block diagram of voltage source PWM rectifier in natural three-phase coordinates

    $#)#" 0$#)#" 0$#)#" 0$#)#" 0((((31313131

    Eq.3.13 after coordinate transformation will receive following form:

    CdSd Cd Cq Cd

    diu Ri L Li u

    dt= + + (3.16a)

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    Cq

    Sq Cq Cd Cq

    diu Ri L Li u

    dt= + + + (3.16b)

    ( )dc Cd d Cq q dcdu

    C i S i S idt

    = + (3.17)

    where: tStSSd sincos += ; tStSSq sincos =

    )2(6

    1cba

    SSSS = ; )(2

    1cb

    SSS =

    A block diagram of PWM Rectifier in synchronous rotating d-qmodel [6.5] is presented in

    Fig. 3.8.

    Fig. 3.8. Block diagram of voltage source PWM rectifier in synchronous d-q coordinates

    Rcan be practically neglected because voltage drop on resistance is much lower than voltage

    drop on inductance, what gives simplification of Eq. 3.13.

    C

    S C

    diu L u

    dt= + (3.18)

    Sa Ca Ca

    Sb Cb Cb

    Sc Cc Cc

    u i ud

    u L i udt

    u i u

    = +

    (3.19)

    CS C

    S C C

    uu idL

    u i udt

    = +

    (3.20)

    Therefore, Eq. 3.16a and b receive following shape:

    CdSd Cq Cd

    diu L Li u

    dt= + (3.21a)

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    Cq

    Sq Cd Cq

    diu L Li u

    dt= + + (3.21b)

    The active and reactive power supplied from the grid is given by

    { }*Re S C S C S C Sa C a Sb Cb Sc Ccp u i u i u i u i u i u i = = + = + + (3.22)

    { } ( )*1

    Im3

    S S C S C Sc Ca Sa Cb Sb Ccq u i u i u i u i u i u i = = = + + (3.23)

    It gives in the synchronous d-qcoordinates:

    3( )

    2Sq Cq Sd Cd m m

    p u i u i E I= + = (3.24)

    ( )Sq Cd Sd Cqq u i u i= (3.25)

    For a unity power factor operation, following conditions can be obtained:

    iCq = 0, uSq = 0, 32

    Sd mu E= , 32

    Cd mi I= , q = 0 (3.26)

    3.4 Operating limits

    For proper operation of PWM rectifier a minimum DC-link voltage is required [4, 6, 6.3].

    Generally it can be determined by the peak value of line-to-line grid voltage. Defining the

    natural DC-link voltage value, as possible to obtain in case of not operating transistors, their

    freewheeling diodes becomes a standard three-phase diode bridge. Therefore, the boost nature

    of the active rectifier leads to:

    min ( ) ( )3 2 2,45DC S rms S rmsU u u = (3.27)

    If this condition is not fulfilled, the full control of the input current is not possible. Moreover,

    to keep the switching losses down, a DC-link voltage should be as low as possible. Typically,

    the reference value for the controlled DC-link voltage should be chosen about 10% above the

    natural DC-link voltage. If unity power factor is s required for PWM Rectifier operation, it

    can be obtained in case of:

    2 2 2C S Iu u u= +

    (3.28)

    The voltage drop across the inductor (uI) depends on reactance of the inductor at the input

    frequency and on the input current. The magnitude of the switching voltage vectors depends

    on the DC-link voltage level. This means that the maximum AC voltage (uS) a PWM Rectifier

    can generate in the linear PWM region.

    Assuming the grid side resistance equal to zero and neglecting the converter losses the active

    power can be calculated as follows:

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    3 3 DCC S C S U

    P u i uL

    = = (3.29)

    This means that high value of a DC-link voltage and small value of the input inductor,

    determine a high power rating of the rectifier. The active power can be also defined using DC-

    link voltage and load current as follows:2

    3( )C S C C DC DC P u i Ri U I = = (3.30)

    Therefore, the input current becomes:

    241

    2 3

    S S CC

    u u Pi

    R R R

    =

    (3.31)

    if the following relation is satisfied:

    23

    4

    S

    C

    u

    P R (3.32)

    At steady state operating conditions the capacitor current is zero. Thus the converter output

    power is:

    C DC C P U i= (3.33)

    and the maximum load current that can be delivered is obtained:

    2

    ,max

    3

    4

    SC

    DC

    ui

    RU= (3.34)

