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International Journal of Computer Applications (0975 8887) Volume 178 No.6, November 2017 21 Wind Energy System MVA Profile Enhancement based on Feedback Quadratic Function Controller Firas M. Tuaimah University of Baghdad College of Engineering Electrical Department ABSTRACT With the increase in the wind turbine power and size, its control system plays an important role to operate it in safe region and also to improve energy conversion efficiency and output power quality. In this paper a feedback quadratic function controller 1 for controlling a wind 1 energy 1 system is presented. A 1 nonlinear wind 1 energy system has been linearized and simulated using MATLAB programming language. An enhanced profile has been acquired for active and reactive power when adopting the feedback quadratic controller, through checking the settling time of the step response. Keywords Wind Energy, quadratic Function, and feedback controller. 1. INTRODUCTION Wind 1 energy 1 is the most 1 promising renewable 1 source 1 of electrical 1 power generation 1 for the 1 future. Many countries 1 promote 1 the wind 1 power technology 1 through various 1 national programs 1 and market 1 incentives. Wind 1 energy 1 technology has 1 evolved rapidly 1 over 1 the past three 1 decades with increasing 1 rotor 1 diameters and the 1 use of sophisticated 1 power 1 electronics to allow 1 operation at variable 1 speed [1]. Wind energy 1 can be harnessed 1 by a wind energy 1 conversion 1 system, composed 1 of wind turbine 1 blades, an electric 1 generator, a power 1 electronic 1 converter and the corresponding 1 control 1 system. There are different 1 WECS configurations 1 based 1 on using synchronous 1 or asynchronous 1 machines, and stall-regulated 1 or pitch regulated 1 systems. However, the functional 1 objective 1 of these 1 systems is the same: converting 1 the wind kinetic 1 energy into electric 1 power and injecting 1 this electric power 1 into 1 a utility 1 grid. [1] Proposed a nonlinear controller 1 for 1 a variable 1 speed 1 device to produce 1 electrical energy 1 on a power 1 network, based 1 on a doubly 1 - fed induction 1 generator (DFIG) 1 used in wind 11 energy 1 conversion 1 systems, two 1 types 1 of controllers: adaptive 1 fuzzy logic 1 and sliding 1 mode. Their 1 respective 1 performances 1 are compared 1 in terms of power 1 reference 1 tracking, response 1 to sudden speed 1 variations, 1 sensitivity 1 to perturbations 1 and robustness 1 against 1 machine parameters 1 variation. [2] proposed A new 1 method for obtaining 1 the maximum 1 power output 1 of a doubly 1 - fed 1 induction 1 generator (DFIG) wind turbine 1 to control 1 the rotor 1 and grid 1 - side 1 converter, a control 1 technique based 1 on the Lyapunov 1 function 1 are adopted, the 1 simulation results shows that 1 when the proposed 1 method is 1 used, the 1 wind turbine 1 is capable 1 of properly tracking 1 the optimal 1 operation 1 point. [3] Presented a complete 1 - order 1 modeling 1 of state 1 - space 1 representations 1 of synchronous 1 and induction generators 1 for wind 1 turbine 1 applications. Fully equivalent 1 models 1 with different 1 state 1 variables, suitable for 1 different control 1 schemes, 1 are 1 given. Simulation results of the 1 featured representations are assessed. [4]Presented the modeling of variable speed wind 1 turbines for stability studies, suitable control algorithms for 1 the simulation of the doubly-fed induction machine (DFIM) as 1 well as the permanent 1 magnet synchronous machine 1 (PMSM), The control schemes include the pitch-angle/speed 1 control and the decoupled 1 control of the real and reactive 1 power outputs. [5] Presented the Mathematical 1 modeling 1 of 1 synchronous 1 and induction 1 generators for 1 wind turbines 1 using 1 state 1 - space. Equivalent models 1 with 1 different state 1 variables, 1 suitable for 1 different control 1 schemes, are 1 given. The 1 performance 1 of fixed 1 and variable 1 - speed wind 1 turbines 1 under 1 faults 1 and voltage 1 sags 1 is assessed. [6] Presents 1 a new artificial 1 intelligence-based 1 detection 1 method of open 1 switch faults 1 in power converters 1 connecting 1 doubly-fed 1 induction (DFIG) 1 generator wind 1 turbine 1 systems to 1 the grid. In order to 1 improve the 1 performance 1 of the closed 1 - loop 1 system during 1 transients and 1 faulty conditions, current 1 control is based 1 on a PI 1 (proportional 1 - integral) controller optimized 1 using 1 genetic 1 algorithms. The 1 simulation model was developed in 1 Matlab/Simulink environment 1 and the simulation 1 results 1 demonstrate 1 the effectiveness 1 of the proposed 1 FTC method 1 and closed 1 - loop current control 1 scheme. [7] Presents 1 a distributed 1 model predictive 1 control 1 (DMPC) 1 based 1 on coordination 1 scheme. The proposed 1 algorithm solves a series 1 of local optimization 1 problems to minimize 1 a performance objective 1 for each control 1 area. The generation 1 rate constraints 1 (GRCs), load disturbance 1 changes, and the 1 wind speed 1 constraints are considered. Furthermore, the DMPC 1 algorithm may 1 reduce the impact 1 of the randomness 1 and intermittence 1 of wind turbine effectively. 1 A performance comparison 1 between the proposed 1 controller 1 with and without 1 the participation of the wind 1 turbines is carried out. 1 Analysis and simulation 1 results show 1 possible improvements 1 on closedloop 1 performance, and computational 1 burden with the 1 physical constraints. 1 2. THE PROPOSED WIND TURBINE SYSTEM The basic 1 components involved 1 in the representation 1 of a typical wind 1 turbine generator 1 are shown in Figure 1. 1

