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10-E-REN-1691




    A New Method of Maximum Power Point Tracking for DFIG Based
                          Wind Turbine

                                         Shabani, A. Deihimi
                                 Department of electrical engineering
                              Bu Ali Sina university, Hamedan, I. R. Iran
                                         a.shabani@basu.ac.ir


                         Keywords: wind turbine, DFIG, mppt, rotational speed




   Abstract                                              electric networks. In the grid of today
   In this paper, different operational regions of       penetration of wind turbines (WTs) is
   doubly fed induction generator (DFIG) based           growing rapidly in size and number. This
   wind turbine (WT), from viewpoints of rotor           increase in the size of wind turbines leads to
   speed, generated power, tip speed ratio (λ)           further reduction in the cost of wind power.
   and the angle of blades of the WT's rotor, is         And on the other hand, the decrement of cost
   studied and classified. Then a new fast and           of wind power redound to intensification in
   explicit method of maximum power point                the use of WECSs.
   tracking (mppt) will be proposed. The method          Along different types of WTs, the DFIG
   is based on the difference between optimum            based wind turbine has caught most of
   and current rotational speed of the shaft of          interest. This is because of: 1) in comparison
   WT. The proposed method is compared with              with constant speed WTs, DFIG based WT
   another method to unfold the superior one.            operates in much wider range of wind
   This comparison will be done based on the             velocity and it's production has a better power
   speed of operation and quality of generated           quality. 2) in comparison with synchronous
   power and the results shows the priority of the       generator based WT (PMSG or WRSG),
   proposed method.                                      DFIG based WT has less manufacturing cost
                                                         [1].
                                                         In DFIG based WT by using back-to-back
   1. INTRODUCTION                                       PWM inverters between the grid and the rotor
   The soaring use of fossil fuels and their             circuit (see fig. 1), and employing vector
   depletion over the last two decades combined          control techniques, the active and reactive
   with a growing concern about pollution of             powers handled by the machine can be
   environment have led to a boost for renewable         controlled independently [2]. Since the stator
   energy generation. This accelerated drive has         is directly connected to the grid, the stator
   led to a tremendous progress in the field of          flux is constant over the entire operating
   renewable energy systems during last decade.          region. Therefore, the torque can be
   Now a day wind energy conversion systems
   (WECS) becomes an essential part of modern
                                                     1
A New Method of Maximum Power Point Tracking for DFIG Based Wind Turbine
                                     25th International Power System Conference

maintained at its rated value even above the                 2. AERODYNAMIC POWER
synchronous speed [3].                                       Encountering of the wind with the blades of
However this type of WT is a variable speed                  the WT's rotor leads to creation of mechanical
one, but it's range of operational speeds is                 power in the rotor. The value of this power
restricted by the rate of power of it's rotor side           depends on the velocity of the wind,
inverter. In usual, the rate of power of                     rotational speed of WT's rotor, the angle of
converter is between 0.1 through 0.4 of                      rotor's blade and the structure of blades. The
generator rated power, and hence the                         produced power may be expressed as:
maximum slip (Smax) of generator would be
0.1 through 0.4, too [4].                                           1                                      (1)
Same as rotational speed, the rated power of                          .       . .       .     ,
                                                                    2
the DFIG based WT, is dictated by rated
power of generator and of course the rated                   Where PM is the mechanical power extracted
power of it's inverter [5].                                  from the wind in N.m/s; ρ is the air density
Based on the maximum value of speed and                      (1.225kg/m3); V is the wind speed (m/s) and
rated generating power, different controlling                R is the wind turbine rotor radius (m). Cp is
regions may be exposed and in each region,                   the Efficiency coefficient which is formulated
an especial controlling law                                  by use of the structural data of the WT's rotor,
                                                             blades angle (β) and tip speed ratio (λ) which
                                                             may be described as:
                                            WT's rotor

                                                                    .                                      (2)
        Back to back
         converter
                                         Gear
                                         box                 Where ωwt stands for rotational speed of WT's
                              DFIG
                                                             rotor.
 Fig. 1 a simple structure of DFIG based wind turbine        Cp can be described as:

governs. These controlling algorithms are                                                   116            (3)
                                                                          ,         0.22             0.4
described by maximum power point tracking
(mppt) controller [6].                                                                            12.5
In recent years, many papers has been                                               5
published about different methods of mppt                    Where
algorithm, some of them used sophisticated
controlling method like sliding mode [6]-[7],                 1           1                 0.035          (4)
and some used adaptive control [8] or Rotor
                                                                           0.08                 1
Position Phase Lock Loop (PLL) [9], [10].
But drawback of these method is their
complicated methods used by them. And                        λopt is a value of λ which make the maximum
meanwhile none of them describes the                         value of Cp (see fig. 2).
controlling algorithm of all operational                     Fig. 3 illustrates mechanical power curves for
regions.                                                     each wind speed versus ωwt with use of
In this paper, controlling method of whole                   equations (1) through (4). And effect of β on
operational regions are described and a new                  the extracted power is shown in fig. 4 [1].
simple and explicit mppt algorithm is
proposed.