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    4. Introduction to Active Filtering

    4.1 Basic Configuration

    The Shunt Active Filters (SAF) can be divided into two groups [5.2, 5.3, 5.4]: a shuntand

    series type of APF. The first one group serve for current and the second one for voltage

    compensation. Shunt Active Filters(SAF) [5.2] are most often used for compensating current

    distortion produced by nonlinear loads, like diode or thyristors rectifiers fed adjustable speed

    drives. General scheme and typical waveforms are shown in Fig. 4.1a and b respectively.

    a)

    b)

    0,280 0,285 0,290 0,295 0,300

    -1 5

    -1 0

    -5

    0

    5

    10

    15

    active filter current

    diode rectifier current

    Line current

    curr

    ent

    time

    Fig. 4.1. a) Basic configuration of Shunt Active Filter (SAF) b)Typical waveforms for input current of

    a diode rectifier compensation

    The SAF current injection has a large influence on the grid current and only a small on the

    nonlinear load (diode rectifier) current [5.9]. The grid voltage can be modified by SAF,

    particularly when it is much distorted and as a result, it modifies the load current. The SAF

    effect on the load current is small but may lead to unstable operation in some cases if the

    designer has not taken its dynamics into account. If this small influence is neglected and the

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    load is considered as a current source, there is no interaction between the AF and the load

    currents.

    4.2 Control of SAF

    Two main ways to cancel the grid current harmonics depending on which current is measured

    can be maintained. These two ways have a different control structure and lead to different

    properties.

    )#"#% 4 2 )#"#% 4 2 )#"#% 4 2 )#"#% 4 2

    This method is based on load current measurement and then the harmonic content is extracted

    from the load current (Fig. 4.2). In this way, the SAF injects the compensating current into the

    grid, without information about the grid current [5.7]. All errors in the system, like parameter

    uncertainties, measurement errors or control errors, will appear in the grid current as

    unfiltered harmonics. The most important advantage of open loop method is system stability,

    but it is connected with extended control algorithm and enlarged number of current sensors.

    a)

    Motor

    u SLS

    LC

    LLiS

    iC

    iL

    DS P

    U DC

    b)

    GuS

    zS

    iL

    iS

    iC

    uC

    Fig. 4.2. a) Open loop Shunt Active Filter (SAF), b) Equivalent circuit for open loop control of SAF

    C Li G i= (4.1)

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    1

    SC

    G ii

    G

    =

    (4.2)

    (1 )S Li i G= (4.3)

    Full compensation can be achieved if: 1G

    G is the equivalent transfer function of the SAF, including detection circuit and delay of the

    control. In general, G has a function of notching for the fundamental component 0f

    G = and

    1h

    G = for harmonics.

    )#"#" ' 2 )#"#" ' 2 )#"#" ' 2 )#"#" ' 2

    Another way to generate the reference current is to measure the grid current. In this way, in

    addition to the inner load current control loop, there is an outer grid current loop in the

    control. This method does not allow harmonic correction without phase balancing and

    reactive power compensation. The control algorithm is less complicated then in open loop

    method and requires minimal number of current sensors.

    a)

    Motor

    uSLS

    LC

    LLiS

    iC

    iL

    DSP

    b)

    GuS

    zS

    iL

    iS

    iC

    uC

    Fig. 4.3. a) Closed loop SAF , b) quivalent circuit for closed loop control of SAF

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    C Si G i= (4.4)

    1

    LC

    G ii

    G

    =

    (4.5)

    1

    LS

    ii

    G=

    (4.6)

    Full compensation can be achieved for G

    4.3 Types of Harmonic Sources

    The harmonic sources are mainly divided into two groups: current and voltage types,

    depending on impedance [5.14].

    )#$#% 5 ')#$#% 5 ')#$#% 5 ')#$#% 5 ' 6 6 6 6

    a)

    ZS

    Harmonic source

    Ld

    AC Source

    b)

    uS

    ZS

    iL

    AC SourceHarmonicCurrentSource

    Fig. 4.4. Typical harmonic current source a) block scheme, b) equivalent circuit

    The common sources of harmonic currents are thyristor converters (Fig. 4.5) where a

    sufficient dc inductance Ldforces a constant DC current. The grid voltage and rectifier current

    are presented in Fig. 4.5. Because of current contents, this behaves like a current harmonic

    source. However, as a current source of harmonics can be also shown a diode rectifier with a

    smoothing capacitor and additional AC or DC inductors, applied for decreasing high order

    harmonics content.