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Page 1: Wind Energy System MVA Profile Enhancement based on ...€¦ · Wind energy 1 can be harnessed 1 by a wind energy 1 conversion 1 system, composed 1 of wind turbine 1 blades, an electric

International Journal of Computer Applications (0975 – 8887)

Volume 178 – No.6, November 2017

21

Wind Energy System MVA Profile Enhancement based

on Feedback Quadratic Function Controller

Firas M. Tuaimah University of Baghdad College of Engineering Electrical Department

ABSTRACT

With the increase in the wind turbine power and size, its

control system plays an important role to operate it in safe

region and also to improve energy conversion efficiency and

output power quality. In this paper a feedback quadratic

function controller1 for controlling a wind1 energy1 system is

presented. A1 nonlinear wind1 energy system has been

linearized and simulated using MATLAB programming

language. An enhanced profile has been acquired for active

and reactive power when adopting the feedback quadratic

controller, through checking the settling time of the step

response.

Keywords

Wind Energy, quadratic Function, and feedback controller.

1. INTRODUCTION Wind1 energy1 is the most1 promising renewable1 source1 of

electrical1 power generation1 for the1 future. Many countries1

promote1 the wind1 power technology1through various1

national programs1 and market1 incentives. Wind1energy1

technology has1 evolved rapidly1 over1 the past three1 decades

with increasing1 rotor1 diameters and the1 use of

sophisticated1 power1 electronics to allow1 operation at

variable1 speed [1].

Wind energy1 can be harnessed1 by a wind energy1

conversion1 system, composed1 of wind turbine1 blades, an

electric1 generator, a power1 electronic1 converter and the

corresponding1 control1 system. There are different1 WECS

configurations1 based1 on using synchronous1 or

asynchronous1 machines, and stall-regulated1 or pitch

regulated1 systems. However, the functional1 objective1 of

these1 systems is the same: converting1 the wind kinetic1

energy into electric1 power and injecting1 this electric power1

into1 a utility1 grid.

[1] Proposed a nonlinear controller1 for1 a variable1 speed1

device to produce1 electrical energy1 on a power1 network,

based1 on a doubly1- fed induction1 generator (DFIG) 1 used in

wind11 energy1 conversion1 systems, two1 types1 of

controllers: adaptive1 fuzzy logic1 and sliding1 mode. Their1

respective1 performances1 are compared1 in terms of power1

reference1 tracking, response1 to sudden speed1 variations,

1sensitivity1 to perturbations1 and robustness1 against1

machine parameters1 variation.