                                                         2
A New Method of M
                                  Maximum Power Point Track
                                                          king for DFIG Based Wind Turbine
                                                                      G          d
                                    25t Internation Power Sys
                                      th
                                                  nal       stem Confere
                                                                       ence

                                                              th rotor or from the rotor to th grid) is
                                                               he        r                        he       s
                                                              us
                                                               sually betw
                                                                         ween 0.1 t   through 0.4 of rated
                                                                                                  4        d
                                                              po
                                                               ower of gen nerator and this ratio determines
                                                                                      d                    s
                                                              th maximu
                                                               he         um slip o generato So the
                                                                                     of          or.       e
                                                              ro
                                                               otational sp
                                                                          peed of g  generator should laid
                                                                                                 s         d
                                                              be
                                                               etween the rrange of [6] :
                                                                                      ]

                                                                           1     |           |                                    )
                                                                                                                                (5)
                                                                                                        1       |      |

                 Fig. 2 C versus λ .
                        Cp                                    Where ωrated is the synchronous speed of
                                                              W                                 s          f
                                                              ge
                                                               enerator.
                                                              The rated pow of WT may be rep
                                                                           wer                  presented as
                                                                                                           s
                                                              a function of stator or ro rated po
                                                                          f            otor     ower:

                                                                                         1                                      (6)
                                                                                                                                  )
                                                                      1                           | |

                                                              Where Pt is t delivere power of WT to the
                                                              W           the         ed          f           e
                                                              gr Ps is the power del
                                                               rid,       e           livered just by stator of
                                                                                                              f
                                                              ge
                                                               enerator and Pr is the p
                                                                          d           power delivvered by the e
                                                              ro circuit [5].
                                                               otor

Fig. 3 harves mechanic power vers ωwt , spee
            sted         cal        sus    eds                Pt
            of
            o the wind fro 4m/s to 22
                         om         2m/s.                                         I               II                 III
                                                                   Pmax

                                                                                                                                Vw
                                                              ωr

                                                                   ωrmax

                                                                                                                                 Vw
                                                              Cp
                                                                   Cpmax
  Fig. 4 diffe
             erent mechanic power for constant wind
                          cal                       d
speed of 12m which are results of fluc
             m/s                     ctuations in β (in
                        de
                         egree)                                                                                                 Vw
                                                                                Var.
                                                                                V ωr             Co ωr
                                                                                                  ons.              Co ωr
                                                                                                                     ons.
OPERATI    IONAL RE  EGIONS                                                     Opt. λ            V λ
                                                                                                  Var.              Co Pt
                                                                                                                     ons.
                                                                                 Β=0               Β=0               Β>0
                                                                                                                     Β
As can be seen in fig 1, the ro
                      g.         otor circuit of
generator i connected to the util grid via a
          is          d           lity       a                        Vcut in            Vr max        Vrated               Vcut out
back to back conv     verter. By using th
                                y            his
converter, the generat power o WT may b
                     ted        of            be
controlled. The maxi
          .          imum powe which can
                                 er                                  Fig. 5 DF based WT controlling regions
                                                                             FIG      T             r
flow throu the con
          ugh        nverter (from the grid to
                                 m

                                                          3
A New Method of Maximum Power Point Tracking for DFIG Based Wind Turbine
                               25th International Power System Conference