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    Fig. 4.5. Voltage and current of thyristor rectifier (commutation effect is neglected)

    )#$#" 5 7 6)#$#" 5 7 6)#$#" 5 7 6)#$#" 5 7 6

    a)

    AC Source

    ZS

    Harmonic source

    b)

    uS

    ZS

    AC Source

    uL

    iL

    HarmonicVoltageSource

    Fig. 4.6. Typical Harmonic Voltage Source

    A diode rectifier with smoothing capacitor (Fig. 4.6) becomes another common harmonic

    source. Fig. 4.7 present its voltage and current waveforms. The rectifier current is highly

    distorted, its harmonic are affected by the ac side impedance. Therefore this behaves like a

    voltage harmonic source.

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    Fig. 4.7. Voltage and current of diode rectifier

    4.4 Analysis of Shunt Active Filter (SAF) Operation with Different

    Harmonic Sources

    A Shunt Active Filter (SAF) is a PWM inverter placed in parallel with a load (harmonic

    source) to inject a harmonic current with the same amplitude as that of the load, but opposite

    phase into the ac system. A pure current source of harmonic representsL

    z , whereas a

    pure voltage source of harmonic represents 0Lz .

    )#)#% 6 5 ' 6)#)#% 6 5 ' 6)#)#% 6 5 ' 6)#)#% 6 5 ' 6

    GuS

    ZS

    iC

    iS iL

    iLOZL

    Fig. 4.8. Basic principle of shunt active filter with harmonic current source

    Fig. 4.8 presents basic principle of SAF for harmonic current source, where the harmonic

    source is presented as a Nortons equivalent circuit. ZS is source impedance, ILO is the

    equivalent harmonic current source, ZL is the equivalent impedance on the load side which

    may include passive filters and power factor correction capacitors. All equations in the

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    following analysis are in per unit representation. Following equation from Fig.4.8 can be

    obtained:

    C Li Gi= (4.7)

    1 1

    SLS LO

    L LS S

    uZi i

    Z ZZ ZG G

    = +

    + +

    (4.8)

    11

    1

    1 1

    L

    SL LO

    L LS S

    Z

    uGi iZ ZG

    Z ZG G

    = ++ +

    (4.9)

    Focusing on harmonics

    1

    LS h

    h

    ZZ

    G>>

    (4.10)

    which is the required operating condition for the SAF to cancel the load current harmonic.

    When it is satisfied, the Eqs. (4.7)-(4.9) can be written as:

    C Lhi i= (4.11)

    (1 ) (1 ) 0ShSh LOh

    L

    ui G i G

    Z + (4.12)

    ShLh LOh

    L

    ui i

    Z= + (4.13)

    It is seen from the equation (4.12) that source current becomes sinusoidal because of

    1 0h

    G = for harmonics when (4.10) is satisfied. In the Eq. (4.10) only G can be pre-

    designed and determined by the SAF, while ZSand ZLare determined by the system. Because

    of pure current harmonic source, represented by a thyristor rectifier with a large dc

    inductance, we have L SZ Z>> . Equations (4.8) and (4.10) can be reduced respectively:

    (1 )S

    LO

    IG

    I= (4.14)

    1 1h

    G > will not satisfy any more.

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    )#)#" 6 5 7 6)#)#" 6 5 7 6)#)#" 6 5 7 6)#)#" 6 5 7 6

    GuS

    ZS

    iC

    iS iL

    uL

    ZL

    Fig. 4.9. Basic principle of shunt active filter with harmonic voltage source

    Fig. 4.9 shows the basic principle of SAF with harmonic voltage source, where the harmonic

    source is represented by Thevenins equivalent circuit, a voltage source VLand impedance ZL.