[2] proposed A new1 method for obtaining1 the maximum1

power output1 of a doubly1- fed1 induction1 generator (DFIG)

wind turbine1 to control1 the rotor1and grid1- side1 converter, a

control1 technique based1 on the Lyapunov1 function1 are

adopted, the1 simulation results shows that1 when the

proposed1 method is1 used, the1 wind turbine1 is capable1 of

properly tracking1 the optimal1 operation1 point.

[3] Presented a complete1- order1 modeling1 of state1- space1

representations1 of synchronous1 and induction generators1 for

wind1 turbine1 applications. Fully equivalent1 models1 with

different1 state1 variables, suitable for1 different control1

schemes, 1 are1 given. Simulation results of the1 featured

representations are assessed.

[4]Presented the modeling of variable speed wind1 turbines

for stability studies, suitable control algorithms for1 the

simulation of the doubly-fed induction machine (DFIM) as1

well as the permanent1 magnet synchronous machine1

(PMSM), The control schemes include the pitch-angle/speed1

control and the decoupled1 control of the real and reactive1

power outputs.

[5] Presented the Mathematical1 modeling1 of1 synchronous1

and induction1 generators for 1wind turbines1 using1 state1-

space. Equivalent models1 with1 different state1 variables, 1

suitable for1 different control1 schemes, are1 given. The1

performance1 of fixed1 and variable1- speed wind1 turbines1

under1 faults1 and voltage1 sags1 is assessed.

[6] Presents1 a new artificial1 intelligence-based1 detection1

method of open1 switch faults1 in power converters1

connecting1 doubly-fed1 induction (DFIG) 1 generator wind1

turbine1 systems to1the grid. In order to1improve the1

performance1of the closed1- loop1 system during1transients

and1 faulty conditions, current1control is based1on a PI1

(proportional1- integral) controller optimized1using1genetic1

algorithms. The1simulation model was developed in1

Matlab/Simulink environment1 and the simulation1results1

demonstrate1the effectiveness1of the proposed1FTC method1

and closed1- loop current control1 scheme.

[7] Presents1 a distributed1 model predictive1control1(DMPC)

1based1on coordination1scheme. The proposed1algorithm

solves a series1of local optimization1problems to minimize1a

performance objective1for each control1area. The

generation1rate constraints1(GRCs), load disturbance1changes,

and the1wind speed1constraints are considered. Furthermore,

the DMPC1algorithm may1reduce the impact1of the

randomness1and intermittence1of wind turbine effectively. 1A

performance comparison1between the

proposed1controller1with and without1the participation of the

wind1turbines is carried out. 1Analysis and simulation1results

show1possible improvements1on closed–loop1performance,

and computational1burden with the1physical constraints. 1

2. THE PROPOSED WIND TURBINE

SYSTEM The basic1components involved1in the representation1of a

typical wind1turbine generator1are shown in Figure 1. 1

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International Journal of Computer Applications (0975 – 8887)

Volume 178 – No.6, November 2017

22

Fig 1: 1Schematic1diagram of the wind1turbine system

The figure shows1model blocks for1wind speed, the1

aerodynamic1wind1 turbine, mechanical1components,

electrical1 generator, 1matrix converter, and utility1grid. The1

system1may also contain1some mechanical parts for blades1

angle control.

MC interfaces the1 induction generator with1 the grid and1

implements1 a shaft1 speed control methods1to achieve1

maximum1 power-point1 tracking at varying1wind velocities.

