International Journal of Electrical and Computer Engineering (IJECE) Vol.
No.
June 2016, pp.
ISSN: 2088-8708.
DOI: 10.
11591/ijece.
Tip Speed Ratio Based MPPT Algorithm and Improved Field Oriented Control for Extracting Optimal Real Power and Independent Reactive Power Control for Grid Connected Doubly Fed Induction Generator Ananth1.
Nagesh Kumar2 Department of e.
Viswanadha Institute of Technology and Management.
Visakhapatnam,531173.
India Department of e.
GITAM University.
Visakhapatnam, 530045.
Andhra Pradesh.
India
Article Info
ABSTRACT
Article history:
Doubly Fed Induction Generator (DFIG) needs to get adopted to change in wind speeds with sudden change in reactive power or grid terminal voltage as it is required for maintaining synchronism and stability as per modern grid This paper proposes a controller for DFIG converters and optimal tip speed ratio based maximum power point tracking (MPPT) for turbine to maintain equilibrium in rotor speed, generator torque, and stator and rotor voltages and also to meet desired reference real power during the turbulences like sudden change in reactive power or voltage with concurrently changing wind speed.
The performance of DFIG is compared when there is change in wind speed only, changes in reactive power and variation in grid voltage along with variation in wind speed.
Received Jan 7, 2016 Revised May 1, 2016 Accepted May 16, 2016 Keyword:
Doubly fed induction generator Optimal tip speed ratio Mmaximum power point Real and reactive power control Grid side converter Wind energy conversion system Copyright A 2016 Institute of Advanced Engineering and Science.
All rights reserved.
Corresponding Author:
Nagesh Kumar.
Departement of e.
GITAM University.
Visakhapatnam, 530045.
Andhra Pradesh.
India.
Email: drgvnk14@gmail.
INTRODUCTION
The wind and solar electric power generation systems are popular renewable energy resources and are getting significance due to retreating of primary fuels and because of eco-friendly nature and is available from few kilo-watt power to megawatt rating.
The extractable maximum power from wind depends mostly on the pitch angle control of the wind turbine system and operating rotor at optimal speed for DFIG.
The maximum power point tracking (MPPT) of wind turbine generator system is for techno-economic benefits.
As per literature, four control techniques are used for extracting maximum real power from wind.
The strategies are perturbation and observation (P&O) control, tip speed ratio (TSR) control, optimal torque control (OTC) and Power signal feedback (PSF) control .
Ae.
with their description in .
The P&O or hill-climb searching (HCS) method generally requires details on rotor speed and variation of wind turbine power for extracting optimal power.
This method does not oblige on characteristic curve of wind turbine or parameters of generator .
However, for large-inertia wind turbine systems this method goes out of step with rapid variation in wind speed and produces oscillations near the peak points of maximum power locus point.
In TSR method, with variations in wind speed, the wind turbine rotational speed will also varied to achieve the optimal TSR .
However, an accurate and continuous wind turbine shaft speed and wind speed measurement is required, which in real time is very difficult.
In OTC, the control of generator Journal homepage: http://iaesjournal.
com/online/index.
php/IJECE A ISSN: 2088-8708 torque is done to meet its optimal value to get maximum value of coefficient of power .
This method is slower in performance due to slow calculation of wind speed and retrieving data processes by anemometer.
The performance of DFIG wind energy conversion system is compared with PI.
ANN and hybrid PI and ANN in .
A comparison is made with power transfer matrix and Direct Power Control (DPC).
The authors found that compared to DPC, power transfer matrix is having better control over real power generation, faster control action, stable.
The performance of DFIG is studied in .
with the operation of rotor speed adjusting to sub-synchronous and super-synchronous speed.
Also independent control of active and reactive power examined in this paper and found that fuzzy controller is better than conventional PI The fuzzy controller is having faster control action and accurate performance due to faster changing disturbances.
A hybrid PI and ANN controller for DFIG is examined in .
to rapidly changing grid voltage conditions.