    From Fig.9 we can write following equations:

    C Li Gi= (4.16)

    1

    S LS

    LS

    u ui

    ZZ

    G

    =

    +

    (4.17)

    1

    1 (1 )

    1

    S L S LL

    L S LS

    u u u ui

    ZG G Z Z Z

    G

    = =

    ++

    (4.18)

    Therefore, following equation (represents required operating condition for the SAF to cancel

    the load voltage harmonic) is satisfied

    11

    LS

    h

    ZZ pu

    G+ >>

    (4.19)

    the grid current will be sinusoidal. So, with condition (4.19), equations (4.16)-(4.18) are:

    C Lhi i= (4.20)

    0Shi = (4.21)

    Sh LhLh

    L

    u ui

    Z

    = (4.22)

    But it is difficult for SAF to satisfy equation (4.19), because harmonic voltage source

    represents usually very low impedance ZL for a diode rectifier with a large smoothing

    capacitor 0LZ as long no series reactor placed on the ac side of the rectifier.

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    4.5 Conclusions

    A Shunt Active Filters (SAF) have fast dynamic behavior, thanks to large energy storage are

    not sensitive for load transients. However, injection of high order harmonics requires large

    power rating of applied VSI, typically 25%-100% related to load system. From the stability

    point of view, are independent of system parameters and typically not influenced by the loads,

    except for capacitive loads. Generally are applied for variable fundamental reactive power

    compensation, suppression of non-characteristic harmonics and unbalanced systems.

    Reliability of the system is good for low voltage applications, however, over-rating is

    required. SAF are proposed for low to medium power systems with highly dynamics loads.

    General futures of SAF are summarized in Table 4.1.

    Table 4.1 Summary of Shunt Active Filter

    System configuration

    Basic operation principle Operates as a current source

    Adaptive loadsInductive or current-source loads or harmonic current

    source, e.g. phase-controlled thyristor rectifiers of ac drives

    Required operation

    conditions ZL should be high and the SAF should meet 1 1hG

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    5. PWM Rectifier with Active Filtering Function

    5.1 Introduction

    Shunt Active Power Filters (SAF) [5.18 5.20] and PWM rectifiers [4] are two typical

    examples from several solutions, which are used for harmonics elimination. Both of them

    have basically the same power circuit configuration and can operate based on the same

    control principle. SAF are able to compensate not only current harmonics, but also a reactive

    power and load unbalance. Design and control have been investigated in many papers [5.11,

    5.12, and 5.13] where use ness of SAF was proved. PWM Rectifiers [4] as non-polluting

    equipment with sinusoidal input currents are going to be more popular because of several

    advantages like:

    -Bi-directional power flow,

    -Closed loop based stabilization of output DC voltage,-Low harmonic distortion of line currents,

    -Regulation of input power factor to unity.

    This chapter explores another task of PWM rectifier - active filtering function, which adds

    Motor

    VS

    Motor

    LS

    LC

    LL

    iS

    iC

    iL

    DSP

    UDC

    Motor

    VS

    Motor

    LS

    LC

    LL

    iS

    iC

    iL

    DSP

    a)

    b)

    Fig. 5.1. Control strategy a) open loop with 4 current sensors and b) closed loop with 2 current sensors

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    advantages of SAF and PWM Rectifiers. So, the PWM rectifier supplies its load and at the

    same time compensates AC grid current. This concept was at first introduced in works [4.1 -

    4.4 and 14].

    The open loop control strategy illustrated in Fig. 5.1a requires additional control functions

    and measurement of nonlinear load current (iL). In contrast the closed loop control strategy

    presented in Fig. 5.1b is based on PWM Rectifier operation and do not require additional

    current sensors or any modifications in control algorithm. The difference results from location

    of line current sensors. Compared to open loop control strategy, where current harmonic

    content and power factor improvement can be controlled independently, such a system

    performs both of these functions simultaneously.

    5.2 Control Methods of PWM Rectifier

    The dynamic and static performance of PWM Rectifier depends strongly on adopted control

    methods. Therefore, in the next section some basic control strategies used for PWM Rectifiers

    will be presented.

    +#"#%# 7 4 ' 074'1+#"#%# 7 4 ' 074'1+#"#%# 7 4 ' 074'1+#"#%# 7 4 ' 074'1

    Voltage Oriented Control (VOC) is based on coordinate transformations between stationary

    and synchronous rotating dq reference system. It guarantees fast transient response and

    high performance in steady state. Because of VOC uses an internal current control loops final

    performance of the system strongly depends on applied current control techniques [1.2]

    mentioned in Appendix.The conventional VOC system (Fig. 5.3) uses synchronous current control in rotating

    reference coordinates, as shown in Fig. 5.2. A meaningful feature for this type of current

    controller is signal processing in two coordinate systems. The first is stationary -and the

    second is synchronously rotating d-q coordinate system. Three phase measured values are

    converted to equivalent two-phase system -and then are transformed to rotating coordinate

    system in a block -/d-q:

    cos sin

    sin cos

    d US US

    q US US

    k k

    k k

    =

    (5.1a)

