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    ADVANCED POWER ELECTRONIC FORWIND-POWER GENERATION BUFFERING

    By

    ALEJANDRO MONTENEGRO LEN

    A DISSERTATION PRESENTED TO THE GRADUATE SCHOOL

    OF THE UNIVERSITY OF FLORIDA IN PARTIAL FULFILLMENTOF THE REQUIREMENTS FOR THE DEGREE OF

    DOCTOR OF PHILOSOPHY

    UNIVERSITY OF FLORIDA

    2005

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    Copyright 2005

    by

    Alejandro Montenegro Len

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    To my brother

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    iv

    ACKNOWLEDGMENTS

    I would like to first express my gratitude to Charles Edwards, the principle

    engineer at S&C Electric Co. (Chicago, IL) for his patience and the knowledge he shared

    throughout the project. I would also like to acknowledge Kenneth Mattern (manager at

    S&C Electric Co., Power Quality Division) for his constant encouragement and

    confidence in my ability. I am grateful to S&C Electric Company in general for all of

    their contribution and concern.

    Additionally, I would like to thank Alexander Domijan (my supervisory committee

    chair) for his funding during my graduate studies. My gratitude also goes to my

    supervisory committee (Dr. Ngo, Dr. Arroyo, and Dr. Goswami) for all of their time and

    effort.

    I would furthermore like to acknowledge my family in Spain, for supporting me

    and believing in me throughout my stay in the United States. I would finally like to

    express my love and gratitude to my girlfriend, Andrea Victoriano, for her help with the

    proofreading and for always being the shoulder I could lean on throughout the project

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    v

    TABLE OF CONTENTS

    page

    ACKNOWLEDGMENTS ................................................................................................. iv

    LIST OF TABLES........................................................................................................... viii

    LIST OF FIGURES ........................................................................................................... ix

    ABSTRACT.................................................................................................................... xvii

    CHAPTER1 INTRODUCTION........................................................................................................ 1

    Wind-Energy Outlook .................................................................................................. 1Electrical Issues ............................................................................................................ 3Solutions to Wind-Power Fluctuations.........................................................................9State of the Art.............................................................................................................. 9Objective..................................................................................................................... 11

    2 SYSTEM DESIGN.....................................................................................................14

    Introduction................................................................................................................. 14Control Scheme .......................................................................................................... 14

    Positive Sequence Calculation ............................................................................14Real Power Calculation Using dq Components ..................................................20Phase Locked Loop .............................................................................................21Control Algorithm Design...................................................................................26

    Inner regulators ............................................................................................27Outer regulators............................................................................................35

    Per-Unit System Model ..............................................................................................56Inverter Output-Filter Design..............................................................................56

    Harmonic content .........................................................................................57

    Switching frequency.....................................................................................60Passive filter design......................................................................................61Passive filter damping..................................................................................65

    Direct-Current Link Capacitor Design ................................................................68Energy Storage Design........................................................................................69Chopper Inductor Design ....................................................................................71Per-Unit System Model Summary.......................................................................72

    Simulated Model......................................................................................................... 73

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    3 SYSTEM DESCRIPTION..........................................................................................78

    System Overview........................................................................................................ 78Electrical Network Model...........................................................................................80

    Synchronous Machine .........................................................................................80Voltage regulation ...............................................................................................81Prime Mover ........................................................................................................ 81Synchronous Machine Control Algorithm ..........................................................83

    Wind-Farm Model ...................................................................................................... 87Wind-Farm Control Algorithm............................................................................90Wind-Farm Power-Factor Correction..................................................................90Wind-Farm Soft-Start System.............................................................................94

    Power Stabilizer.......................................................................................................... 97Power-Stabilizer Hardware Description..............................................................97

    Interface board..............................................................................................99Digital signal processor..............................................................................105Field-programmable gate array..................................................................106Intelligent power module ...........................................................................107Isolation interface circuit............................................................................108

    Power Stabilizer Software Description .............................................................108Description of DSP program......................................................................109FPGA program description ........................................................................114

    4 SYSTEM PERFORMANCE....................................................................................121

    System Data .............................................................................................................. 121Power Stabilizer Transient Response .......................................................................121

    Direct-Current Link Voltage Control................................................................121

    Reactive Current Control...................................................................................123Passive Filter Performance .......................................................................................126Voltage Regulation ...................................................................................................127System Losses........................................................................................................... 128Power Limiter Results ..............................................................................................130

    Power Limiter 1 (High Pass Filter) ...................................................................131Power Limiter 1 (Adaptive High Pass Filter)....................................................136Power Limiter 2.................................................................................................138

    Power Limiters Comparison Study...........................................................................145

    5 SUMMARY.............................................................................................................. 148

    Conclusions............................................................................................................... 148Further Work ............................................................................................................ 150

    APPENDIX

    A MATHEMATICAL TRANSFORMATIONS..........................................................151

    B MATLAB CODES ...................................................................................................158

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    C POWER STABILIZER CONTROL MODULES ....................................................168

    LIST OF REFERENCES.................................................................................................172

    BIOGRAPHICAL SKETCH ...........................................................................................176

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    viii

    LIST OF TABLES

    Table page

    1-1 Technical specifications of IEC and IEEE................................................................4

    1-2 Wind-farm output-power requirements.....................................................................8

    1-3 Large-scale wind-power output-leveling projects...................................................10

    1-4 Conceptual wind-power filtering projects...............................................................12

    1-5 Basic system configurations....................................................................................13

    2-1 Outer regulator assignation .....................................................................................35

    2-2 Rate-of-change limits or PPA for a 10 MW wind farm ..........................................47

    2-3 Generalized Harmonics of line-to-line voltage .......................................................59

    2-4 L filter vs. LCL filter...............................................................................................61

    2-5 LCL filter design ..................................................................................................... 64

    2-6 LCL equivalent impedance with damping resistance .............................................65

    2-7 Per-unit system........................................................................................................ 65

    2-8 Per-unit system parameters .....................................................................................73

    2-9 Designed system results and simulated system results comparison........................76

    3-1 Synchronous machine output voltage profile at rated speed...................................82

    3-2 Alternatives for the power stabilizer controller.....................................................106

    3-3 FPGA code words .................................................................................................120

    4-1 System parameters................................................................................................. 122

    A-1 Mathematical transformations summary...............................................................157

    C-1 Control Modules....................................................................................................168

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    LIST OF FIGURES

    Figure page

    1-1 Wind-power output for two wind farms during one month. .....................................5

    1-2 Power fluctuation comparison...................................................................................6

    1-3 Typical power curve of a wind turbine. ....................................................................6

    1-4 Wind-farm output power vs system frequency. ........................................................7

    1-5 Control strategies along the power curve..................................................................8

    1-6 Wind-farm generation buffering concept ................................................................13

    2-1 Unbalanced system..................................................................................................15

    2-2 Space vector trajectory of an unbalanced system in the d-q-o plane ......................16

    2-3 Space vector trajectory projection over the d-q plane.............................................16

    2-4 Direct and quadrature components of an unbalanced system .................................17

    2-5 Representation of an unbalanced system in the frequency domain.........................17

    2-6 Positive-sequence extraction algorithm ..................................................................19

    2-7 Voltage waveforms for an unbalanced fault event..................................................19

    2-8 Response of the positive-sequence extraction algorithm ........................................20

    2-9 Distortion of phase angle due to a negative sequence component ..........................22

    2-10 PLL diagram............................................................................................................ 23

    2-11 PLL simplified model..............................................................................................24

    2-12 PLL system step response .......................................................................................25

    2-13 Root locus for two different regulator gains ...........................................................25

    2-14 PLL system response to an unbalanced system condition ......................................26

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    2-15 PLL system response to a frequency excursion ......................................................26

    2-16 System description ..................................................................................................27

    2-17 Simplified system model .........................................................................................28

    2-18 Electrical representation of the dq components ......................................................30