The authors found that, active and reactive powers are having surges and also rotor and stator parameters got disturbed much with PI and their effects are low with ANN.
However when using both Pi and ANN, the effects said above got minimized and hence the authors in .
conclude that hybrid is better control when grid voltage conditions are high.
In .
, authors compared the performance of DFIG during three phase to ground when controlled using PI and fuzzy.
It is found that with fuzzy, stator and rotor voltage, current and power waveforms are better and have better stability than a conventional PI controller.
Predictive direct power control technique is applied to DFIG system in .
to have quicker and robust performance to maintain constant DC link voltage with lesser harmonic current and for operation during sub synchronous and super- synchronous speed operation.
Drooping characteristics of DFIG is studied in .
and found that DFIG output power is controlled according to varying wind speed.
In this paper, performance of DFIG was compared and analyzed under situations like, .
with variation in wind speed alone, .
with reactive power variation and .
with grid voltage variation for same variation in wind speed.
In these cases, variation in tip speed ratio and coefficient of turbine power, effect on real and reactive power flows, voltages and current from stator and rotor, rotor speed and electromagnetic torque are examined.
The paper was organized as follows: overview of WECS with wind turbine modeling and pitch angle controller in section II.
study of mathematical modelling of DFIG in section i, the section IV deals with RSC architecture and design.
section V analyses the performance of DFIG for two cases like effect of variation on .
reactive power demand along with variation in wind speed and i.
grid voltage variation with wind speed.
Conclusion was given in Section VI followed by appendix and references.
WIND ENERGY CONVERSION SYSTEM (WECS)
In this study, the WECS is designed using DFIG connected with the stator connected directly to grid and the rotor via a back-to-back PWM-VSC as shown in Figure 1.
The control of the system has been done through the rotor side converter (RSC) and the grid side converter (GSC).
The MPPT algorithm has been achieved through controlling the turbine shaft blade angle to optimal tip speed, the RSC controls the rotor to rotate and optimal speed.
The GSC maintains the DC-link voltage at the reference value by transferring active power to the grid and controls the exchange of reactive power with the grid.
Figure 1.
Single line diagram of grid connected DFIG The wind turbine modelling The wind turbine is the prime mover which facilitates in converting kinetic energy of wind into mechanical energy which further converted into electrical energy.
From basic theory of wind energy conversion, the output mechanical power from turbine is given by IJECE Vol.
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= Cp(, ) A 1321 Where is the mechanical power output from wind turbine.
Cp is coefficient of wind power as a function of pitch angle () and tip speed ratio ( A is specific density of air, r is radius of wind turbine blade, is wind speed.
Cp(, ) = 0.
- 0.
4 - .
radius of turbine blades and wind speed The tip sped ratio is a relation between turbine speed ( and tip speed ratio at particular angle AoiAo is given the relation as shown below the output power at nominal wind speed is given by the below equation .
Where Psh is the turbine shaft power and Cp max is maximum mechanical power coefficient.
The maximum power from wind turbine can be extracted by using the equation AA Pitch angle controller The wind turbine blade angles are controlled by using servo mechanism to maximize turbine output mechanical power during steady state and to protect the turbine during high wind speeds.
This control mechanism is known as pitch angle controller.
When wind speed is at cut-in speed, the blade pitch angle is set to produce optimal power, at rated wind speed.
it is set to produce rated output power from generator.
At higher wind speeds, this angle increases and makes the turbine to protect from overspeeding.
The pitch angle controller circuit is as shown in Figure 2a.
Figure 2a.
Pitch angle controller design for wind turbine Tip Speed Ratio Based MPPT Algorithm and Improved Field Oriented Control for .
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MPPT algorithm for wind turbine to develop optimal rotor speed estimation In this system reference generator speed is 2pu and actual speed of the generator is Wr.
the similar way, the difference in reference (P*=.
and actual power outputs from turbine (PT) is controlled by PI controller.
Both the outputs from PI controller are designed to get reference pitch angle controller .
The closed loop control of pitch angle is obtained as shown in Figure 2a.