It is evident that the limits of maximum               This means that in this region, the λ is not at
allowable generating power and maximum                 it's optimum value any more and would be
and minimum allowable rotational speed of              reduced (see fig. 2).
generator should not be exceeded. Based on             In this region the value of β is still zero.
these limitations, different operational regions
may be introduced.                                     C. Region III
Fig. 5 shows different operational regions             This condition is the last situation that a WT
which may be considered in controlling of a            would operate in. the lower wind speed limit
DFIG based WT.                                         of this region is Vrated and the upper limit is
As can be seen in fig. 5, there are three major        Vcut out . if the wind speed exceed this limit the
controlling regions, which are discussed here:         operation of WT would be stopped and the
                                                       braking system would engaged because
A. Region I                                            mechanical damage is expected.
This region is between Vcut in and Vr max. When        In this region, the rotational speed of WT is
the wind velocity is less than Vcut in , the WT        still kept constant at it's maximum value. λ
doesn't produce any electrical power and the           and Cp are not on their optimum value and
incoming mechanical power is wasted in                 further more, the angle of blades has
rotational components of WT. At speed of cut           increased from zero to kept the mechanical
in, which depends on the type of WT is                 power at it's rated value (see fig. 4).
between 2.5 m/s through 4 m/s, producing the           The increment command of angle of blades is
electrical power which is commanded by                 issued by mppt algorithm.
mppt unit, would be begun. The transferring
ratio of gear box should be chosen in a way
that when the Cp has its maximum value, the            3. PROPOSED MPPT ALGORITHM
ωr cutin corresponds to Vcutin be as:                  Basis of all these controlling regions shown in
                                                       fig. 5, is on contrasting of mechanical and
          .                                 (7)        electrical torque which with neglecting the
                    1   |     |                        damping factor and spring constant, it can be
                                                       formulated as:
And the upper limit of this region would be as                                                     (8)
upper limit in (5). In whole this region, the λ
should have it's optimum value, which leads
to maximum of Cp and hence, for each wind              Whit knowing that:
speed, the maximum extractable power would
yields (see fig. 2 and 3).                                    .                                      (9)
And the angle of blades would be kept zero,
because the maximum mechanical power has               It is evident that with convenient adjustment
been not reached yet.                                  of recommended power (Pset), changes of ω
                                                       can be controlled.
B. Region II                                           Now controlling algorithm of different
This region laid between two wind speed of             regions may be expanded.
Vr max and Vrated . in this region, the speed of
the generator's rotor                                  A. Region I
 Reached to it's maximum value and should              As mentioned before, in this region, it is need
not be exceeded (should be kept constant at            to follow the optimum λ and hence according
it's maximum value). So the controlling                to (2), the ω should be changed linearly with
algorithm should operate in a way that                 change of wind speed. So with regards to (8)
increase of wind speed doesn't lead to                 and (9), if the ω should be increased, the
increase in rotational speed of WT's rotor.            value of Pset must be set much lower than

                                                   4
A New Method of M
                                 Maximum Power Point Track
                                                         king for DFIG Based Wind Turbine
                                                                     G          d
                                  25t Internation Power Sys
                                    th
                                                nal       stem Confere
                                                                     ence

mechanica power (PM) and if the ω should b
         al                   e          be                WT's rotating parts, and this lead to reduction
                                                           W             g        d                      n
decreased, the value of Pset sh
                    e         hould be sset                in ωr and it w last unti Δω acced to zero.
                                                            n           will       il        de
much high than PM . the propos followin
         her                  sed        ng                With proper choosing of K, its possible to
                                                           W            r                      p         o
equation w
         would do it a well:
                     as                                    co
                                                            ontrol the rrate and accuracy of fluctuations
                                                                                              f          s
                                                           in produced p
                                                            n            power.
                                                (10)
                                                           B. Region II
                                                           B
Where ωopt is the               rotati
                                     ional    speed        In this regi
                                                            n          ion, it is n
                                                                                  need to ke the ωr
                                                                                             ept
correspond
         ding to λopt .                                    co
                                                            onstant, so t value of Pset should be equals
                                                                        the                            s
                                                           to PM, which means tha the rate of change of
                                                            o          h         at                    f
                                                           ωr should be zero.