    2-19 System model block diagram ..................................................................................30

    2-20 Inverter current regulator-system model block diagram .........................................31

    2-21 Inverter current regulator-system model simplified block diagram........................32

    2-22 Simplified current control diagram .........................................................................32

    2-23 Current regulator step response...............................................................................33

    2-24 Chopper equivalent system .....................................................................................34

    2-25 Chopper current controller ......................................................................................35

    2-26 Powers' definition.................................................................................................... 36

    2-27 System model .......................................................................................................... 37

    2-28 DC link equivalent system block diagram ..............................................................37

    2-29 DC link simplified system block diagram...............................................................38

    2-30 DC link voltage regulator step response .................................................................38

    2-31 Simplified system model .........................................................................................40

    2-32 Source impedance voltage drop ..............................................................................41

    2-33 Transfer functions of inverters quadrature current component..............................42

    2-34 Transfer functions of inverters direct current component......................................42

    2-35 Voltage regulator system block diagram.................................................................44

    2-36 Positive sequence extraction algorithm equivalent system.....................................44

    2- 37 Voltage regulator detailed block diagram ...............................................................45

    2- 38 Voltage regulator simplified control diagram .........................................................45

    2- 39 System response to a 5% change in voltage reference............................................45

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    2-40 Adaptive control scheme.........................................................................................46

    2-41 Power Regulator general control scheme................................................................47

    2-42 Power limiter 1. Control block diagram..................................................................48

    2-43 Power limiter 1. Performance using different cut-off frequencies (unlimitedpower and energy)....................................................................................................49

    2-44 Power limiter 1. Performance using different cut-off frequencies (Pinverter=1.0MW and Einverter=8.5 MJ) .......................................................................................49

    2-45 Power limiter 2. Limiters details .............................................................................50

    2-46 Power limiter 2. Control block diagram..................................................................51

    2-47 Power limiter 2. Compensation performance.........................................................51

    2-48 Power limiter 2. Inverter response for a sampling time of 2 seconds .....................52

    2-49 Power limiter 2. Inverter response for different power ratings. Sampling time 2seconds ..................................................................................................................... 53

    2-50 Power limiter 2. Inverter response for different ESS sizes. Sampling time 2seconds ..................................................................................................................... 53

    2-51 Power limiter 3. Control block diagram..................................................................54

    2-52 Power limiter 3. Compensation performance.........................................................55

    2-53 Power limiter 3. Inverter response for a sampling time of 2 seconds .....................55

    2-54 Inverter topology ...................................................................................................... 57

    2-55 Line-to-line and line-to-neutral voltage of a three phase inverter...........................57

    2-56 RMS Line-to-line voltage harmonic spectrum........................................................58

    2-57 Static Synchronous Generator diagram...................................................................59

    2-58 LCL filter topology .................................................................................................61

    2-59 LCL equivalent block diagram................................................................................62

    2-60 Single phase equivalent filter model at the fundamental frequency .......................62

    2-61 Single phase equivalent filter model at the hth harmonic ........................................63

    2-62 LCL equivalent impedance with damping resistance .............................................66

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    2-63 Single phase harmonic generator equivalent circuits ..............................................66

    2-64 LCL gain frequency response .................................................................................67

    2-65 Inverter frequency analysis .....................................................................................67

    2-66 Capacitor Voltage vs. Energy Storage ....................................................................70

    2-67 ESS-Chopper topology............................................................................................71

    2-68 Equivalent circuit for maximum current ripple calculation ....................................72

    2-69 System overview ..................................................................................................... 74

    2-70 Per-unit electric system model ................................................................................74

    2-71 Power Stabilizer Control Scheme ...........................................................................75

    3-1 Equivalent system model ........................................................................................79

    3-2 DC gen-set............................................................................................................... 83

    3-3 Two single quadrant chopper circuit .......................................................................83

    3-4 Synchronous generator control system ...................................................................84

    3-5 Frequency deviation ................................................................................................85

    3-6 DC-GEN set control scheme ...................................................................................85

    3-7 System frequency response forf=-1Hz ................................................................86

    3-8 Frequency control equivalent system......................................................................87

    3-9 Equivalent model frequency response forf= - 0.01666 pu ..................................88

    3-10 Dynamic model used for transient studies ..............................................................88

    3-11 Static model used for steady-state studies...............................................................88

    3-12 Wind-farm model ....................................................................................................89

    3-13 Wind-farm controller...............................................................................................90

    3-14 Wind-farm power regulator & current regulator step response (P=100%) ..........91

    3-15 Induction generator PQ curve .................................................................................92

    3-16 Wind-farm PF correction capacitor bank ................................................................93

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    3-17 PF correction capacitor bank current waveforms....................................................93

    3-18 Capacitor bank impedance frequency scan .............................................................94

    3-19 Machine control scheme operating states................................................................95

    3-20 Electric power system start-up ................................................................................96

    3-21 Detail of the transition from start-up mode to run mode.........................................96

    3-22 Power Stabilizer system overview ..........................................................................97

    3-23 Interface board overview.......................................................................................100

    3-24 AC voltage scaling circuit (input [-1000+1000V], output [0 +3V]) .....................101

    3-25 DC voltage scaling circuit (input [0 +1000V], output [0 +3V]) ...........................101

    3-26 CT current scaling circuit (input [-5 +5A], output [0 +3V]).................................101

    3-27 LEM current scaling circuit (input [-0.36 +0.36A], output [0 +3V])....................101

    3-28 Power supplies voltage monitoring......................................................................102

    3-29 Systems critical signals during turn on ................................................................103

    3-30 Systems critical signals during turn off ...............................................................103

    3-31 Darlington drivers .................................................................................................104

    3-32 IPM status signals interface circuitry ...................................................................104

    3-33 DAC circuit ........................................................................................................... 105

    3-34 DSP built-in PWM output performance vs. FPGA...............................................107

    3-35 IMP power circuit configuration ...........................................................................108

    3-36 Isolated interface board .........................................................................................109

    3-38 Power stabilizer control algorithm sampling rates................................................110

    3-37 Interconnections between the different sub-systems of the power stabilizer........111

    3-39 Power stabilizer control stages..............................................................................113

    3- 40 Power stabilizer start-up sequence ........................................................................113

    3-41 FPGA system overview.........................................................................................116

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    3-42 Up/Down counter. .................................................................................................117

    3-43 PWM generator ..................................................................................................... 117

    3-44 One phase dead-time generator detailed diagram .................................................119

    3-45 Dead-time generators waveforms ........................................................................119

    3-46 Watchdog logic .....................................................................................................120

    4-1 DC link voltage response for different Kp gains...................................................121

    4-2 DC link voltage response for different Ki gains ...................................................122

    4-3 Iqrefcommand step change from -0.5 to 0.5 A per unit. Integral gain effect ........123

    4-4 Iqrefcommand step change from -0.5 to 0.5 A per unit. Proportional gain

    effect....................................................................................................................... 1244-5 Iq current regulator output for different Kp ..........................................................124

    4-6 Iqref command step change from -0.5 to 0.5 and back to -0.5 A per unit ............124

    4-7 Power stabilizer harmonic injection response for Ki=18 and Kp=1 .....................125

    4-8 Current regulator frequency response ...................................................................126

    4-9 Front-end inverter current waveform ....................................................................126

    4-10 Frequency spectrum of the LCL currents..............................................................1274-11 Simplified system description ...............................................................................127

    4-12 Power stabilizer voltage regulation performance..................................................128

    4-13 Energy storage charge/discharge cycle .................................................................129

    4-14 Control scheme with a losses compensation term.................................................129

    4-15 Power stabilizer equivalent system .......................................................................130

    4-16 Wind-power conditions under study .....................................................................1304-17 Measured and modeled high pass filter results for Kc=0.0064 W/J,

    fcut_off=0.005 Hz......................................................................................................132