It1 also performs1power factor1control at the1grid interface

and1 satisfies1the Var demand1 at the induction1 generator1

terminals. 1[8]

2.1 Common Generator1Types in

Wind1Turbines The1function of an1electrical generator1is providing a1

means1for energy conversion1between the mechanical1torque1

from1the wind rotor1turbine, as the1prime mover, and1the

local1 load1or the electric1grid. Different1types of generators1

are being1used with wind1turbines. Small wind1turbines are1

equipped with1DC generators of up1to a few kilowatts1in

capacity. Modern1wind turbine systems1use three phase1AC

generators [8 and 9]. The common types1of AC generator1that

are1 possible candidates1in modern wind1turbine systems

are1as1follows:

Squirrel1- Cage1(SC) rotor Induction1Generator1

(IG),

Wound1- Rotor (WR) 1Induction Generator, 1

Doubly1- Fed Induction1Generator (DFIG), 1

Synchronous1Generator (With external1field

excitation), 1and

Permanent1Magnet (PM) 1Synchronous Generator1

2.2 Matrix1Converter (MC) 1 Matrix converter1(MC) is a one1- stage AC/AC1converter that

is1composed of an1array of nine1bidirectional

semiconductor1switches, connecting1each phase of the1input

to each1phase of the1output. This1structure is shown1in Figure

2. 1The basic1idea behind matrix1converter is that1a desired

output1 frequency, 1output voltage1and input displacement1

angle1can be obtained by1properly operating the

switches1that1 connect1the output1 terminals1of the

converter1to its input1 terminals. 1In this method, 1known as

direct1method, the1output1voltages are obtained1 from

multiplication1of the1modulation1 transfer matrix by1input

voltages. 1Since then, the1research on1 the MC1has

concentrated1 on implementation1of bidirectional1 switches,

1as well as1modulation techniques. 1

Fig 2: Matrix converter structure

One of practical1 problems in the implementation of MC is

the1 use of four-quadrant bidirectional switches. Using this

type of1 switch1 is necessary for successful1 operation of MC

[8].

3. CONTROL METHODS With the evolution1of WECS during1the last1 decade, 1many

different1control methods have1been developed. 1The control

methods1developed for WECS1are usually1 divided into1the

following1two major1categories:

Constant1- speed methods, 1and

Variable1- speed methods. 1

3.1 Variable1- Speed turbine1Versus

Constant-Speed1 Turbine In constant1- speed turbines, 1there is no1control on

the turbine1shaft speed. Constant1speed control is1an easy and

low1- cost method, but1variable speed brings1the following

advantages: 1

Maximum power1tracking for harnessing1the

highest possible1energy from the1wind,

Lower mechanical1stress,

Less variations1in electrical1power, and1

Reduced1acoustical noise1at lower wind1speeds.

4. DYNAMIC MODEL OF THE WIND

TURBINE SYSTEM The components of the wind turbine1system, shown in1 Figure

3 below, will be modeled by thirteen nonlinear1 equations

(excluding the wind model): three, equations for the1 wind

turbine and shafts; six for the MC in balanced1three-phase

operation; and four, 1for the induction1machine. Using1 these

equations, a complete dynamic model of the wind1 turbine

will be developed in this section. In the proposed1 system of

Figure 1, the input and output sub-circuits of the1 MC are

connected1to the1electrical grid1and the stator1 terminals of

the induction generator, respectively. Therefore, the following

equations can be written for the voltages, 1 currents and

frequency of the MC, as well as the induction generator

terminal voltages [8]:

Fig 3: block diagram of wind turbine system model

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International Journal of Computer Applications (0975 – 8887)

Volume 178 – No.6, November 2017

23

Generator terminal voltages:

Generator terminal currents:

Generator synchronous frequency and MC input frequency:

ωo = ωe , ωi = ωGrid (3)

MC input sub-circuit terminal voltages:

The generator terminal voltages, vqs and vds, should be stated

in terms of state variables and inputs variables. Note that, for

the overall system, the grid voltage, vqG and vdG, are the input

variables.

The generator voltage can be written as follows:

The generator terminal voltages can be expressed as

a function of the system state variables, as follows:

Next, using equations (7) and (8), the stator flux linkage

equations, can be presented as a function of system state

variables, as follows:

Where,

Finally, by combining the state-equation of the

mechanical1shaft, electrical generator, 1and the MC, the

overall1model of the system1can be described1by the

following eleven nonlinear1equations.