The optimal speed estimation .
pd_ref or WR) is shown in Figure 2b.
Using Tip Speed Ratio (TSR), wind speed.
Coefficient of Power (CP) and mechanical power output from turbine are used as main inputs to generate reference rotor The control scheme is useful to extract maximum mechanical power, thereby more mechanical torque (T.
by using the optimal tip speed ratio based MPPT algorithm.
Figure 3.
Equivalent circuit of DFIG in rotating reference frame at speed O Mathematical modeling of DFIG The equivalent circuit of DFIG in rotating reference frame at an arbitrary reference speed of O is shown in Figure 3.
The stator direct and quadrature axis .
voltages of DFIG can be written as .
The rotor direct and quadrature axis are derives as .
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and rotor speed is known as slip speed For The difference between stator speed motoring action, this difference is less than zero and for generating, the slip speed is negative.
The stator and rotor flux linkages in axis frame are given below
IJECE
The stator real power in terms of two axis voltage and current is = ( .
The rotor real power in terms of two axis voltage and current is = ( .
The stator reactive power in terms of two axis voltage and current is = ( .
The rotor reactive power in terms of two axis voltage and current is = ( .
The quadrature and direct axis rotor current in terms of stator parameters can be written as .
The output electromagnetic torque is given by the equation .
The mechanical torque output from the turbine in terms of mechanical power and rotor speed is .
ROTOR SIDE CONTROLLER (RSC) AND GRID SIDE CONTROLLER (GSC) ARCHITECTURE AND DESIGN The control circuit for grid side controller (GSC) is shown in Figure 4a.
The rotor side converter (RSC) in Figure 4b is used to control the speed of rotor and also helps in maintaining desired grid voltage as The GSC and RSC have four control loops each, later has one speed control loop, other is reactive power and last two are direct and quadrature axis current control loops.
The speed and reactive power control loops are called outer control loop and direct and quadrature axis control loops are called inner control loops.
The difference between reference speed of generator and actual speed of generator is said to be rotor speed Speed error is minimized and maintained nearly at zero value by using speed controller loop which is a PI controller.
The output from speed controller is multiplied with stator flux (F.
and ratio of stator and rotor (Ls and L.
inductances to get reference quadrature current (Iq.
for rotor.
The error in reference and actual Tip Speed Ratio Based MPPT Algorithm and Improved Field Oriented Control for .
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The difference between these reference and actual two axis currents is controlled by tuned PI controller to get respective direct and quadrature axis voltages.
Figure 4a.
Grid side controller for DFIG Figure 4b.
Rotor side controller for DFIG For given wind speed, reference or control power from turbine is estimated using lookup table.
From equation .
, stator real power (Pstato.
is calculated and the error in powers is difference between these two powers .
P) which is to be maintained near zero by PI controller.
The output from PI controller is multiplied with real power constant (K.
gives actual controllable power after disturbance.
The difference in square of reference voltage across capacitor dc link (Vdc*) and square of actual dc link voltage (Vd.
is controlled using PI controller to get reference controllable real power.
The error in the reference and actual controllable power is divided by using 2/3Vsd to get direct axis .
-axi.
reference current near grid terminal (Igdre.
Difference in Igdref and actual d-axis grid current is controlled by PI controller to get d-axis voltage.
Similarly from stator RMS voltage (V.
or reference reactive power, actual stator voltage or reactive power is subtracted by PI controller and multiplied with appropriate reactive power constant (K.
to get actual reference reactive power compensating parameter.
From equation .
, actual reactive power is calculated and the difference in this and actual compensating reactive power and when divided by 2/3Vsq, we get quadrature axis .
-axi.
reference current (Iqre.
When the difference in Iqref and stator actual q-axis current (I.
is controlled by PI controller, reference q-axis voltage is obtained.
To improve transient response and to control steady state error, decoupled q-axis voltage has to be added as shown in Figure 4a.
Finally both d and q axis voltage parameters so obtained are converted to three axis abc parameters by using inverse ParkAos transformation and reference voltage is given to scalar PWM controller to get pulses for grid side IJECE Vol.