    4-19 Measured high pass filter performance for different cut-off frequencies. Systemparameters Kc=0.0064 W/J.....................................................................................134

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    4-20 Modeled high pass filter performance for different cut-off frequencies. Systemparameters Kc=0.0064 W/J.....................................................................................135

    4-21 Measured high pass filter performance for different energy storage sizes.System parameters, Kc=0.0064 W/J, fcut-off=0.005 Hz. ..........................................135

    4-22 Cut-off frequency trajectory of the adaptive high pass filter for a given energydeviation................................................................................................................. 136

    4-23 Measured adaptive high pass filter performance for different Kfs. Systemparameters, Kc=0.0064 W/J, fcut-off-origin=0.005 Hz.................................................137

    4-24 Measured adaptive high pass filter performance for different energy storagesizes........................................................................................................................ 137

    4-25 Multiple sampling concept. ...................................................................................139

    4-26. Measured and modeled power limiter 2 results for Kc=0.0064, RR=2MW/minute, A=0.3 MW/minute, I=1MW/2 seconds fcut-off=0.005 Hz. ................140

    4-27 Measured power indexes activity. System parameters: Kc=0.0064 W/J, RR=2MW/minute, A=0.3 MW/minute, I=1 MW/2 seconds, and fs=10Hz.....................141

    4-28 Measured power limiter 2 response to different Kc . System parameters: RR=2MW/minute, A=0.3 MW/minute, I=1MW/2 seconds, and fs=10Hz......................142

    4-29 Measured power limiter 2 response to different ramp rate limits. ........................142

    4-30 Measured power limiter 2 response to different average power fluctuation

    limits....................................................................................................................... 143

    4-31 Effect of linear interpolation on the average power fluctuation index activity.The sampling time of the original wind-power data is 2 seconds.... ......................144

    4-32 Measured power limiter 2 response to different instantaneous power fluctuationlimits....................................................................................................................... 144

    4-33 Measured power limiter 2 response to different sampling frequencies.................145

    4-34 Measured synchronous machine output power for the different power limiter

    control schemes......................................................................................................1464-35 Measured synchronous machine output power for the different power limiter

    control schemes. .....................................................................................................147

    4-36 Frequency regulator output for the different power limiters.................................147

    A-1 Relationships among ds-qs, and abc axes .............................................................153

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    A-2 Stationary ds-qs components in the time domain.....................................................153

    A- 3 Relationship among ds-qs and dr-qraxes ...............................................................154

    A-4 Direct and quadrature components........................................................................155

    A-5 Time domain representation of abc and d-q components .....................................156

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    Abstract of Dissertation Presented to the Graduate Schoolof the University of Florida in Partial Fulfillment of theRequirements for the Degree of Doctor of Philosophy

    ADVANCED POWER ELECTRONIC FORWIND-POWER GENERATION BUFFERING

    By

    Alejandro Montenegro Len

    May 2005Chair: Alexander Domijan, JrMajor Department: Electrical and Computer Engineering

    As the cost of installing and operating wind generators has dropped, and the cost of

    conventional fossil-fuel-based generation has risen, the economics and political

    desirability of more wind-based energy production has increased. High wind-power

    penetration levels are thus expected to augment in the near future raising the need for

    additional spinning reserve to counteract the effects of wind variations. This solution is

    technologically viable, but it has high associated costs. Our study presents a different

    solution to short-term wind-power variability, using advanced power electronic devices

    combined with energy-storage systems. New control schemes (designed to filter power

    swings with a minimum of energy) were designed, modeled and verified through

    experimental tests. We also determined the procedure to extract the corresponding per-

    unit model parameters for simulations and test purposes.

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    We first reviewed D-Q transformations with emphasis on modeling of the system

    and control algorithm. System components were then designed using criteria similar to

    those used to design medium-voltage power products.

    We tested a proof-of-concept for performance of the power converter in a scaled-

    down isolated system using real wind-power data. Tests were conducted under realistic

    system conditions of wind-penetration level and energy-storage levels, to better

    characterized the impacts and benefits of the Power Stabilizer. We described the scaled-

    down isolated electric power system used in the testing. We also analyzed the

    performance of the wind-farm model and the synchronous machines governor to gain aninsight into the model systems limitations.

    Simulation results carried out in Mathematical Laboratory (MATLAB) and Power

    Systems Computer Aided Design (PSCAD) were compared to experimental data to verify

    the performance of the power converter under different system conditions and algorithms.

    Power limiters were also contrasted and evaluated for frequency deviations and

    attenuated power fluctuations.

    In summary we can say that, among all the power limiters considered in our study,

    the adaptive high pass filter presented the best performance in terms of system robustness

    and effectiveness.

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    1

    CHAPTER 1INTRODUCTION

    Wind-Energy Outlook

    Wind power has been used for at least 3000 years, mainly for milling grain,

    pumping water, or driving various types of machines. However, the first attempt to use

    wind turbines for producing electricity date back to the 19th century. In 1891, Poul La

    Cour in Demark built an experimental wind turbine driving a dynamo. The oil crisis of

    the 1970s revived interest in wind turbines. Nowadays, the power is the fastest growing

    source of energy in the world and its growth rates have exceeded 30% annually over the

    past decade [1]. Cumulative global wind-energy generating capacity approached 40,000

    MW by the end of 2003 [2]-[3]. The main drivers for developing of the wind industry in

    the United States are

    Federal Renewable Energy Policies, particularly the Production Tax Credit (PTC)that provides a 1.5 cent per kilowatt-hour credit for electricity produced from awind farm during the first 10 years of operation. This wind energy PTC expiredDecember 31, 2003 but will be reinstated through 2005 as part of a major taxpackage (H.R. 1308).

    State-level renewable energy initiatives, such as the Renewable Portfolio Standard,or green pricing.

    The Database of State Incentive for Renewable Energy [4] gives more information

    on incentives. These government initiatives, together with technological advances, plus

    the need for a new source of energy capable of meeting the worlds growing power

    demand and the rising prices of conventional fossil fuel-based generation, make the wind

    power one of the most promising industries in the future.

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    According to the European Wind Energy Association and Greenpeace, no barriers

    exist for wind to provide 12% of the worlds electricity by 2020. The American Wind

    Energy Association forecasts that wind power will provide 6% of the USs electricity by

    2020 if the wind industry maintains an annual growth rate of 18%.

    The positive effects of using such types of renewable resources are well known.

    However, wind-power plants, like all other energy technology, have some drawbacks that

    should be mentioned. These problems can be divided into major groups: environmental

    issues and interconnection issues.

    Environmental issues. Most significant among these are the following: Sound from turbines: Some wind turbines built in the early 1980s were very

    noisy. However, manufactures have been working on making the turbines quieter.Today, an operating wind farm at a distance of 750 to 1,000 feet is no noisier than amoderately quiet room. Research in aero-acoustics is still being carried out tofurther reduce noise from wind on the blades.

    Bird death: Wind turbines are often mentioned as a risk to birds, and severalinternational tests have been performed. The general conclusion is that birds areseldom bothered by wind turbines. Studies show that for example, overhead powerpole lines are far more hazardous for birds than wind turbines [2].

    Wind-tower shadow effect: Wind turbines, like other tall structures cast a shadowon the neighboring area when the sun is visible. It may be irritating if the rotorblades chop the sunlight, causing a flickering effect while the rotor is in motion,especially when the sun is low in the sky.

    Interconnection issues. Connecting wind turbine to operate in parallel with the

    electric power system influences the system operating point (load flow, nodal voltages,

    power losses, etc). These changes in the electric power system state bring up new system-

    integration issues that system operators and power quality engineers must take into

    account. These interconnection issues can be divided into operational issues and electrical

    issues.

    Operational Issues: These include unit commitment and spinning reserve.