The power exchanged between grid and the wind turbine is an

important quantity of the wind1turbine system. Therefore,

the1grid active and reactive1powers injected1into the grid1are

chosen as1the output variables1for the model. 1

Where VGm is the peak value of the grid phase voltage.

The schematic diagram of the wind turbine system’s overall

dynamic model is shown in Figure 4. The model is

characterized1by six inputs (u), 1two outputs (y), 1and eleven

state variables (x). Out of the six inputs, ωe, q, a, and αo are

adjustable1control1variables of the MC, β is pitch angle1of the

turbine1blades, 1and VW is the wind1velocity. The active1and

reactive1powers injected1into the grid1are treated1as

output1variables for the1model.

Fig 4: Inputs, state variables and outputs of the overall

dynamic model of wind turbine system

5. LINEARIZED MODEL OF THE

WIND TURBINE SYSTEM The nonlinear state-space model of the wind turbine system

contains eleven nonlinear equations. The sources of

nonlinearity are the turbine torque equation, induction

machine equations, and the MC equation. The small-signal

model is developed by linearizing the eleven nonlinear

equations around an operating point. The linearized model, is

described by the following state-space equations:

Where,

]T

T ,and T

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International Journal of Computer Applications (0975 – 8887)

Volume 178 – No.6, November 2017

24

In equation (24), A, 1B, 1C, and D1are the Jacobian1matrices,

1calculated at the operating point. This linearization results in

the matrices A, B, C, and D as follows:

Where,

6. OUTPUT EQUATIONS OF THE

SMALL-SIGNAL MODEL The output of small-signal model contains the grid real and

reactive powers, i.e., ∆PGrid and ∆QGrid that can be derived

based on the nonlinear equations (22) and (23), as follows:

7. FEEDBACK QUADRATIC

FUNCTION CONTROLLER The theory1of optimal control is1concerned with

operating1a dynamic system1at minimum1cost. The case

where1the system dynamics1are described by a set1of linear

differential1equations and the cost1is described1by

a quadratic1function is called1the QR problem. 1One of

the1main results1in the theory1is that the1solution is

provided1by the linear1– quadratic regulator, 1a feedback

controller whose shown in Figure 5.

The QR algorithm1is essentially an automated1way of

finding1an appropriate state1- feedback controller. 1As such,

it1is not uncommon1for control engineers1to prefer alternative

methods, 1like full state1feedback, also known1as pole

placement, 1in which there is1a clearer relationship1between

controller1parameters and controller1behavior. Difficulty1in

finding1the right weighting1factors limits the1application of

the1 QR based1controller1synthesis.

The schematic1of this type of control1system is shown

below1where is a matrix of control1gains. Note that here

the feedback1for all of the system's states will be done, 1rather

than using1the system's outputs1for feedback. [10]

Fig 5: Normalized Feedback Quadratic Structure

Design an QR control law Kxu which solves the

following Problem,

BuAxx

dtRuQxxJ TRQux

0

2),,,( )( , 0Q , 0R (27)

i.e., compute

01 QPBPBRPAPA TT , (28)

0P , PBRK T1 8. RESULTS To verify the stability it is important to check the eigenvalues

of the linearized system. When the real parts of all

eigenvalues of the linearized system are negative, the

nonlinear system is locally stable around the steady-state

operating point. The eigenvalues of the small-signal model

linearized around the operating point are shown in Table 1.

The real parts of all eigenvalues are negative; therefore, the

linearized small signal model is asymptotically stable at the

steady-state operating point.

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International Journal of Computer Applications (0975 – 8887)

Volume 178 – No.6, November 2017

25

Table 1 Eigen Values

-12.205 ± 32.232i -25.237 -28.126 ± 140.2i -49.646 ± 32400i -49.764 ± 31574i -50.91± 372.8i

Next, to calculate the maximal and minimal singular values at

the (arbitrary) frequency ω= 10 rad/s for the two studied

cases, namely the closed loop feedback system with unity

controller and the feedback linear quadratic regulator

controller. The plot shows us that the maximal and minimal

singular values are very close to each other at the crossover

frequency when using feedback regulator controller, as shown

in Figure 6.