    Thanks to the above transformation the control values are DC signals. An inverse

    transformation d-q/-is used on the output of control system and it gives a result on rectifier

    reference signals in stationary coordinate:

    cos sin

    sin cos

    dUS US

    qUS US

    k k

    k k

    =

    (5.1b)

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    The angle of the voltage vector USis defined as:

    ( ) ( )22

    sin / US S S S u u u = + (5.2a)

    ( ) ( )22

    cos / US S S S u u u = + (5.2b)

    In voltage oriented d-qcoordinates, the AC line current vector iCis split into two rectangular

    components iC=

    [iCd, iCq](Fig. 5.2).The component iCddeterminates active power, where iCq

    decides about reactive power flow. Thus the active and the reactive power can be controlled

    independently via active and reactive components of line current vector iC. The UPF

    condition is met when the line current vector, iC,is aligned with the line voltage vector, uS. By

    placing the d-axis of the rotating coordinates on the line voltage vector uS a simplified

    dynamic model can be obtained.

    axis(fixed)

    axis

    d-axis

    (rotating)

    q-axisiS

    iCd

    iCq

    uS= u

    Sd

    US

    =t

    iC

    iC

    uS

    uS

    Fig. 5.2. Vector diagram of VOC. Coordinate transformation of line current, line voltage and rectifier

    input voltage from stationary coordinates to rotating d-qcoordinates

    The grid voltage equations in the d-qsynchronous reference frame are as follows:

    CdSd Cd Cd Cq

    diu R i L u L i

    dt= + + (5.3)

    Cq

    Sq Cq Cq Cd

    diu R i L u L i

    dt= + + + (5.4)

    According to Fig. 5.3, the q-axis current is set to zero in all condition for unity power factorcontrol while the reference current iCdis set by the DC-link voltage controller and adjust the

    active power flow between the grid and the DC-link. ForR 0equations (5.3), (5.4) can be

    reduced to:

    Cd

    Sd Cd Cq

    diu L u L i

    dt= + (5.5)

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    0Cq

    Cq Cd

    diL u L i

    dt= + + (5.6)

    With the q-axis current regulated to zero, the following equations (5.5 and 5.6) becomes

    C

    Sd Cd

    diu L u

    dt= + (5.7)

    0 Cq Cd u L i= + (5.8)

    As current controller, the PI-type can is used. However, the PI current controller has no

    satisfactory performance, because of the coupled system described by Eqs. (5.5), (5.6).

    Therefore, for high performance application with accuracy current tracking at dynamic state

    the decoupled controller should be applied. The output signals from PI controllers after dq/

    transformation (Eq. (5.1b)) are delivered to a Space Vector Modulator (SVM) which

    generates switching signals for power transistors.

    -

    udc_ref udc id_ref

    PI

    PI

    PIica

    icc

    icb

    PWM

    PI

    abc

    dq

    dq

    iq

    id -

    -

    -

    -

    ud

    uq

    us

    id_err

    iq_err us

    udc

    +

    +

    ul ul

    iq_ref

    = 0

    Fig. 5.3. Baseic block of VOC scheme

    +#"#" +#"#" +#"#" +#"#"

    5.2.2.1 VOC with active filtering function: total harmonic compensation method

    As an active filter, PWM rectifier is able to compensate higher harmonics in a grid current

    taken by the whole load. In order to compensate higher harmonics additional control block

    (AFF) has to be added to standard VOC strategy (Fig. 5.4).A PWM Rectifier part of control is the same like described in previous chapter. The distorted

    currents ila, ilb, ilc are delivered to the abc/dq transformation, where a fundamental (50 Hz)

    harmonic becomes a DC quantity and other harmonics are non-DC values. Next those signals

    are delivered to the High Pass Filter (HPF), which provides the higher harmonics signals

    extraction. Then higher harmonics compensating signals id_fr, iq_frare added with an opposite

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    sign to the standard VOC reference signals iCd, iCqand in the same provide higher harmonics

    compensation.