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    3

    The unit commitment problem is to schedule specific or availablegenerators (on or off) on the utility system to meet the required loads at aminimum cost, subject to system constraints. The most conservativeapproach to unit commitment and economic dispatch is to discount anycontribution from interconnected wind resources because of wind

    variability. Operating reserve is further defined to be a spinning or non- spinning

    reserve. Any probable load or generation variations that cannot beforecasted, such as wind power, have to be considered when determiningthe amount of operating reserve to carry out.

    Electrical issues: These factors are considered in the next section.

    Electrical Issues

    Wind-turbine generator-system operation has some negative influence on power

    systems. This influence on the electric power system depends on wind variations and on

    wind-turbine technology. Impacts on the electric power system can be grouped as

    follows:

    Power quality: Voltage variations, flicker, harmonics, power-flow variations Voltage and angle stability Protection and control

    The IEEE 1547 [5] and the IEC 61400-21 [6] standards are the bases to evaluating

    the impact of such wind-turbine generation systems on the electric power system.

    According to the IEEE 1547 [5, page 2] abstract,

    This standard focuses on the technical specifications for, and testing of, theinterconnection itself. It provides requirements relevant to the performance,operation, testing, safety considerations, and maintenance of the interconnection. Itincludes general requirements, response to abnormal conditions, power quality,islanding, and test specifications and requirements for design, production,

    installation evaluation, commissioning, and periodic tests. The stated requirementsare universally needed for interconnection of distributed resources (DR), includingsynchronous machines, induction machines, or power inverters/converters and willbe sufficient for most installations. The criteria and requirements are applicable toall DR technologies, with aggregate capacity of 10 MVA or less at the point ofcommon coupling, interconnected to electric power systems at typical primaryand/or secondary distribution voltages.

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    According to the IEC 61400-21 [6, page 9] abstract,

    The purpose of this part of IEC 61400 is to provide a uniform methodology thatwill ensure consistency and accuracy in the measurement and assessment of powerquality characteristics of grid connected wind turbines (WTs). In this respect the

    term power quality includes those electric characteristics of the WT that influencethe voltage quality of the grid to which the WT is connected.

    This standard provides recommendations for preparing the measurements andassessment of power quality characteristics of grid connected WTs.

    Table 1-1 shows technical specifications for interconnection and power assessment

    covered in both standards.

    Table 1-1. Technical specifications of IEC and IEEEInterconnection systemresponse to excursions Power quality assessment

    IEEE VoltageFrequency

    IEC VoltageFrequency

    Voltage fluctuations:Continuous operationSwitching operation

    Harmonics

    As shown in Table 1-1, both standards overlooked one of the most significant

    characteristics of wind farms: its variability (i.e., power fluctuations) [7], the mostimportant ones being

    Gusty wind variations having a spectrum of frequencies from 1-10 Hz.

    Shadow effect having a spectrum of frequencies from 1-2 Hz and producing torquevariations up to 30%.

    Complex oscillations of the turbine tower, rotor shaft, gear box, and blades withspectrum frequencies from 2-100 Hz, and creating torque variations up to 10%.

    Figure 1-1 shows actual output power data collected by NREL from two large

    wind-power plants in the United States. The small wind farm has a capacity of about 35

    MW, and the large one has a capacity of 150 MW.

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    5

    0 0.5 1 1.5 2 2.5 3

    x 106

    0

    10

    20

    30

    40

    Power(MW)

    Time (s)

    0 0.5 1 1.5 2 2.5 3

    x 106

    0

    50

    100

    150

    Trent Mesa Project. Wind power output May 2003

    Power(MW)

    Time (s)

    Figure 1-1. Wind-power output for two wind farms during one month (May 2003). A)

    Nominal capacity 35 MW. B) Nominal capacity 150 MW.

    Even though the technology used in constructing the small wind farm is more than

    a decade older than the large one, power fluctuations keep being an issue. Figure 1-2 is a

    close-up ofFigure 1-1 and shows the magnitude of these power fluctuations.

    Wind turbine manufactures usually provide power curves (Figure 1-3) to

    developers to determine the amount of power that will be transferred into the grid for a

    single turbine, given the wind speed. However, those figures represent only the mean

    values, since a series of stochastic values cannot be controlled, and create additional

    power fluctuations.

    Wind-output power fluctuations can have different effects on the electric power

    system, but the most significant ones are voltage variation and frequency variation in

    small or isolated systems.

    A

    B

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    6

    0 1 2 3 4 5 6 7 8

    x 104

    0

    10

    20

    30

    40

    .

    Power(MW)

    Time (s)

    0 1 2 3 4 5 6 7 80

    50

    100

    150

    Trent Mesa Project. Wind power output May 2003

    Power(MW)

    0 1 2 3 4 5 6 7 8

    x 104

    0

    10

    20

    30

    40

    Power(MW)

    Time (s)

    0 1 2 3 4 5 6 7 8

    x 104

    40

    50

    60

    70

    80Trent Mesa Project. Wind power output May 2003

    Power(MW)

    Time (s)

    Figure 1-2. Power fluctuation comparison. A) Nominal capacity 35 MW. B) Nominalcapacity 150 MW.

    Figure 1-3. Typical power curve of a wind turbine.

    As the power fluctuates, the reactive power required by the turbines changes as

    well, and therefore voltage variations are expected, especially when the wind farm is

    A

    B

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    7

    located at weak points in the system. To compensate for such voltage variations and keep

    the voltage close to its rated value, several solutions are available: simple capacitor

    banks, static voltage compensator (SVC), or static compensators (STATCOM).

    A different approach must be taken for frequency variations due to power

    fluctuations. Normally, wind farms connected to big systems do not present a major

    problem in terms of frequency variations, because of the stiffness of the system.

    However, with small or isolated systems that contain slow or no automatic generation

    controls, a mismatch between generated and absorbed power can significantly affect

    system frequency unless spinning reserves are significant. Figure 1-4 shows the effect ofwind-power fluctuation on an isolated system with a wind penetration level of 1%.

    To counter these negative effects, countries and small isolated systems with high

    wind-penetration factors developed special purchase power agreement (PPA)

    requirements or indexes for wind-farm developers (Table 1-2).

    Figure 1-4. Wind-farm output power vs system frequency.

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    8

    Table 1-2. Wind-farm output-power requirements

    Ramp Rate dP/dt InstantaneousAverage (maxvariation)

    Netherlands

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    9

    Solutions to Wind-Power Fluctuations

    To reduce the effects of wind-power variations and meet the PPA requirements for

    electric utilities, two solutions can be considered:

    Higher spinning reserves Wind farm buffer

    Increasing spinning reserves is a costly solution. A better approach would be to use

    an energy-storage system that could deliver the required power when needed.

    Work has been done in developing large-scale energy storage systems that have

    overcome these issues by absorbing undesirable power fluctuations and providing firm,

    dependable peaking capacity [8]. However, a less costly solution should be explored

    based exclusively on power-fluctuation indexes (such as ramp rate indexes or

    instantaneous fluctuation indexes).

    State of the Art

    Storing wind power is not a new concept; in fact, back in 1900, the father of the

    modern wind turbine, Poul La Cour, tackled for the first time the problem of energy

    storage. He used the electricity from the wind turbines for electrolysis and to store energy

    in the form of hydrogen. However, with time, system requirements, energy storage

    systems, and wind turbine ratings have changed.

    Nowadays, the average wind turbine installed is around 1 MW, according to the

    European Wind Energy Association, and wind-power farms usually consists of ten to

    several tens of wind-turbine generators of rated power up to 2 MW. Thus, the amount of

    energy storage needed to stabilize the power output change in the short term has

    increased. Table 1-3 shows some recent projects dealing with output leveling of wind-

    energy conversion.

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    Table 1-3. Large-scale wind-power output-leveling projects

    Project name Wind farm size Energy storage systemActive power refercontrol scheme

    Subaru Project [9].Tomamae wind-powerstation.