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The general form of speed regulation is given by = (Js B) A 1325 .
Where torque.
J is moment of inertia and B is friction coefficient, considered to be disturbance.
Multiplying both sides with , we get the equation as = (Js B) Considering .
constant and change in speed error is is control variable, the above equation .
As product of torque and speed is power, we will be getting stator reference power and disturbance power as shown below.
Where, .
Finally direct axis reference voltage can be written by using equation .
and from Fig.
5b is .
The rotating direct and quadrature reference voltages of rotor are converted into stationary abc frame parameters by using inverse parks transformation.
Slip frequency is used to generate sinusoidal and cosine parameters for inverse parks transformation.
RESULT ANALYSIS: CASE STUDIES
The dynamic performance of the DFIG system is investigated under two different cases and the rating specifications for DFIG and wind turbine parameters is given in appendix.
The wind speed change in these two cases in meters per seconds as 8, 15, 20 and 10 at 15, 25 and 35 seconds.
The reactive power and voltage value change in individual two cases with change in time is from -0.
6pu at 12 seconds to 0pu change at 20 seconds.
It was further changed from 0pu to 0.
6pu magnitude at 30 seconds.
Due to addition of large furnace or induction motor or non linear type load, leading reactive power greater than 0pu is required, while for light load lagging reactive power is required (<0p.
Hence DFIG will become better generator source if it can supply any desired reactive power effectively.
The change in grid terminal voltage takes place when suddenly switching on or off large loads or due to small faults near PCC.
The changes in tip- speed ration and power coefficient Cp both reactive power and wind speed variation in Figure 5a .
and variation with grid terminal voltage and wind speed both is shown in Figure 5a .
When wind speed is at 8m/s, tip speed ratio (TSR) is high near 4.
8 degrees and slowly decreases to 2.
at 15s when speed increases to 15m/s, further increased to 1.
9o at 25s when speed of wind is 20m/s and decreased to 3.
9o when wind speed decreased to 10m/s at 35s.
In the similar way.
Cp is also changing from 25 to 1.
7 at 15s, and further decreased to 1.
25 at 25s, and then increased to 2.
55 at 35 seconds with wind speed variation from 8 to 15 and then to 20, and 10 m/s.
The variation in TSR and Cp with change in reactive power is independent and has no effect as shown in Figure 5a .
However, with change in grid terminal voltage, a very small change in TSR and Cp can be observed.
It is due to the fact that the TSR and Cp depends on parameters as described by equations 1 to 5 and is independent on voltage and reactive power.
The reference mechanical turbine torque and generator torque with magnitudes overlapping and variation of rotor speed for two cases comparison is shown in Figure 5b.
With increase in wind speed, torque is increasing and vice-versa.
Till time up to 15 seconds, wind speed is at low value of 8m/s, so torque is at 0.
2pu and increased to -0.
5pu at 15s with increase in wind speed to 15m/s.
The torque further increased to 0.
9pu when wind speed is 20m/s and decreased to -0.
28pu when speed decreased to 10m/s.
there are small Tip Speed Ratio Based MPPT Algorithm and Improved Field Oriented Control for .
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With the change in wind speed, rotor speed is also varying but is maintained nearly at constant value of 1.
3pu RPM.
The changes in torque has effect with change in reactive power as in Fig.
and further more surges been observed when grid voltage disturbance occurred as in Figure 5b .
is taking place.
When reactive power is lagging at -0.
6pu, there is a small surge in torque at 20 seconds.
Generator speed is also low 27pu at -0.
6pu reactive power, while at 0pu reactive power, it is 1.
32pu speed.
But rotor speed increased 4pu speed at low terminal grid voltage of 0.
When, reactive power changes to 0pu from -0.
6pu, rotor speed increase from 1.
3pu to 1.
27pu and grid terminal voltage changes to 1pu from 0.
8pu between 20 to 30 Speed further increased to 1.
35pu with leading reactive power of 0.
6pu and decreased when grid voltage increase from 1pu to 1.