                                                           C. Region II
                                                           C            III
                                                           The controll  ling algorit thm of reg gion II, iss
                                                           ta
                                                            aken in this region too, and in add
                                                                                     ,          dition, since
                                                                                                            e
                                                           th mechanic power h reached to it's limit,
                                                            he           cal        has                      ,
                                                           th pitch con
                                                            he          ntrol takes a part in the controlling
                                                                                                            g
                                                           prrocess. As can be s     seen in fig 4, with
                                                                                                 g.         h
                                                           in
                                                            ncreasing t  the angle of blades (β), the
                                                                                                 s          e
                                                           haarvesting      mechaniccal     poweer     wouldd
                                                           deecreased an hence in
                                                                         nd         nput power remains in   n
                                                           it's upper lim
                                                                        mit.
  Fig. 6 disp
            placement of o
                         operation poin in proposed
                                      nt          d
                    mppt method
                         t                                 Siince the p  pitch contr  rol is a mechanical   l
                                                           prrocess, has it's own dyynamic which depends    s
Fig. 6 illus
           strates the w equation (10) work
                        way                      ks.       on the struct
                                                             n           ture of win turbine. In WTs of
                                                                                    nd                      f
At first, assume that th wind spe is V2, an
                          he         eed         nd        to
                                                            oday, the m maximum ch  hanges in bl lade's angle
                                                                                                            e
the mechan  nical power has settled at P2 and ω
                         r          d                      is about 10 d
                                                            s            degrees per second [1] Structure
                                                                                     r           ].         e
of WT is ω2. Now th     here is an in
                                    ncrease in the         of pitch con
                                                             f          ntroller can be found in [11] and
                                                                                                 i          d
wind speed from V2 t V3. Due to enormo
            d             to                    ous        [1
                                                            12].
moment of WT's rotating compo
            f                       onents, at fir
                                                 rst
instant, flluctuation of rotation speed is
                                    nal                    4. SIMULAT
                                                             .          TION RES  SULTS
neglectable and hen
            e            nce the o output pow  wer         All simulatio here ha been acc
                                                           A            ons        as          complished
                                                                                                        d
would be P23. Accord     ding to (10 in the fir
                                   0),           rst       in MATLAB
                                                            n           B/simulink. The para
                                                                                   .           ameters of
                                                                                                        f
moment, th discrepan betwee PM and Pset
            he            ncy       en                     WT which h been c
                                                           W            has        considered as the test
                                                                                                        t
is K(ω3 - ω2 ), whi would b subtracted
                         ich         be                    beench is av vailable in appendix. for more  e
from PM. t differen between PM and Ps ,
           this         nce         n            set        nformation about mode
                                                           in                      eling of WT one may
                                                                                               T,       y
will led the ωr to increase. During th          his        re to [5] a [13]. the value of K in (10) is
                                                            efer       and         e                    s
process, PM moves f      from P23 to
                                   oward P3, an  nd        ch
                                                            hosen as 5e the othe algorithm suggested
                                                                        e6.        er        m          d
Pset tracks the trajec
           s            ctory of B to P3. Wi     ith       in [3], is com
                                                            n           mpared wit proposed algorithm
                                                                                   th         d        m
approachin Pset to P3 the stateme K(ω3 – ωr
           ng                        ent                   to unfold su
                                                            o          uperior one. This algo orithm uses
                                                                                                        s
) reduces to zero.
            o                                              th changes of power t control the WT. as
                                                            he                     to          t        s
At the nex step, its assumed t
            xt                      that the win nd        th input, th wind spe assume to be 10
                                                            he         he          eed        ed        0
speed has a reductio from V2 to V1. Lik
                        on                       ke        m/s, in secon 70 it red
                                                           m            nd          duces to 9 m/s and in
                                                                                                        n
pervious st tate, at the f
                         first momen ωr rema
                                    nt,         ain        se
                                                            econd 150, it increases to 10 m/s again (see
                                                                                   s          s         e
unchanged and PM ha a step d
           d             as        down from P2            fig. 7). The rated wi
                                                                        e          ind speed of WT is   s
to P21. The Pset woul be P21+K 2 – ω1). In
           en            ld        K(ω                     su
                                                            upposed to b 12 m/s.
                                                                        be
this case Pset is more than PM, an deficiency
                                     nd                    As can be se in fig. 8 the produ
                                                           A            een        8,          uced power
                                                                                                        r
of mechan  nical input p power will compensated            of proposed algorithm (the bolt one) is
                                                             f         d          m                     s
by kinetic energy sto   ored in rotaating mass of          sm
                                                            moother tha the othe one and it's power
                                                                        an         er                   r

                                                       5
A New Method of Maximum Power Point Tracking for DFIG Based Wind Turbine
                                   25th International Power System Conference

quality is better, too. Another drawback of                 outputs of this algorithm are shown. In fig. 9,
suggested mppt algorithm in [3].                            the amplitude of λ, is shown which according
                                                            to fig. 2 should be about 7.2. fig. 10, shows
                                                            the rotational speed of WT's rotor. Fig.11,
                                                            illustrates the electrical torque of generator.
                                                            Fig. 12, presents the mechanical input power
                                                            (bolt one) which delivered by the WT's shaft
                                                            and electrical produced power delivered to the
                                                            utility grid. In these simulations, demanded
                                                            reactive power is supposed to be zero. As can
                                                            be seen in fig. 12, the generated electrical
 Fig. 7 profile of wind speed, applied for comparison       power has an overshoot at time 70s, and an




 Fig. 8 comparison of produced power by proposed                  Fig. 11 generated electrical torque of WT.
mppt algorithm (the bolt one) and the mppt algorithm
                  suggested in [3].