Fig 6: Singular Values

That tells the designer for the good parameters choice for the

proposed linear quadratic regulator controller, and thats

because the controlled system shows an ’almost SISO’

behavior at the crossover frequency. Figures (7-15) shows the

active and reactive power changes of the wind turbine system

to changes in output frequency, displacement power factor,

voltage angle, wind velocity and pitch angle respectively.

Table 2 and Table 3 shows the comparison between the

settling time for the application of the unity feedback

controller and Feedback regulator controller.

Fig 7: Step Response1of the Grid Active1Power with

Output Frequency Change

Fig 8: Step Response of the Grid Active Power with

Displacement Power Factor Change

Fig 9: Step Response1of the Grid Active1Power with

Voltage Angle Change

Fig110: Step Response1of the Grid1Active Power1with

Wind Velocity Change

Fig 11: Step Response of the Grid Active Power with Pitch

Angle Change

Fig 12: Step Response1of the Grid Reactive1Power with

Output Frequency Change

Fig 13: Step Response1of the Grid Reactive1Power with

Displacement Power Factor Change

Fig 14: Step Response of the Grid Reactive Power with

Voltage Angle Change

Singular Values

Frequency (rad/s)

Sin

gu

lar

Valu

es (

dB

)

100

101

102

103

104

105

106

107

70

80

90

100

110

120

130

140

150

160

170

System: Closed Loop

Peak gain (dB): 163

At frequency (rad/s): 3.16e+04

System: LQR Controller

Peak gain (dB): 112

At frequency (rad/s): 3.61e+04

Closed Loop

LQR Controller

Step Response of the Grid Active Power with Output Frequency Change

Time (seconds)

Pg

rid

(Watt

)

0 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4-1

-0.5

0

0.5

1

1.5

2

2.5

3x 10

4

System: LQR Controller

Peak amplitude: 2.5e+04

Overshoot (%): 4.03e+03

At time (seconds): 0.0305

System: Closed Loop

Peak amplitude: 2.43e+04

Overshoot (%): 7.24e+03

At time (seconds): 0.036

System: LQR Controller

Settling time (seconds): 0.26

System: Closed Loop

Settling time (seconds): 0.355

Closed Loop

LQR Controller

Step Response of the Grid Active Power with Displacement Power Factor change

Time (seconds)

Pg

rid

(Watt

)

0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2-2.5

-2

-1.5

-1

-0.5

0

0.5

1

1.5

2

2.5x 10

5

System: Closed Loop

Peak amplitude: 2.21e+05

Overshoot (%): 2.94e+05

At time (seconds): 0.00373

System: LQR Controller

Peak amplitude: 1.23e+04

Overshoot (%): 1.36e+03

At time (seconds): 0.00379 System: Closed Loop

Settling time (seconds): 0.0892

System: LQR Controller

Settling time (seconds): 0.211

Closed Loop

LQR Controller

Step Response of the Grid Active Power with Voltage Angle Change

Time (seconds)

Pg

rid

(Watt

)

0 0.05 0.1 0.15 0.2 0.25 0.3-4

-2

0

2

4

6

8

10

12

14

16x 10

5

System: Closed Loop

Peak amplitude: 1.44e+06

Overshoot (%): 1.44e+03

At time (seconds): 0.00919

System: LQR Controller

Peak amplitude: -3.69e+04

Overshoot (%): 117

At time (seconds): 0.0684

System: LQR Controller

Settling time (seconds): 0.211

System: Closed Loop

Settling time (seconds): 0.284

Closed Loop

LQR Controller

Step Response of the Grid Active Power with Wind Velocity Change

Time (seconds)

Pg

rid

(Watt

)

0 0.05 0.1 0.15 0.2 0.25 0.3-3

-2.5

-2

-1.5

-1

-0.5

0x 10

4

System: LQR Controller

Settling time (seconds): 0.228

System: Closed Loop

Settling time (seconds): 0.319

System: LQR Controller

Peak amplitude: -2.67e+04

Overshoot (%): 24.6

At time (seconds): 0.091

System: Closed Loop

Peak amplitude: -2.8e+04

Overshoot (%): 32.5

At time (seconds): 0.0945

Closed Loop

LQR Controller

Step Response of the Grid Active Power with Pitch Angle Change

Time (seconds)