Therefore rotor speed increases if reactive power changes from lagging .
to leading ( v.
and rotor speed decreases with increase in grid terminal voltage beyond 1pu value in The surges in torque will be observed very high when terminal grid voltage changes is due to the fact of change in mechanical power is not that faster in comparison with electrical power change.
Figure 5a.
Tip speed ratio and Coefficient of power Cp for .
reactive power change & wind speed variation, .
both grid voltage & wind speed changes b .
Figure 5b.
Reference and actual generator torque and rotor speed variation with time for .
reactive power change & wind speed variation, .
both grid voltage & wind speed changes From Figure 5c .
, there is an increase in current from 0.
18pu to 0.
5pu at 15 seconds with increase in wind speed from 8 to 15m/s and further increased to 0.
9pu amps when speed increased to 20m/s and decreased to 0.
3pu amps when speed of wind is 10m/s.
When reactive power (Q) change from 0pu to -0.
current increased from 0.
5pu amps and decreased to 0.
5pu amps when Q changes from -0.
6pu to 0pu and increased to 1pu amps when speed of wind is 20m/s and reactive power is 0.
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Figure 5c.
Stator voltage and current three phase waveform with time for .
reactive power change & wind speed variation, .
both grid voltage & wind speed changes With sudden decrease in grid terminal voltage from 1pu to 0.
8pu volts at 12 seconds, slowly stator current decreased exponentially when wind speed is very low of 0.
1pu amps at 8m/s and this current was improved to 1pu when wind speed increased to 15m/s.
But when terminal voltage changed to 1pu from 0.
at 20s, current again reached to normal value of 0.
5pu amps as in case 1 and the current increased to again 1pu when wind speed reaches 20m/s.
when the grid terminal voltage increased to 1.
2pu from 1pu, the stator current again decreased to 0.
8pu amps and when wind speed finally reaches 10m/s with voltage at 1.
2pu, the current is 0.
2pu Amps as in Figure 5c .
Hence with increase in voltage at constant wind speed, current decreases and with increase in wind speed at same voltage current will increase and vice-versa.
In the similar way as does in stator voltage and current, rotor voltage and current will also vary, but rotor current is bidirectional unlike stator current does.
In these two cases, rotor voltage is nearly constant at 0.
32pu, but current is varying with both wind speed and reactive power change in Figure 5d .
and for voltage and wind speed variation as in Figure 5d .
When reactive power at -0.
6pu, rotor current is 0.
8pu is even low at 8m/s wind speed and increased to 1pu amps when wind speed reaches 15m/s as in Fig.
When reactive power reaches 1pu, rotor current is 5pu amps at wind speed of 15m/s and for leading reactive power of 0.
6pu, the rotor current is again 1pu at wind speed of 20m/s and 0.
5pu amps at 10m/s wind speed.
With increase in wind speed or at leading or lagging reactive power, rotor current is also increasing like stator current.
In the same scenario, rotor current is decreasing with increase in grid terminal voltage and vice-versa but without any appreciable change in rotor voltage.
With sudden changes in voltage at 12, 20 and 30 seconds, there are few spikes in rotor current due to sudden reversal of current magnitude and angle with respect to terminal voltages respectively.
Figure 5d.
Rotor voltage and current three phase waveform with time for .
reactive power change & wind speed variation, .
both grid voltage & wind speed changes The stator real and reactive power flow for all three cases is shown in Figure 5d.
The reference power which is the mechanical power output from turbine and actual generator real power change is shown in Figure 5e.
With change in wind speed, with very low wind speed of 8m/s, output stator real power is 1pu watts till 15 seconds.
When wind speed reaches 15m/s, stator real power increased to 0.
5pu and further increased to 0.
8pu for 20m/s wind speed at 25s and decreased to 0.
2pu power at 35s for 10m/s speed as Tip Speed Ratio Based MPPT Algorithm and Improved Field Oriented Control for .
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During the change in wind speed, real power alone is changing and reactive power is constant at reference of 0pu.