                                                            Fig. 12 mechanical (bolt line) and electrical (thin line)
                                                                                   power.
                Fig. 9 amplitude of λ.




                                                                Fig. 13 terminal out coming d and q currents.
       Fig. 10 rotational speed of WT's rotor.
                                                            undershoot at time 150 s. these are because of
Now that the superiority of proposed                        the kinetic energy stored in rotating mass
algorithm has been unfolded, the other                      which       unleashes during reduction in
                                                            rotational speed, and stores during increment
                                                        6
A New Method of Maximum Power Point Tracking for DFIG Based Wind Turbine
                                25th International Power System Conference

. this affects terminal currents shown in fig.              Ind. Electron. Soc., vol. 48, pp. 786–793,
13, which exposes terminal out coming d and                 Aug. 2001.
q currents.                                             [3] R. Datta and V.T. Ranganathan," A
                                                            Method of Tracking the Peak Power
                                                            Points for a Variable Speed Wind Energy
5. CONCLUSION                                               Conversion System", IEEE Trans, energy
Different operating and controlling regions of              conversion, VOL. 18, NO. 1, MARCH
                                                            2003
DFIG based wind turbine from viewpoints of
                                                        [4] Ion Boldea, Variable Speed Generators.
rotor speed, generated power, tip speed ratio               Boca Raton, FL: Taylor & Francis, 2006.
(λ) and the angle of blades of the wind                 [5] Hee-Sang Ko, Gi-Gab Yoon, and Won-
turbine's rotor, is studied and classified. Based           Pyo Hong, "Active Use of DFIG-Based
on these regions, a new simple method of                    Variable-Speed Wind-Turbine for Voltage
maximum power point tracking algorithm is                   Regulation at a Remote Location," IEEE
presented which is based on Δω of rotor. This               Trans, Power systems, VOL. 22, NO.
algorithm applied to model of a typical DFIG                4,pp. 1916-1925, NOVEMBER 2007
based WT in MATLAB/simulink, and results                [6] B. Beltran, M.E.H. Benbouzid and T.
                                                            Ahmed-Ali, " High-Order Sliding Mode
proves the efficiency of new method.
                                                            Control of a DFIG-Based Wind Turbine
                                                            for Power Maximization and Grid Fault
                                                            Tolerance " Electric Machines and Drive
APENDIX                                                     Conference, 2009
Wind turbine and generator data:                        [7] Xuemei Zheng, Lin Li, Dianguo Xu and
Drive train:                                                Jim Platts, "Sliding Mode MPPT Control
Jgen=121.5,                      Jwt=6.41e6,                of Variable Speed Wind Power System"
Kse=1.4035e4,                     De=500e3,                 Power and energy engineering conference,
Kgear=168.3                                                 APPEEC, 2009
                                                        [8] Changhong Shao, Xiangjun Chen and
Generator:                                                  Zhonghua Liang, " Application Research
                                                            of Maximum Wind-energy Tracing
                                                            Controller Based Adaptive Control
P=4,                ns=20,                nr=80,            Strategy in WECS", IPEMC 2006
f=50Hz,            Van=690V                             [9] Baike Shen, , Bakari Mwinyiwiwa,
Sb=2.5MW,                           Rs=4.29e-3,             Yongzheng Zhang, , and Boon-Teck Ooi,"
Ls=0.257e-3,                        Rr=7.68e-2,             Sensorless Maximum Power Point
Lr=4.858e-3,      Lm=8.0428e-3                              Tracking of Wind by DFIG Using Rotor
                                                            Position Phase Lock Loop (PLL)" IEEE
Wind turbine:                                               Trans, power electronics, VOL. 24, NO.
                                                            4, APRIL 2009
                                                        [10] A. Petersson " Analysis, Modeling and
Slip(Smax)=0.25,                                            Control     of    Doubly-Fed      Induction
cut-in wind speed: 4 m/s,                                   Generators for Wind Turbines", Ph.D.
cut-out wind speed: 22 m/s,                                 dissertation, Dept. of Energy and
rated wind speed:12m/s,                                     Environment, Univ. Chalmers, Goteborg,
turbine rotor radius: 41.5m                                 Sweden 2005
                                                        [11] E. Hau, Wind turbines. Berlin,
REFERENCE                                                   Germany: Springer, 2006
[1] T. Ackermann, Wind Power in Power                   [12] F.B. Bianchi, H. De Battista, Wind
    Systems. New York, UK: John Wiley &                     Turbine     Control    Systems.      Berlin,
    Sons, 2005.                                             Germany: Springer, 2007
[2] R. Datta and V. T. Ranganathan, “A                  [13] F. Iov, A. D. Hansen, P. Sørensen, F.
    simple position sensorless algorithm for                Blaabjerg, "Wind Turbine Blockset in
    rotor side field oriented control of wound              Matlab Simulink". Aalborg University,
    rotor induction machine,” IEEE Trans.                   Denmark: March 2004