Pg

rid

(Watt

)

0 0.05 0.1 0.15 0.2 0.25 0.30

1000

2000

3000

4000

5000

6000

7000

System: Closed Loop

Peak amplitude: 6.51e+03

Overshoot (%): 32.5

At time (seconds): 0.0945

System: LQR Controller

Peak amplitude: 6.22e+03

Overshoot (%): 24.6

At time (seconds): 0.091System: LQR Controller

Settling time (seconds): 0.228

System: Closed Loop

Settling time (seconds): 0.319

Closed Loop

LQR Controller

Step Response of the Grid Reactive Power with Output Frequency Change

Time (seconds)

Qg

rid

(Var)

0 0.05 0.1 0.15 0.2 0.25 0.3 0.35-3000

-2000

-1000

0

1000

2000

3000

4000

5000

6000

System: LQR Controller

Settling time (seconds): 0.169

System: Closed Loop

Settling time (seconds): 0.353

Closed Loop

LQR Controller

Step Response of the Grid Reactive Power with Displacement Power Factor Change

Time (seconds)

Qg

rid

(Var)

0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09-5

-4

-3

-2

-1

0

1

2x 10

5

System: LQR Controller

Settling time (seconds): 0.00192

System: Closed Loop

Settling time (seconds): 0.077

Closed Loop

LQR Controller

Step Response of the Grid Reactive Power with Voltage Angle Change

Time (seconds)

Qg

rid

(Var)

0 0.02 0.04 0.06 0.08 0.1 0.12-4

-2

0

2

4

6

8

10x 10

5

System: LQR Controller

Settling time (seconds): 0.0787

System: Closed Loop

Settling time (seconds): 0.115

Closed Loop

LQR Controller

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International Journal of Computer Applications (0975 – 8887)

Volume 178 – No.6, November 2017

26

Fig 15: Step Response1of the Grid1Reactive Power with

Wind Velocity Change

Fig 16: Step1Response1of the Grid Reactive1Power with

Pitch Angle Change

Table.2 Grid Active Power (PGrid) Settling Time Response

Change Settling Time

for Closed

Loop, sec

Settling Time

for Regulator

Feedback, sec

Output Frequency 0.355 0.26

Displacement Power Factor 0.0892 0.211

Voltage Angle 0.284 0.211

Wind Velocity 0.319 0.228

Pitch Angle 0.319 0.228

Table.3 Grid Reactive Power (QGrid) Settling Time

Response Change Settling Time

for Closed

Loop, sec

Settling Time

for Regulator

Feedback, sec

Output Frequency 0.353 0.169

Displacement Power Factor 0.077 0.00192

Voltage Angle 0.115 0.0787

Wind Velocity 0.323 0.225

Pitch Angle 0.323 0.225

9. CONCLUSION In this paper, the investigation of the apparent power (MVA)

profile resulting from connecting the wind energy system on

the power grid, in which the effect of changing number of

inputs, namely output frequency, displacement power factor,

voltage angle, wind velocity and pitch angle respectively, has

been studied.

As shown in figures from (7-16), Table 2 and Table 3, that

there is an enhancement in the step response profiles for the

MVA profile (i.e. the MW and MVAR) resulting from the

change in the pre mentioned inputs, when using feedback

regulator controller.