    1.65 MW *16(Vestas).1.5 MW * 5(Enercon).

    Total Capacity30.6 MW

    VanadiumRedox Flow Battery

    PVRB nominal =4.000kWEVRB=6.000kWhS inverter=6.000kVA

    Moving Average odetermined as

    Pbattery=Pwind average ((fort=8 seconds t

    King Island [10]. Energy-storage system providedby Pinnacle VRB

    250 kW*3850 kW*2

    Total Capacity2.45 MW

    VanadiumRedox Flow Battery

    PVRB nominal=200kWPVRB short-term ( 5 minutes)=300kWPVRB short-term (10 seconds)=400kWEVRB =1100kWh

    Isochronous frequepower range.

    Speed droop characand short-term loa

    Oki project by FujiElectric

    600 kW *3

    Total Capacity1.8 MW

    Flywheel

    E flywheel = 100 kW - 90 secP inverter flywheel side= 110kVAP inverter power system side= 150kVA

    Power ramp rate lim

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    11

    However, small-scale concepts and technical/economic feasibility studies have

    been proposed (Table 1-4). Each of these projects has a different objective (frequency

    control, power smoothing, load leveling, etc.). However, they all end up using one of the

    topologies and energy-storage systems shown in Table 1-5, where the flywheel or

    capacitors may be replaced by some other energy-storage medium. Tables 1-3 and 1-4

    show that the amount of energy needed for wind-power balancing using current

    technology and current pricing is so significant, that a more flexible and integrated

    approach is needed.

    Our study focused on developing new power smoothing control algorithms. Thenew integrated approach used a shunt-connected voltage-source converter with added

    storage included on the DC link bus. The system can

    Exchange active power with the system. Regulate voltage at the point of common coupling Increase power quality and system stability

    Objective

    Our purpose was to develop, simulate, and implement a proof-of-concept prototype

    advanced-power electronic device capable of controlling and smoothing the power

    fluctuations of a wind farm using an optimal amount of energy. The wind-power

    generation buffering concept is shown in Figure 1-6. The Power Stabilizer was designed

    to store excess power during periods of increased wind-power generation and release

    stored energy during periods of decreased generation due to wind fluctuations.

    We tested the performance of the advanced electronic device on

    DC-synchronous machine set Passive load DC-asynchronous machine set Wind-farm buffer or also called Power Stabilizer

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    Table 1-4. Conceptual wind-power filtering projectsWind farm size Energy storage system Active power reference control scheme 20 MW Zinc-bromide battery

    PZBB nominal (charge) =-750kWPZBB nominal (discharge)=1500kWEZBB =1500 kWh

    Limiting instantaneous power fluctuations basedon a 2 seconds intervalPinstantaneous (t=2 seconds) = 1.3 MWAverage power levels over a 2 hour windowPaverage(t- t=2hours)= 200 kW

    Maximum poweroscillation 2.5 MW

    Super-conducting magneticenergy storage (SMES)

    Active power reference is chosen to controlsystem frequency

    300kW Electric double layercapacitorP ECS =100 kWE ECS =1.1 kWh

    ESS active power reference is determined bydetection power oscillation components using ahigh pass filter

    6GW Redox-flow battery(Regenesys )E=62004 MWhP=255MW

    Power balancing

    45KW FlywheelE flywheel= 12MJP drive=45kW

    The active power demand is extracted via a 2ndorder Butterworth high pass filter, with a 5mHzbandwidth

    55kW Lead Acid BatteryE battery=35kWhP converter=50kVA

    Power smoothing

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    13

    A

    B

    C

    A

    B

    C 0.69

    #2 #1

    12.47

    ?L1

    L2

    L3

    Vestas

    VRCCV47

    VnaS

    NAS

    VnbS

    NBS

    VncS

    NCS

    A

    B

    C

    A

    B

    C0.48

    #2#1

    12.47

    ?

    g1

    g2

    g3

    g4

    g5

    g6

    2

    1

    300.0

    2

    3

    2

    5

    2

    4

    2

    6

    2

    2

    dcCur

    gc12

    5

    gc22

    5

    1.0

    ChopperReactor

    1.0

    EnergyStorageCapacitor

    A

    B

    C

    A

    B

    C 12.47

    #2 #1

    69.0

    ?

    INVERTER

    WIND FARM

    0 20 40 60 80 100 1208800

    9000

    9200

    9400

    9600

    9800

    10000

    10200

    10400

    10600

    10800Wind Power Output

    Power(W)

    Time (s)

    0 20 40 60 80 100 120-1000

    -800

    -600

    -400

    -200

    0

    200

    400

    600Power Stabilier Power Output

    Power(W)

    Time (s)

    0 20 40 60 80 100 1208800

    9000

    9200

    9400

    9600

    9800

    10000

    10200

    10400

    10600

    10800Wind Power Output

    Power(W)

    Time (s)

    Wind power + Wind farm buffer Power

    Figure 1-6. Wind-farm generation buffering concept

    Table 1-5. Basic system configurations

    System configuration

    Voltage source inverterESS connected at the DC link side [19]-[21]-[24]

    SynchronousMachine

    Voltage Source

    Inverter

    ESS (flywheel)

    Electric SystemWind Turbine

    DClink

    ESS connected at the AC side [18]-[20]-[22]-[23]-[25]

    InductionMachine

    Voltage Source

    Inverter ESS (flywheel)

    Electric SystemWind Turbine

    DClink

    Current source inverter (shunt connected) [13]

    InductionMachine

    Current Source

    Inverter ESS (capacitors)

    Electric SystemWind Turbine

    Chopper(DC/DCconverter)

    ECS

    Energy storage system

    Available options [26] Compressed air energy storage Battery storage Electro-chemical flow cell systems Fuel cell/electrolyser/hydrogen systems Kinetic energy (flywheel) storage Pumping water

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    15

    =

    =

    =

    240

    120

    0

    0.1

    0.1

    5.0

    c

    b

    a

    V

    V

    V

    (2-1)

    Figure 2-1 shows the time domain representation of this three-phase unbalanced system.

    Figure 2-1. Unbalanced system

    If we now calculate the symmetrical components of this unbalanced system, we obtain

    =

    =

    =

    1800

    1802

    01

    167.0

    167.0

    833.0

    V

    V

    V

    (2-2)

    The symmetrical components transformation is a good tool to determine the type of

    distortion or asymmetry the system has. However, it has the drawback of having to use

    phasors as input instead of time domain signals. Therefore a different transformation was

    needed in order to extract the positive sequence component out of the rotating space

    vector.Figure 2-2 shows the trajectory followed by the rotating space vector of the

    unbalanced system in the d-q-o plane using Clarkes transformation. This trajectory is

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    16

    clearly distorted from the ideal one, and the space vector no longer follows a circular path

    (Figure 2-3).

    Figure 2-2. Space vector trajectory of an unbalanced system in the d-q-o plane

    Figure 2-3. Space vector trajectory projection over the d-q plane

    Figure 2-4 shows the Vdrand Vqrcomponents (Parks transformation) of the

    unbalanced system in the time domain for= 0.

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    Figure 2-4. Direct and quadrature components of an unbalanced system

    It is clear that the Vdrcomponent is not constant any more, and it contains a 2nd

    harmonic due to the negative sequence. This effect can also be explained in the frequency

    domain as shown in Figure 2-5. The rotating reference frame aligns with the fundamental

    frequency, w=2f, and therefore

    a negative sequence (-w) appears as a 2nd harmonic a dc component appears as a 1st harmonic a positive sequence (w) has a constant value.

    abcaxis

    drq

    raxis

    0.167

    0.833

    -w wdcw

    dc-w-2w

    Figure 2-5. Representation of an unbalanced system in the frequency domain

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    Thus, it can be concluded that Clarkes and Parks transformations do not provide

    suitable components that can be used in a voltage regulation control algorithm. It is

    therefore necessary then to redefine the transformations in order to extract the desired

    components.