                                                    7

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10 e-ren-1691

  • 1. 10-E-REN-1691 A New Method of Maximum Power Point Tracking for DFIG Based Wind Turbine Shabani, A. Deihimi Department of electrical engineering Bu Ali Sina university, Hamedan, I. R. Iran a.shabani@basu.ac.ir Keywords: wind turbine, DFIG, mppt, rotational speed Abstract electric networks. In the grid of today In this paper, different operational regions of penetration of wind turbines (WTs) is doubly fed induction generator (DFIG) based growing rapidly in size and number. This wind turbine (WT), from viewpoints of rotor increase in the size of wind turbines leads to speed, generated power, tip speed ratio (λ) further reduction in the cost of wind power. and the angle of blades of the WT's rotor, is And on the other hand, the decrement of cost studied and classified. Then a new fast and of wind power redound to intensification in explicit method of maximum power point the use of WECSs. tracking (mppt) will be proposed. The method Along different types of WTs, the DFIG is based on the difference between optimum based wind turbine has caught most of and current rotational speed of the shaft of interest. This is because of: 1) in comparison WT. The proposed method is compared with with constant speed WTs, DFIG based WT another method to unfold the superior one. operates in much wider range of wind This comparison will be done based on the velocity and it's production has a better power speed of operation and quality of generated quality. 2) in comparison with synchronous power and the results shows the priority of the generator based WT (PMSG or WRSG), proposed method. DFIG based WT has less manufacturing cost [1]. In DFIG based WT by using back-to-back 1. INTRODUCTION PWM inverters between the grid and the rotor The soaring use of fossil fuels and their circuit (see fig. 1), and employing vector depletion over the last two decades combined control techniques, the active and reactive with a growing concern about pollution of powers handled by the machine can be environment have led to a boost for renewable controlled independently [2]. Since the stator energy generation. This accelerated drive has is directly connected to the grid, the stator led to a tremendous progress in the field of flux is constant over the entire operating renewable energy systems during last decade. region. Therefore, the torque can be Now a day wind energy conversion systems (WECS) becomes an essential part of modern 1
  • 2. A New Method of Maximum Power Point Tracking for DFIG Based Wind Turbine 25th International Power System Conference maintained at its rated value even above the 2. AERODYNAMIC POWER synchronous speed [3]. Encountering of the wind with the blades of However this type of WT is a variable speed the WT's rotor leads to creation of mechanical one, but it's range of operational speeds is power in the rotor. The value of this power restricted by the rate of power of it's rotor side depends on the velocity of the wind, inverter. In usual, the rate of power of rotational speed of WT's rotor, the angle of converter is between 0.1 through 0.4 of rotor's blade and the structure of blades. The generator rated power, and hence the produced power may be expressed as: maximum slip (Smax) of generator would be 0.1 through 0.4, too [4]. 1 (1) Same as rotational speed, the rated power of . . . . , 2 the DFIG based WT, is dictated by rated power of generator and of course the rated Where PM is the mechanical power extracted power of it's inverter [5]. from the wind in N.m/s; ρ is the air density Based on the maximum value of speed and (1.225kg/m3); V is the wind speed (m/s) and rated generating power, different controlling R is the wind turbine rotor radius (m). Cp is regions may be exposed and in each region, the Efficiency coefficient which is formulated an especial controlling law by use of the structural data of the WT's rotor, blades angle (β) and tip speed ratio (λ) which may be described as: WT's rotor . (2) Back to back converter Gear box Where ωwt stands for rotational speed of WT's DFIG rotor. Fig. 1 a simple structure of DFIG based wind turbine Cp can be described as: governs. These controlling algorithms are 116 (3) , 0.22 0.4 described by maximum power point tracking (mppt) controller [6]. 12.5 In recent years, many papers has been 5 published about different methods of mppt Where algorithm, some of them used sophisticated controlling method like sliding mode [6]-[7], 1 1 0.035 (4) and some used adaptive control [8] or Rotor 0.08 1 Position Phase Lock Loop (PLL) [9], [10]. But drawback of these method is their complicated methods used by them. And λopt is a value of λ which make the maximum meanwhile none of them describes the value of Cp (see fig. 2). controlling algorithm of all operational Fig. 3 illustrates mechanical power curves for regions. each wind speed versus ωwt with use of In this paper, controlling method of whole equations (1) through (4). And effect of β on operational regions are described and a new the extracted power is shown in fig. 4 [1]. simple and explicit mppt algorithm is proposed. 2