    _ _ _

    _ _ _

    d err Cd ref Cd d f

    q err Cq ref Cq q f

    i i i i r

    i i i i r

    =

    = (4.9)

    -

    udc_ref udc iCd_refPI

    PI

    PIica

    icc

    icb

    ilc

    ilb

    ila

    HPF

    PWM

    PI

    abc

    dq

    abc

    dq

    dq

    ab

    idl

    iCq

    iql

    iCd -

    -

    -

    -

    ud

    uq

    us aid_err

    iq_err usb

    udc

    HPFid_fr

    iq _ fr

    +

    +

    ul

    ul

    ul

    iCq_ref= 0

    AFF

    Fig. 5.4. Block diagram of VOC scheme with Active Filtering Function (AFF) block based on total

    harmonic compensation

    The compensating signals are high frequency components, added to the DC values reference

    signal produce non-DC reference signals passed to a PI controllers. These give non ideal

    conditions for PI controllers operation and produce an additional phase shift between

    reference and actual current.

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    5.2.2.2 VOC with active filtering function: selective harmonic compensation method

    7 harm

    id_fr iq_fr

    -

    udc_ref udc iCd_ref

    PI

    PI

    PIica

    icc

    icb

    PWM

    PI

    abc

    dq

    dq

    iCq

    iCd -

    -

    -

    -

    ud

    uq

    us

    id_err

    iq_err

    us

    udc

    +

    +

    ul ul

    iCq_ref

    = 0

    ul

    dq

    ilc

    ilb

    ila

    LPF

    abc

    dq

    idl_7h

    iql_7h

    LPFid_7h

    iq_7h

    ul

    dq

    ul 7*7*

    + +

    + +

    5 harm

    ilc

    ilb

    ila

    LPF

    abc

    dq

    idl_5h

    iql_5h

    LPFid_5h

    iq_5h

    ul

    dq

    ul-5* -5*

    11 harm 13 harm+ +

    Fig. 5.5. Block diagram of VOC with Active Filtering Function (AFF) scheme based on selective

    harmonic compensation

    In scheme of Fig. 5.5 active filtering function operates independently on few different main

    current harmonics, like 5th

    , 7th

    , 11th

    and 13th

    in harmonic synchronous coordinates [5.5, 5.15,

    5.17]. Moreover, nonlinear load currents ila, i lb, i lcare transformed to dq frame using suitably

    angle ul for each harmonic intended to compensation. Then the distorted currents ila, ilb, ilcare

    delivered to the Low Pass Filter (LPF), which provides the higher harmonics signals

    extraction. Next after back transformation dq/ these signals idfr and iqfrare added with an

    opposite sign to the standard VOC reference signals iCdand iCqgiving final commands id_err,

    iq_err delivered to PI current controllers. The same procedure is used for all specified

    harmonics.

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    +#"#$ +#"#$ +#"#$ +#"#$

    -

    udc_ref udc id_ref

    PI

    PI

    PIisa

    isc

    isb

    PWM

    PI

    abc

    dq

    dq

    abciq

    id -

    -

    -

    -

    ud

    uq

    us

    id_err

    iq_err

    us

    udc

    +

    +

    ul ul

    iq_ref

    = 0

    Fig. 5.6. VOC closed loop control strategy

    Closed loop control strategy of Fig. 5.6 operates like conventional VOC with the only change

    on current sensor location instead PWM rectifier input currents iLa, iLb, iLc, the source

    currents iSa, iSb, iScare measured and controlled.

    The nonlinear load current iL is not measured (see Fig. 5.1b). It is naturally created by the

    converter as a result of ac-line current sensor location at point of common coupling (PCC),

    where the system controls the current to be sinusoidal and may be determined by considering

    the summation of currents at the PCC:

    C S Li i i=

    The source currents iSa, iSb, iScare measured and taken into control strategy.

    +#"#) 7 8 9+#"#) 7 8 9+#"#) 7 8 9+#"#) 7 8 9 & ' 07 & ' 07 & ' 07 & ' 07((((&' 671&' 671&' 671&' 671

    Basic principles of virtual flux based active and reactive power estimation is presented below.

    It is economically motivated to replace the AC-line voltage sensors [3.1] with a virtual flux

    (VF) estimator [4, 6.1, 12]. The principle of VF is based on assumption that the voltages

    imposed by the line power in combination with the AC side inductors can be considered as

    quantities related to a virtual AC motor (see Fig. 5.7). Where R and L represent the stator

    resistance and leakage inductance of the virtual motor. Line to line voltages: USab, USbc, USca

    can be considered as induced by a virtual flux. Hence the integration of the voltages leads to

    determination of a virtual flux vector S , in stationary -coordinates presents Eq.5.11.