    Assuming the three-phase electric system has positive and negative sequence

    components

    )34

    cos()34

    cos(

    )3

    2cos()

    3

    2cos(

    )cos()cos(

    ++=

    ++=

    +=

    wtVwtVV

    wtVwtVV

    wtVwtVV

    npc

    npb

    npa

    (2-3)

    Clarkes transformation can be used to obtain

    +

    +

    +==

    +=+=

    qsqsnpqs

    dsdsnpds

    VVwtVwtVV

    VVwtVwtVV

    )sin()sin(

    )cos()cos((2-4)

    where+ds

    V and+qs

    V are the d-q components of the positive sequence, whileds

    V andqs

    V

    are the d-q components of the negative sequence.If we now assume that the symmetrical components remained constant for at least a

    quarter of cycle, the equations can be rewritten as

    ( ) ( )

    ( ) ( )

    ( ) ( )

    ( ) ( )

    =

    +=

    +

    =

    =

    +

    +

    ttt

    ttt

    ttt

    ttt

    qsdsqs

    qsdsds

    qsdsqs

    qsdsds

    V2

    V2

    1V

    2VV

    21V

    V2

    V2

    1V

    2VV

    2

    1V

    (2-5)

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    These components can now be transformed using the rotating reference frame in

    order to obtain the positive sequence component. Figure 2-6 shows the block diagram of

    the algorithm used to extract the positive-sequence component. The same concept could

    be used if the negative sequence magnitude is needed.

    abd

    dsq

    s

    Vds

    Vqs

    Delay (1/f/4)

    +

    +

    0.5

    Delay (1/f/4)

    _

    +

    0.5

    Vds+

    Vqs+

    dsqs

    drq

    r

    x+

    +

    +

    Vdr+

    Vqr+

    x Vmagnitudepositive sequence

    Vdr

    Vqr

    VaVbV

    c

    dsq

    s

    drqr

    Filter

    Sliding windowfilter

    Figure 2-6. Positive-sequence extraction algorithm

    Figure 2-8 shows the algorithm performance when an unbalanced fault condition

    takes place at t=0.02 sec (Figure 2-7). The data used for this example is given by

    Equation 2-2.

    Figure 2-7. Voltage waveforms for an unbalanced fault event

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    Figure 2-8. Response of the positive-sequence extraction algorithm. A) Positive sequenceusing and 1 cycle filters. B) Positive sequence using Vdrwith 1 cycle filter

    The meaning of the different plotted variables is the following:

    Vpositive-sequence magnitude is the output of the positive-sequence extraction algorithm. Asexpected, its time response is only one quarter of a cycle. However, the transientresponse is very abrupt an uneven.

    Vpositive-sequence magnitude (1/2 cycle filter) is the filtered signal of Vpositive-sequence magnitude usinga half cycle sliding window filter.

    Vpositive-sequence magnitude (1 cycle filter) is the filtered signal of Vpositive-sequence magnitude using aone-cycle sliding window filter. Its transient response is the slowest but at the sametime the smoothest among the three signals.

    Vdr filtered is the filtered signal of Vdr . The one cycle sliding window filter (alsocalled moving average) rejects all harmonics. Therefore there is no need to use theVds+ and Vqs+ calculator to extract the positive sequence. However its transientresponse is not as smooth as the Vpositive-sequence magnitude (1 cycle filter) one.

    Real Power Calculation Using dq Components

    As shown in Appendix A Parks transformation matrix is not unitary

    ( [ ] [ ] 1 dqot

    dqo TT ) and therefore is not power invariant.

    The total instantaneous power in abc quantities can be transformed into q-d-o

    quantities as shown in Equation 2-6.

    A B

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    21

    This relationship between dqo quantities and the instantaneous power is later used

    in the control system to determine the amount of direct-current component ( drI ) needed

    to meet the power fluctuation requirements.

    [ ] [ ]

    [ ] [ ][ ] [ ]

    [ ]

    ( )ooqrqrdrdr

    o

    qr

    dr

    oqrdr

    o

    qr

    dr

    dqo

    t

    dqooqrdr

    o

    qr

    dr

    dqo

    t

    o

    qr

    dr

    dqo

    c

    b

    a

    t

    c

    b

    a

    ccbbaaabc

    IVIVIV

    I

    I

    I

    VVV

    II

    I

    TTVVV

    I

    I

    I

    T

    V

    V

    V

    T

    I

    I

    I

    V

    V

    V

    IVIVIVP

    ++=

    =

    =

    =

    =++=

    3

    1

    2

    3

    3

    100

    02

    30

    002

    3

    11

    11

    (2-6)

    Phase Locked Loop

    The phase angle of the utility voltage () is of vital importance for the operation of

    most of the advanced power electronic devices connected to the electric utility, since it

    has a direct effect on their control algorithms.

    A simple and fast method to obtain the phase angle of the utility voltage is to use

    Clarkes transformation as shown in Equation 2-7.

    =

    =

    ds

    qs

    c

    b

    a

    qs

    ds

    X

    X

    X

    X

    X

    X

    Xarctan

    2

    3

    2

    30

    2

    1

    2

    11

    3

    2 (2-7)

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    22

    However, this approach is not robust since it is very sensitive to system

    disturbances. The phase angle distorts as the utilitys voltage becomes affected by

    different power quality events, such as voltage unbalance, voltage sags, frequency

    variations, etc.

    Figure 2-9 shows the voltages phase angle under unbalanced conditions using

    Equation 2-7. The angle distortion is due to the negative sequence component of the

    unbalanced three-phase system.

    Figure 2-9. Distortion of phase angle due to a negative sequence component

    In order to lock the phase angle of the utility voltage in a robust way, a phase

    locked loop (PLL) was used.

    Assuming a balanced three phase system, the control model of the PLL was

    obtained using Parks transformation as shown in Equation 2-8.

    =

    =

    =

    )240cos(

    )120cos(

    )cos(

    21

    21

    21

    )240sin()120sin()sin(

    )240cos()120cos()cos(

    3

    2

    21

    21

    21

    )240sin()120sin()sin(

    )240cos()120cos()cos(

    32

    ***

    ***

    ***

    ***

    wtV

    wtV

    wtV

    V

    V

    V

    V

    V

    V

    c

    b

    a

    o

    qr

    dr

    (2-8)

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    23

    Where * is the PLL phase angle output, is the utilitys phase angle, anddt

    dw = .

    Thus, if(t=0)=0, we can substitute wt for(t) and obtain

    =

    )240cos(

    )120cos()cos(

    21

    21

    21

    )240sin()120sin()sin()240cos()120cos()cos(

    3

    2 ***

    ***

    V

    VV

    V

    VV

    o

    qr

    dr

    (2-9)

    Using trigonometric identities, Equation 2-9 results in

    =

    =

    0

    )sin(

    )cos(

    0

    )sin(

    )cos(*

    *

    VV

    V

    V

    V

    o

    qr

    dr

    (2-10)

    Where is the error between the utility angle and the PLL output. If the is set to

    zero, Vdr=V and Vqr=0. Therefore, it is possible to lock the utility angle by regulating Vqr

    to zero without needing any information regarding the magnitude of the utility voltage.

    Figure 2-10 shows the details of the PLL algorithm used in our study. The limits of

    the controller integrator and the limiter were 30 rad/sec. Thus, the PLL was able to track

    the system frequency as long as this was within 26030 rad/sec or 55 to 65 Hz range.

    To use linear control techniques for the design and tuning of PLL controller, it was

    assumed that:

    For small values of, the term sin () behaved linearly, i.e., sin() . Wref was assumed to be a constant perturbation. Limiters behave linearly for small control actions, and therefore can be removed.

    abd

    dsq

    s

    Vds

    Vqs

    dsq

    s

    drq

    r

    Vdr

    Vqr

    Va

    Vb

    Vc

    Ki

    Kp +

    +

    30

    -30

    s

    1

    30

    -30

    +

    +

    Wref

    =2f

    s

    1

    Figure 2-10. PLL diagram

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    Figure 2-11 shows the PLL control loop after eliminating the non-lineal terms.