There are few surges in the reactive power due to change in voltage angle with respect to grid and also mainly due to change in stator and rotor current flows and rotor voltage change.
With the change in reactive power demand from grid from 0pu to -0.
6pu and 0.
6pu at 12 and 30 seconds are shown in Figure 5d .
With change in reactive power from 0pu to -0.
6pu, reactive power from generator is changing with a small time lag of 0.
8s and real power maintained nearly constant value of 0.
1pu at 8m/s wind Similarly with reactive power changing to 0pu and 0.
6pu, the reactive power is changing within 1 second and real power is almost constant with small surges in real stator power during this transient.
In case with both voltage and wind speed changing, with the grid voltage variation from 1 to 0.
8pu at 12th second, real power which is at 0.
1pu changed to 0.
05pu and reactive power which is at 0pu reached 1pu at this 12th second instant and slowly decaying to reach to reference 0pu value as shown in Figure 5d .
This change in reactive power is to make voltage of stator to get adjusted to grid voltage without losing synchronism.
Figure 5e.
Stator real and reactive power waveform with time for .
reactive power change & wind speed variation, .
both grid voltage & wind speed changes The reference mechanical power output and generator actual power is matching with reference power and the mismatch is because of looses in turbine, gear wheels and generator and this mismatch is With increase in wind speed, reference power is increasing and vice versa.
With the change in voltage at grid, stator terminal real power is maintained at constant value but with surges at instant of transient but reactive power is adjusting till stator voltage reaches the grid voltage for maintaining synchronism as shown in Figure 5d .
and 5e .
At the instant of 20s and 30s, there is surge in real and reactive powers but were maintaining constant stator output real powers of 0.
5 and 0.
8pu watts and 0pu var as in Figure 5d .
Figure 5f.
generator reference and actual real power waveform with time for .
reactive power change & wind speed variation, .
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To meet the desired grid reactive power, both stator and rotor has to supply for faster dynamics with an aid to RSC and GSC control schemes and is achieving as shown in Figure 5f .
With the change in wind speed and reactive power, real power from generator is matching its reference value for case 1, but small deviation can be observed from time 30 to 35 seconds is due to sudden change in reactive power demand from grid and the deviation in real power is from 0.
8pu to 0.
7pu which is small.
However, reactive power is following its trajectory within 1 second.
In the case 2 in Figure 5f .
, both voltage and reactive power changing with time, total output real and reactive powers from stator and rotor is delivering to grid to meet the desired grid power demand.
Unlike with change in reactive power, change in voltage is not affecting any deviation in real power and is following the trajectory nearly accurate with maximum deviation of 5% in real The reactive power change with grid voltage is high when voltage decreased from 1pu to 0.
8pu volts.
In the work in .
by authors, the wind speed is changing gradually and real and reactive powers are changing rapidly.
In our work, the wind speed is varying rapidly and according to changes in wind speed, the real power and current from stator are changing.
Compared to the work in the reference .
, with much change in wind speed conditions, the real power, stator current and power are varying.
The variations are much more precise and also the rotor speed in our case is nearly constant based on speed reference adjustment by MPPT algorithm.
The rotor speed is adjusted to optimal value by using fast acting gear Reactive power control in .
is compared with PI.
ANN and combination of both called as hybrid and authors proved that hybrid is better than individual operation with PI or ANN.
With the proposed methodology, the reactive power can reach the standards of hybrid controller with PI controller.
There are no surges in reactive power output or in current and voltage waveforms at grid or at DFIG a sin .
Similar to the work in .
, with the change in polarity of real power from positive to negative, the proposed method is also varying in the same way.
There is also nearly same action of independent control over real and reactive power outputs from DFIG.
Hence our work can perform better than the works presented in the earlier and can be valid for independent control of real and reactive power, and during rapid changing wind conditions.
Also extraction of reference power from turbine using MPPT and tracking the same from the generator is also possible with the proposed methodology.
The surges during any grid disturbances or due to wind speed conditions, the performance of DFIG system with proposed methodology is very accurate and stable.