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    Fig. 5.7. PWM Rectifier

    With the definitions

    S Su dt = (5.9)

    where

    11

    2 2

    3 30

    2

    S S ab

    S

    S Sbc

    u uu

    u u

    = =

    (5.10)

    SS

    S SS

    u dt

    u dt

    = =

    (5.11)

    30

    2 2

    3 33

    2

    C Ca

    C

    C Cb

    i ii

    i i

    = =

    (5.12)

    1 11

    2 2 20

    3 3 30

    2 2

    CAM

    C

    C CBM

    C

    CCM

    uu

    u uu

    u

    = =

    (5.13)

    Operation of PWM rectifier is based on assumption, that input current ic is controlled by the

    voltage drop across the inductor L interconnecting line and converter voltage sources. It

    means that the inductance voltage uIequals the difference between the line voltage uSand the

    converter voltage uC

    S C Iu u u= + (5.14)

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    and similarly a virtual flux equation can be presented as:

    S C I = + (5.15)

    axis(fixed)

    axis

    d-axis(rotating)

    q-axis

    iC

    iCd

    iCq

    uS= u

    Sq

    S

    =t

    iC

    iC

    uS

    uS

    S

    S

    S

    uCuI

    =j

    Li L

    C

    I

    Fig. 5.8. Reference coordinates and vectors (for fundamental component): S virtual line flux vector,

    C virtual flux vector of converter, I virtual flux vector of inductor, uC converter voltage vector,

    uS- line voltage vector, uI inductance voltage vector, iC input current vector

    Based on the measured DC link voltage Udcand the duty cycles of SVM modulator SA, SB, SC

    the virtual flux Scomponents are calculated in stationary coordinates system as follows:

    2 1( ( )

    3 2S dc A B C C

    U S S S dt Li

    = + +

    (5.16a)

    1( )

    2S dc B C C U S S dt Li

    = +

    (5.16b)

    The measured input converter currents ica, icb and the estimated virtual flux components S

    ,Sare used for estimation of the instantaneous power. The voltage equation can be written

    as

    ( )CS C Cd

    u Ri Lidt

    = + + (5.17a)

    In practice,Rcan be neglected, giving

    C CCS C

    d i d diu L L u

    dt dt dt = + = + (5.17b)

    Using complex notation, the instantaneous power can be calculated as follows:

    Re( )S Cp u i

    = (5.18a)

    Im( )S Cq u i

    = (5.18b)

    where * denotes the conjugate line current vector. The line voltage can be expressed by the

    virtual flux as

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    ( )j t j t j tSSS S Sdd d

    u e e j edt dt dt

    = = = + j tSS

    de j

    dt

    = + (5.19)

    where Sdenotes the space vector and S its amplitude. For the virtual flux oriented d-q

    coordinates (Fig. 5.20), S=Sd, and the instantaneous active power can be calculated from

    (5.10a) and (5.11) as

    SdCd Sd Cq

    dp i i

    d t

    = + (5.20)

    For sinusoidal and balanced line voltages, equation (5.12) is reduced to

    0Sdd

    dt

    = (5.21)

    Sd Cqp i= (5.22)

    which means that only the current components orthogonal to the flux Lvector, produce the

    instantaneous active power.

    Similarly, the instantaneous reactive power can be calculated as:

    SdCq Sd Cd

    dq i i

    dt

    = + (5.23)

    and with (5.13) it is reduced to:

    Sd Cd q i= (5.24)

    As mentioned in [4] for sinusoidal and balanced line voltage the derivatives of the flux

    amplitudes are zero. By simulation and experiment investigation were proofed, that even for

    distorted line voltage the simplified equations for the instantaneous active and reactive powers

    can be used:

    ( )S C S C

    p i i = (5.25a)

    ( )S C S C q i i = + . (5.25b)

    The measured line currents iCa, iCb and the estimated virtual flux components S,S are

    delivered to the instantaneous power estimator block .