    Ki

    Kp +

    +

    s1

    s

    1

    -

    +

    PLL controller Plant transfer

    Function

    Control

    action

    Figure 2-11. PLL simplified model

    The closed loop transfer function ofFigure 2-11 determines the dynamic

    characteristics and stability of the system, and can be expressed as

    Ip

    Ip

    KsKsKsKH++

    +==2

    *

    (2-11)

    The control system (Kp and Ki) was designed to satisfy two performance

    objectives

    < 10% overshoot Settling time inside the 2% band error lower than 2 secs

    The criterion to select the settling time was a tradeoff between high distortion

    rejection and tracking of normal system frequency variations.

    The PLL closed loop transfer function was compared to a standard second order

    transfer function to determine the regulators gains. The obtained values were

    485.27.022

    1.827.0

    44

    sec2t

    )overshoot5%for(7.0

    22

    2

    s

    ===

    =

    =

    ==

    =

    =

    np

    s

    nI

    K

    tK

    Figure 2-12 shows the systems closed-loop step response for two different PI

    regulators.

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    25

    The originally designed regulator did not meet the system requirements due to the

    effect of the zero introduced by the PLL regulator. This additional zero increased the

    overshoot, but it had very little influence on the settling time. Thus, it was necessary to

    tune the original regulator gains in order to meet the system requirements.

    Figure 2-12. PLL system step response

    Figure 2-13 shows the root locus of the single-input single output PLL system for

    the two regulators.

    Figure 2-13. Root locus for two different regulator gains

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    26

    Figures 2-14 and 2-15 show the PLL system response to a negative sequence

    condition (V2=16.6%) and a system frequency excursion (w=260+30 rad/sec).

    Figure 2-14. PLL system response to an unbalanced system condition

    Figure 2-15. PLL system response to a frequency excursion. A) Angle. B) PLL error.

    Control Algorithm Design

    Parks transformation was used to model the systems equations to facilitate the

    design of the control system. The usage of a rotating reference frame had the following

    advantages:

    Improvement of the steady-state performance of the current controllers:Sinusoidal signals were transformed into dc components, and accordingly it ispossible to achieve small signal errors.

    High bandwidth current controllers: Feedback signals and reference signalswere not sinusoidal, but dc.

    A B

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    Decoupling of active and reactive power: This was very useful when trying tocontrol voltage at the point of coupling while meeting the system requirements interms of power fluctuations.

    Figure 2-16 shows the overall system topology as well as the sign notation that was

    used in the control system design. In general, power flowing out of the inverter will be

    considered to be positive. The objective was to smooth out wind-power fluctuations using

    the power stabilizer as a buffer. The energy-storage voltage was expected to change in

    order to accommodate for those changes in wind power.

    Iwind

    Vpcc

    Vf

    Iinv Vinv

    VdcVchopper Vstorage

    IchopperCdcLfLxfrm

    Cf

    WIND

    FARM

    UTILITY

    SYSTEM

    Xsource

    Transformer

    equivalent impedance

    Filter

    Inverter DC link bus Chopper

    ESS

    P + Figure 2-16. System description

    Inner regulators

    Inverter system model. For the following set of equations, it was assumed that the

    inverter behaved as an ideal controllable voltage source, neglecting the effects of the

    current harmonics. Systems non-linearities, such as saturation or dead-time effects were

    taken into consideration later on in the design.

    The capacitor filter was neglected in the analysis, since the filter current

    represented a small portion of the inverters current.

    The system can then be represented as shown in Figure 2-17.

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    Vpcc a R L Vinv a

    VDC LINKC

    Vpcc b R L Vinv b

    Vpcc c R L Vinv c

    Iinv a

    Iinv b

    Iinv c

    Figure 2-17. Simplified system model

    The system equations for the simplified model are

    +

    +

    =

    pcca

    pcca

    pcca

    invc

    invb

    inva

    invc

    invb

    inva

    invc

    invb

    inva

    V

    V

    V

    I

    I

    I

    dtdL

    I

    I

    I

    R

    V

    V

    V

    (2-12)

    Applying Parks transformation we get

    [ ] [ ] [ ] [ ]

    +

    +

    =

    opcc

    qrpcc

    drpcc

    dqo

    oinv

    qrinv

    drinv

    dqo

    oinv

    qrinv

    drinv

    dqo

    oinv

    qrinv

    drinv

    dqo

    V

    V

    V

    T

    I

    I

    I

    Tdt

    dL

    I

    I

    I

    TR

    V

    V

    V

    T1111 (2-13)

    [ ] [ ] [ ] [ ] [ ] [ ]

    +

    +

    =

    opcc

    qrpcc

    drpcc

    dqodqo

    oinv

    qrinv

    drinv

    dqodqo

    oinv

    qrinv

    drinv

    dqodqo

    oinv

    qrinv

    drinv

    V

    V

    V

    TT

    I

    I

    I

    Tdt

    dLT

    I

    I

    I

    TRT

    V

    V

    V111 (2-14)

    [ ][ ]

    [ ]

    +

    +

    +

    =

    opcc

    qrpcc

    drpcc

    oinv

    qrinv

    drinv

    dqo

    oinv

    qrinv

    drinv

    dqo

    dqo

    oinv

    qrinv

    drinv

    oinv

    qrinv

    drinv

    V

    V

    V

    I

    I

    I

    dt

    dT

    I

    I

    I

    dt

    TdTL

    I

    I

    I

    R

    V

    V

    V1

    1

    (2-15)

    [ ][ ]

    [ ] [ ]

    +

    +

    +

    =

    opcc

    qrpcc

    drpcc

    oinv

    qrinv

    drinv

    dqodqo

    oinv

    qrinv

    drinv

    dqo

    dqo

    oinv

    qrinv

    drinv

    oinv

    qrinv

    drinv

    V

    V

    V

    I

    I

    I

    dt

    dTTL

    I

    I

    I

    dt

    TdTL

    I

    I

    I

    R

    V

    V

    V1

    1

    (2-16)

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    [ ][ ]

    +

    +

    +

    =

    opcc

    qrpcc

    drpcc

    oinv

    qrinv

    drinv

    oinv

    qrinv

    drinv

    dqo

    dqo

    oinv

    qrinv

    drinv

    oinv

    qrinv

    drinv

    V

    V

    V

    I

    I

    I

    dt

    dL

    I

    I

    I

    dt

    TdTL

    I

    I

    I

    R

    V

    V

    V 1

    (2-17)

    Where

    [ ]

    dt

    d

    dt

    d

    dt

    d

    dt

    Td dqo

    =

    =

    =

    0)240cos()240sin(

    0)120cos()120sin(

    0)cos()sin(

    1)240sin()240cos(

    1)120sin()120cos(

    1)sin()cos(1

    (2-18)

    It can be shown that

    [ ] [ ]

    =

    =

    =

    =

    000

    00

    00

    000

    001

    010

    0)240cos()240sin(

    0)120cos()120sin(

    0)cos()sin(

    21

    21

    21

    )240sin()120sin()sin(

    )240cos()120cos()cos(

    3

    2 ***

    ***

    1

    dt

    TdT

    dqo

    dqo

    (2-19)

    Thus, the equations for the simplified model in the d-q plane are

    +

    +

    +

    =

    opcc

    qrpcc

    drpcc

    oinv

    qrinv

    drinv

    oinv

    qrinv

    drinv

    oinv

    qrinv

    drinv

    oinv

    qrinv

    drinv

    V

    V

    V

    I

    I

    I

    dt

    dL

    I

    I

    I

    L

    I

    I

    I

    R

    V

    V

    V

    000

    00

    00

    (2-20)

    The zero-sequence component can be removed, since the system is a three-phase

    three-wire inverter with the DC link bus isolated from the AC side (the DC link mid-

    point will not be tapped to neutral). Removing the zero sequence we obtain

    drinvqrpcc

    qrinv

    qrinvqrinv

    qrinvdrpcc

    drinv

    drinvdrinv

    ILVdt

    dILIRV

    ILVdt

    dILIRV

    +++=

    ++=

    (2-21)

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    Equation 2-21 can be represented as a coupled electrical system as shown in Figure

    2-18.