CONCLUSION
From the proposed control scheme, the torque, speed and reactive power control of DFIG is very With change in wind speed, electromagnetic torque surges are low and the variation in wind speed is not getting the generator rotor speed variation is due to better transition in gear wheel mechanism.
Reactive power demand from grid is accurate which can be met by proper control action of RSC and GSC.
The proposed methodology is accurate and following all basic mathematical equations explained in previous When wind speed is increasing, mechanical and electrical torques are increasing without any change in stator reactive power.
Variation in grid reactive power causes quadrature currents on both stator and rotor to change but torque, speed or real powers from stator or rotor remains unaltered.
The variation in grid terminal voltage, a very small change in TSR and Cp can be observed.
It is due to the fact that the TSR and Cp depends on parameters and is independent on voltage and reactive power.
The TSR and Cp are blade size and shape with change in ambient temperature and wind speed dependant natural With increase in voltage at constant wind speed, current decreases but, with increase in wind speed at same voltage, current will increase and the decrease in wind speed caused current from stator to rotor decreases with stator voltage as constant as depicted by grid.
In the similar way as does in stator voltage and current, rotor voltage and current will also vary, but rotor current is bi-directional unlike stator current With the proposed control scheme, maximum power is captured from wind by DFIG even during light load conditions i.
cut-in wind speed.
This is attained by tracking optimal tip-speed ratio by controlling the DFIG electromagnetic torque during low and at rated wind speed.
Further generator speed is maintained at optimal value by using look-up table by using the generated torque and thus the DFIG rotor current is Thereby maximum power is extracted from the turbine-generator set.
Under full load condition when wind speed high, normally 24m/s, maximum output power can be extracted if rotor is driven at optimal speed for that particular wind speed.
If rotor speed can be referred to maintain at specified value, during wind speed variations, the rotor speed varies and gets adjusted.
Independent and faster reactive power control from 1pu to -1pu without deviation in real power from DFIG is achieved with proposed RSC and GSC improved field oriented control techniques.
The actual mechanical power output from turbine is matching with the real power production from DFIG is possible with MPPT and RSC control schemes.
The change in voltage at grid, stator terminal real power is maintained at constant value but with surges at instant of transient but reactive power is adjusting till stator voltage reaches the grid voltage for Tip Speed Ratio Based MPPT Algorithm and Improved Field Oriented Control for .
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To meet the desired grid reactive power, both stator and rotor has to supply for faster dynamics and it depends on faster action of RSC and GSC control schemes.
Distinct from reactive power variation, change in voltage is not affecting any deviation in real power and is following the trajectory nearly accurate with maximum deviation of 5% in real power.
The reactive power change with grid voltage is high when voltage decreased from 1pu to 0.
8pu volts.
Hence the proposed control scheme can be applied with ever changing transients like large variation in wind speed, reactive power and grid voltage.
The system is very stable without losing synchronism when grid voltage is increasing or decreasing to a A0.
2pu change from nominal voltage value.
APPENDIX
The parameters of DFIG used in simulation are.
Rated Power = 1.
5MW.
Rated Voltage = 690V.
Stator Resistance Rs = 0.
0049pu, rotor Resistance Rra = 0.
Stator Leakage Inductance Lls = 0.
Rotor Leakage inductance Llr1 = 0.
Inertia constant = 4.
Number of poles = 4.
Mutual Inductance Lm = 3.
39 pu.
DC link Voltage = 415V.
Dc link capacitance = 0.
Wind speed = 14 m/sec.
Grid Voltage = 25 KV.
Grid frequency = 60 Hz.
Grid side Filter:
Rfg = 0.
Lfg = 0.
Rotor side filter: Rfr = 0.
Lfr = 0.
Wind speed variations: 8, 15, 20 and 10 at 15, 25 and 35 seconds.
Reactive power change: -0.
6 to 0 and 0.
6pu at 20 and 30 seconds.
Grid voltage change: 0.
8 to 1 and to 1.
2pu at 20 and 30 seconds.
REFERENCES