  • 3. A New Method of M Maximum Power Point Track king for DFIG Based Wind Turbine G d 25t Internation Power Sys th nal stem Confere ence th rotor or from the rotor to th grid) is he r he s us sually betw ween 0.1 t through 0.4 of rated 4 d po ower of gen nerator and this ratio determines d s th maximu he um slip o generato So the of or. e ro otational sp peed of g generator should laid s d be etween the rrange of [6] : ] 1 | | ) (5) 1 | | Fig. 2 C versus λ . Cp Where ωrated is the synchronous speed of W s f ge enerator. The rated pow of WT may be rep wer presented as s a function of stator or ro rated po f otor ower: 1 (6) ) 1 | | Where Pt is t delivere power of WT to the W the ed f e gr Ps is the power del rid, e livered just by stator of f ge enerator and Pr is the p d power delivvered by the e ro circuit [5]. otor Fig. 3 harves mechanic power vers ωwt , spee sted cal sus eds Pt of o the wind fro 4m/s to 22 om 2m/s. I II III Pmax Vw ωr ωrmax Vw Cp Cpmax Fig. 4 diffe erent mechanic power for constant wind cal d speed of 12m which are results of fluc m/s ctuations in β (in de egree) Vw Var. V ωr Co ωr ons. Co ωr ons. OPERATI IONAL RE EGIONS Opt. λ V λ Var. Co Pt ons. Β=0 Β=0 Β>0 Β As can be seen in fig 1, the ro g. otor circuit of generator i connected to the util grid via a is d lity a Vcut in Vr max Vrated Vcut out back to back conv verter. By using th y his converter, the generat power o WT may b ted of be controlled. The maxi . imum powe which can er Fig. 5 DF based WT controlling regions FIG T r flow throu the con ugh nverter (from the grid to m 3
  • 4. A New Method of Maximum Power Point Tracking for DFIG Based Wind Turbine 25th International Power System Conference It is evident that the limits of maximum This means that in this region, the λ is not at allowable generating power and maximum it's optimum value any more and would be and minimum allowable rotational speed of reduced (see fig. 2). generator should not be exceeded. Based on In this region the value of β is still zero. these limitations, different operational regions may be introduced. C. Region III Fig. 5 shows different operational regions This condition is the last situation that a WT which may be considered in controlling of a would operate in. the lower wind speed limit DFIG based WT. of this region is Vrated and the upper limit is As can be seen in fig. 5, there are three major Vcut out . if the wind speed exceed this limit the controlling regions, which are discussed here: operation of WT would be stopped and the braking system would engaged because A. Region I mechanical damage is expected. This region is between Vcut in and Vr max. When In this region, the rotational speed of WT is the wind velocity is less than Vcut in , the WT still kept constant at it's maximum value. λ doesn't produce any electrical power and the and Cp are not on their optimum value and incoming mechanical power is wasted in further more, the angle of blades has rotational components of WT. At speed of cut increased from zero to kept the mechanical in, which depends on the type of WT is power at it's rated value (see fig. 4). between 2.5 m/s through 4 m/s, producing the The increment command of angle of blades is electrical power which is commanded by issued by mppt algorithm. mppt unit, would be begun. The transferring ratio of gear box should be chosen in a way that when the Cp has its maximum value, the 3. PROPOSED MPPT ALGORITHM ωr cutin corresponds to Vcutin be as: Basis of all these controlling regions shown in fig. 5, is on contrasting of mechanical and . (7) electrical torque which with neglecting the 1 | | damping factor and spring constant, it can be formulated as: And the upper limit of this region would be as (8) upper limit in (5). In whole this region, the λ should have it's optimum value, which leads to maximum of Cp and hence, for each wind Whit knowing that: speed, the maximum extractable power would yields (see fig. 2 and 3). . (9) And the angle of blades would be kept