    R LV

    pcc drV

    inv dr

    Iinv dr

    LIinv qr

    R L

    Vpcc qr

    Vinv qr

    Iinv qr

    LIinv dr

    Figure 2-18. Electrical representation of the dq components. A) Direct circuit. B)Quadrature circuit.

    Using Laplaces transformation we can re-write the equations as Equation 2-22.

    ( )

    ( ) )()()()(

    )()()()(

    sILsVsILsRsV

    sILsVsILsRsV

    drinvqrpccqrinvqrinv

    qrinvdrpccdrinvdrinv

    +++=

    ++=

    (2-22)

    Thus, the block diagram of the system is represented in Figure 2-19.

    Vpcc dr

    Vinv dr

    Iinv dr

    LsR +

    1+

    -

    L

    L

    Vinv qr

    Iinv qr

    LsR +

    1+

    -

    Vpcc qr

    +

    -

    Figure 2-19. System model block diagram

    A

    B

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    The inverters critical control variable was the inverters current. This was due to

    the fact the outer control loops, such voltage regulators, power regulators, etc, were based

    on the inner current regulators. That was why the current controllers were designed to

    meet two basic requirements, which were high accuracy and high bandwidth.

    The inverters terminal-voltage needed to generate the desired inverter current can

    be determined as

    drinvqrpccdropdrinvqrpcc

    qrinv

    qrinvqrinv

    qrinvdrpccdropqrinvdrpcc

    drinv

    drinvdrinv

    ILVVILVdt

    dILIRV

    ILVVILVdt

    dILIRV

    qr

    dr

    ++=+++=

    +=++=

    (2-23)

    The voltage drop due to the filter inductance was compensated using a PI

    controller. Figure 2-20 shows the inveters current controller implementation for the

    system given in Equation 2-23.

    Vpcc dr

    Vinv dr

    Iinv dr

    LsR +

    1+

    -

    L

    L

    Vinv qr

    Iinv qr

    LsR +

    1+

    -

    Vpcc qr

    +

    -

    SYSTEM MODEL

    +

    -+

    Vdrop dr

    ++

    +

    Vdrop qr

    Ki

    Kp +

    +

    s1

    +

    -

    Ki

    Kp +

    +

    s

    1

    +

    -

    Iinv dr

    Iinv qr

    Iinv dr ref

    Iinv qr ref

    L

    L

    CURRENT REGULATORS

    drpccV

    qrpccV

    Figure 2-20. Inverter current regulator-system model block diagram

    The character ^ over a constant or variable indicates that the quantity is estimated,

    and therefore subject to measurement errors.

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    To design the current regulator gains, cross-coupling factors were assumed to

    cancel each other out. Under these conditions, the simplified current regulator block

    diagram is shown in Figure 2-21.

    Iinv dr

    LsR +

    1

    Iinv qr

    LsR +

    1

    SYSTEM MODEL

    Ki

    Kp +

    +

    s

    1

    +

    -

    Ki

    Kp +

    +

    s

    1

    +

    -

    Iinv dr

    Iinv qr

    Iinv dr ref

    Iinv qr ref

    CURRENT REGULATORS

    Figure 2-21. Inverter current regulator-system model simplified block diagram

    Figure 2-21 shows that:

    The system behaves linearly, and therefore linear control techniques can be used to

    determine the regulators gains. Both regulators are identical.

    Only an estimation of L and R (filter inductance + transformer equivalentimpedance) are needed to design the current regulator.

    Given the filter/transformer characteristics in p.u., the closed-loop transfer function

    ofFigure 2-22 is shown in Equation 2-24.

    Ki

    Kp +

    +

    s

    1

    +

    -

    Iref

    LsR +

    1 IControl Action

    Figure 2-22. Simplified current control diagram

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    ( )Ip

    Ip

    ref KsKRLs

    KsK

    I

    IsH

    +++

    +==

    2)( (2-24)

    Using the following system data, the transfer function is given in Equation 2-25.

    X=Xtransfomer+Xfilter=5%+10% = 0.15 L= 400 H X/R=10 R=0.015 Note: More on the system parameters can be found in the per-unit mode section.

    ( )Ip

    Ip

    KsKs

    KsKsH

    +++

    +=

    015.00004.0)(

    2(2-25)

    The Figure 2-23 shows the system step response for two different current regulator

    gains.

    Figure 2-23. Current regulator step response

    Even though the current regulator with the highest gains had a faster settling time,

    the control action required to obtain such a response doubled the regulator with the

    lowest gains. To avoid possible system saturations the control action was kept below 1

    pu.

    The best PI controller performance was achieved when the plants dominant pole

    was cancelled by the controller (Equation 2-26). Thus, the zero at -p

    I

    K

    K was assigned to

    the time constant of the plant, which was,L

    R

    K

    K

    p

    I = .

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    s

    K

    KsK

    s

    KKPI

    p

    Ip

    Ip

    +

    =+= (2-26)

    The synthesis was done by selecting the integral time constant of the PI equal tothat of the load. For our study the selected values were

    1

    5.37

    =

    ==

    p

    I

    K

    L

    RK

    Chopper system model. The analysis of the chopper system was less complex than

    the inverter one, since no transformations were involved. Again, it was assumed that the

    chopper behaved as an ideal controllable voltage source and therefore the effects of the

    current harmonics were neglected.

    Vchopper Vstorage

    Ichopper

    Figure 2-24. Chopper equivalent system

    The system equations for the chopper equivalent circuit (Figure 2-24) are given in

    Equaion 2-27.

    dt

    dILVV

    Vdt

    dILV

    chopper

    storagechopper

    chopper

    chopper

    storage

    =

    +=

    (2-27)

    The choppers terminals voltage needed to generate the desired chopper current

    can be determined as

    dropstoragechopper VVV = (2-28)

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    The voltage drop due to the chopper inductance was compensated using a simple P

    controller. The gain of the controller was found by converting the continuous system into

    discrete time system as shown in Equation 2-29.

    t

    LKIKVV

    dt

    IILV

    dt

    ILVV

    LchopperLstoragechopper

    chopperchopper

    storage

    chopper

    storagechopper

    ref

    ==

    =

    =

    where

    )(

    (2-29)

    Where KL is the regulators gain and t is half of the sampling time period.

    Figure 2-25 shows the implementation of the choppers current regulator.

    Ichopper

    +-

    KL

    Vstorage

    -+

    Ichopper ref

    Vchopper

    Figure 2-25. Chopper current controller

    Outer regulators

    There were a total ofthree controllable currents, which consisted of Ichopper_ref,

    Iinvdr_ref, and Iinvqr_ref.. However, there werefourvariables that needed to be controlled,

    which were voltage at the dc link bus, voltage at the point of common coupling, voltage

    at the energy storage system, and wind farm power fluctuation. Table 2-1 shows how

    these variables were assigned to the respective current regulators.

    Table 2-1. Outer regulator assignationInner current

    regulator

    Variable to be

    controlled CommentsIinv dr ref Vstorage, Pwind The direct current component will be responsible

    for controlling the state of charge of the ESSand for smoothing the wind farm output power

    Iinv qr ref Vpcc The quadrature current component will bedeployed for voltage regulation purposes

    Ichopper ref Vdc link The chopper current will regulate the DC link busvoltage.

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    DC link Voltage regulator. The DC link bus was the bridge between the energy

    storage system (chopper) and the inverter. Therefore, it was a critical variable in the

    overall system. Poor DC voltage regulation could bring the system down, since the

    inverter and chopper would not be able to meet their respective voltage requirements.

    The DC link system can be mode