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    Fig. 5.9. VF-DPC control scheme

    A VF-DPC control strategy main scheme is presented in Fig. 5.9. The commanded (delivered

    from the outer PI DC voltage controller) active power prefand reactive power qref(set to zero

    for unity power factor) values are compared with the estimated instantaneous p and q values,

    respectively. The errors are delivered to PI controllers, where the variables are DC quantities

    and steady state error were eliminated. The output signals from PI controllers after

    transformation (5.29) are delivered to a Space Vector Modulator (SVM).

    Fig. 5.10. Power estimation block

    Fig. 5.10 shows an instantaneous powers estimation block. The angle is calculated using

    estimated virtual flux components Sa,Sb.

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    +#+#+#+#""""####++++

    Fig. 5.11. VF-DPC scheme with Active Filtering Function (AFF) block

    Fig. 5.12. Power estimation block

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    In this scheme of Fig. 5.11 measured input converter currents ica, icb and the estimated virtual

    flux components Sa,Sbare used for the power estimation Fig. 5.12. For a PWM rectifier

    operation the reference active powerpref(generated by the outer PI DC voltage controller) and

    reactive power qref (set to zero for unity power factor) values are compared with estimated

    instantaneouspand qvalues, respectively. The errors are delivered to PI controllers, which

    eliminates steady state error. The output signals from PI controllers after transformation

    pq/:

    sin cos

    cos sin

    C CpS S

    C CqS S

    u u

    u u

    =

    (5.26)

    where:

    ( ) ( )22

    sin / S S S S = + (5.27a)

    ( ) ( )22

    cos / S S S S = + . (5.27b)

    are used for switching signals generation by Space Vector Modulator.

    Here a modified algorithm based on virtual flux, which operates directly on instantaneous

    active and reactive power components is presented [5.6]. The instantaneous active and

    reactive powers are estimated using currents intended to compensate ila, ilb, ilcand virtual flux

    Sa,Sbaccording to Eqs (5.11a and b) as:

    ( )A S l S lp i i = (5.28a)

    ( )A L l L l

    q i i = + (5.28b)

    The calculated active power (pA) and reactive power (qA) are delivered to the high pass filter

    (HPF) to obtain values of the instantaneous active power ( p A) and reactive power (q A)

    which finally are used as a compensating components. Adding active filtering function will

    cause suitable distortion of input PWM rectifier current, which will assure almost sinusoidal

    line current. It permits to use PWM rectifier as a current harmonics eliminating device.

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    Fig. 5.13. Instantaneous power waveforms for different current shapes.

    a) current in phase with voltage b) current with phase shift c) distorted current

    From the top: grid voltage, grid current, active and reactive power

    Fig. 5.13 presents simulated examples of active and reactive powers for different current

    shapes. It is obvious that for sinusoidal voltage and in phase current an active power has a

    certain value and reactive power is equal 0 (Fig. 5.13a). In case that grid current is not in

    phase with grid voltage but is still sinusoidal, the active power will have the same level, but

    non zero value of reactive power will appear (Fig. 5.13b). If the current become a distorted

    one, in active and reactive powers a pulsation component will be visible (Fig. 5.13c).

    Summarizing, for higher harmonics elimination two high pass filters are needed, one for each

    power component. For higher harmonics elimination and reactive power compensation, onlyone high pass filter in active power is required (switch in Fig. 5.11).

    +#"#+#"#+#"#+#"#....

    Fig. 5.14. VF-DPC control block

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    Fig. 5.15. Power estimation block

    The nonlinear load current iLis not measured Fig. 5.1b. It is reconstructed by the converter as

    a result of AC-line current sensor location at point of common coupling (PCC), where the

    system controls the current to be sinusoidal and may be determined by considering the

    summation of currents at the PCC.

    C S Li i i= (5.29)

    The grid currents isa, isband the estimated virtual flux components Sa,Sbare used for

    estimation of power components. The reference active power pref and reactive power qref

    values are compared with the estimated instantaneouspand qvalues, respectively. The errors

    are delivered to PI controllers. The output signals from PI controllers after transformation

    pq/are used as a reference signals for Space Vector Modulator.

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    6. Dimensioning of Power Converters

    This chapter is devoted to dimensioning of power converters. This is obvious, that proper

    dimensioning is very critical issue for designing and selection of PWM Rectifier. Main power

    scheme of parallel connected conventional diode rectifier fed Adjustable Speed Drive (ASD)

    and modern PWM rectifier/inverter fed system is shown in Fig.6.1. It is very simp