Parameters of the system under study[11]

Induction Generator

500[hp], 2.3[kV], 1773[rpm], TB=1.98×103 [N.m],

IB(abc)=93.6[A], rs=0.262, rr=0.187 [Ω], Xls=1.206, Xlr=1.206,

XM=54.02 [Ω], J=11.06[Kg.m2], P=4[Poles],

Pmech_loss=1%Prated

Wind Turbine System

JT=100 [kg.m2], Ks=2×106 [Nm/rad], B=5×103 [Nm/rad/s]

ngear=20, ρair =1.25[kg/m3 ], R=10 [m]

Matrix Converter

Ri=Ro=0.1[Ω], Li=Lo=1 [mH], C=0.1[mF], 0≤q≤0.87, 0≤a≤1

Grid(Infinite Bus)

VG=4[kV], fG=60[Hz]

10. REFERENCES [1] Z. Boudjema, A. Meroufel and Y. Djerriri, "Nonlinear

control of a doubly fed induction generator for wind

energy conversion", Carpathian Journal of Electronic and

Computer Engineering, 6/1, 28-35, 2013.

[2] Dinh-Chung Phan and Shigeru Yamamoto," Maximum

Energy Output of a DFIG Wind Turbine Using an

Improved MPPT-Curve Method", Energies, 8, pp.

11718-11736, 2015.

[3] Carlos E. Ugalde-Loo and Janaka B. Ekanayake, " State-

Space Modelling of Variable-Speed Wind Turbines: A

Systematic Approach", IEEE ICSET 2010 6-9 Dec 2010,

Kandy, Sri Lanka.

[4] Istvan Erlich, Fekadu Shewarega and Oliver Scheufeld, "

Modeling Wind Turbines in the Simulation of Power

System Dynamics", Scientific Journal of Riga Technical

University, Volume 27, pp.41-47, 2010.

[5] Carlos E. Ugalde-Loo , Janaka B. Ekanayake and

Nicholas Jenkins, "State-Space Modelling of Variable-

Speed Wind Turbines for Power System Studies ", IEEE

Transactions on Industry Applications, January 2013.

[6] Amina Bouzekri , Tayeb Allaoui, Mouloud Denai and

Youcef Mihoub, "Artificial Intelligence-Based Fault

Tolerant Control Strategy in Wind Turbine Systems",

International Journal of Renewable Energy Research A.

Bouzekri, Vol.7, No.2, 2017.

[7] Yi Zhang, Xiangjie Liu, and Bin Qu"Distributed Model

Predictive Load Frequency Control of Multi-area Power

System with DFIGs", IEEE/CAA Journal of Automatica

Sinica, Vol. 4, No. 1, January 2017

[8] S. Masoud Barakati, " Modeling and Controller Design

of a Wind Energy Conversion System Including a Matrix

Converter", Ph.D. thesis, Waterloo, Ontario, Canada,

2008

[9] Bijaya Pokharel, “Modeling, Control and Analysis of a

Doubly Fed Induction Generator Based Wind Turbine

System with Voltage Regulation", M.Sc. Thesis at

Tennessee Technological University, December 2011.

[10] F.L.Lewis: Control System Design Project; lecture 11,

1999.

[11] P. C. Krause, O Wasynczuk , S. D. Sudhoff, Analysis of

electric machinery, IEEE Press, 1994.

Step Response of the Grid Reactive Power with Wind Velocity change

Time (seconds)

Qg

rid

(Var)

0 0.05 0.1 0.15 0.2 0.25 0.3 0.35-3000

-2500

-2000

-1500

-1000

-500

0

System: LQR Controller

Settling time (seconds): 0.225

System: Closed Loop

Settling time (seconds): 0.323System: LQR Controller

Peak amplitude: -1.5e+03

Overshoot (%): 33.6

At time (seconds): 0.084

System: Closed Loop

Peak amplitude: -2.74e+03

Overshoot (%): 56.5

At time (seconds): 0.0875

Closed Loop

LQR Controller

Step Response of the Grid Reactive Power with Pitch Angle Change

Time (seconds)

Qg

rid

(Var)

0 0.05 0.1 0.15 0.2 0.25 0.3 0.350

100

200

300

400

500

600

700

System: Closed Loop

Settling time (seconds): 0.323

System: LQR Controller

Settling time (seconds): 0.225

System: Closed Loop

Peak amplitude: 638

Overshoot (%): 56.5

At time (seconds): 0.0875

System: LQR Controller

Peak amplitude: 348

Overshoot (%): 33.6

At time (seconds): 0.084

Closed Loop

LQR Controller

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