zero, because the maximum mechanical power has It is evident that with convenient adjustment been not reached yet. of recommended power (Pset), changes of ω can be controlled. B. Region II Now controlling algorithm of different This region laid between two wind speed of regions may be expanded. Vr max and Vrated . in this region, the speed of the generator's rotor A. Region I Reached to it's maximum value and should As mentioned before, in this region, it is need not be exceeded (should be kept constant at to follow the optimum λ and hence according it's maximum value). So the controlling to (2), the ω should be changed linearly with algorithm should operate in a way that change of wind speed. So with regards to (8) increase of wind speed doesn't lead to and (9), if the ω should be increased, the increase in rotational speed of WT's rotor. value of Pset must be set much lower than 4
  • 5. A New Method of M Maximum Power Point Track king for DFIG Based Wind Turbine G d 25t Internation Power Sys th nal stem Confere ence mechanica power (PM) and if the ω should b al e be WT's rotating parts, and this lead to reduction W g d n decreased, the value of Pset sh e hould be sset in ωr and it w last unti Δω acced to zero. n will il de much high than PM . the propos followin her sed ng With proper choosing of K, its possible to W r p o equation w would do it a well: as co ontrol the rrate and accuracy of fluctuations f s in produced p n power. (10) B. Region II B Where ωopt is the rotati ional speed In this regi n ion, it is n need to ke the ωr ept correspond ding to λopt . co onstant, so t value of Pset should be equals the s to PM, which means tha the rate of change of o h at f ωr should be zero. C. Region II C III The controll ling algorit thm of reg gion II, iss ta aken in this region too, and in add , dition, since e th mechanic power h reached to it's limit, he cal has , th pitch con he ntrol takes a part in the controlling g prrocess. As can be s seen in fig 4, with g. h in ncreasing t the angle of blades (β), the s e haarvesting mechaniccal poweer wouldd deecreased an hence in nd nput power remains in n it's upper lim mit. Fig. 6 disp placement of o operation poin in proposed nt d mppt method t Siince the p pitch contr rol is a mechanical l prrocess, has it's own dyynamic which depends s Fig. 6 illus strates the w equation (10) work way ks. on the struct n ture of win turbine. In WTs of nd f At first, assume that th wind spe is V2, an he eed nd to oday, the m maximum ch hanges in bl lade's angle e the mechan nical power has settled at P2 and ω r d is about 10 d s degrees per second [1] Structure r ]. e of WT is ω2. Now th here is an in ncrease in the of pitch con f ntroller can be found in [11] and i d wind speed from V2 t V3. Due to enormo d to ous [1 12]. moment of WT's rotating compo f onents, at fir rst instant, flluctuation of rotation speed is nal 4. SIMULAT . TION RES SULTS neglectable and hen e nce the o output pow wer All simulatio here ha been acc A ons as complished d would be P23. Accord ding to (10 in the fir 0), rst in MATLAB n B/simulink. The para . ameters of f moment, th discrepan betwee PM and Pset he ncy en WT which h been c W has considered as the test t is K(ω3 - ω2 ), whi would b subtracted ich be beench is av vailable in appendix. for more e from PM. t differen between PM and Ps , this nce n set nformation about mode in eling of WT one may T, y will led the ωr to increase. During th his re to [5] a [13]. the value of K in (10) is efer and e s process, PM moves f from P23 to oward P3, an nd ch hosen as 5e the othe algorithm suggested e6. er m d Pset tracks the trajec s ctory of B to P3. Wi ith in [3], is com n mpared wit proposed algorithm th d m approachin Pset to P3 the stateme K(ω3 – ωr ng ent to unfold su o uperior one. This algo orithm uses s ) reduces to zero. o th changes of power t control the WT. as he to t s At the nex step, its assumed t xt that the win nd th input, th wind spe assume to be 10 he he eed ed 0 speed has a reductio from V2 to V1. Lik on ke m/s, in secon 70 it red m nd duces to 9 m/s and in n pervious st tate, at the f first momen ωr rema nt, ain se econd 150, it increases to 10 m/s again (see s s e unchanged and PM ha a step d d as down from P2 fig. 7). The rated wi e ind speed of WT is s to P21. The Pset woul be P21+K 2 – ω1). In en ld K(ω su upposed to b 12 m/s. be this case Pset is more than PM, an deficiency nd As can be se in fig. 8 the produ A een 8, uced power r of mechan nical input p power will compensated of proposed algorithm (the bolt one) is f d m s by kinetic energy sto ored in rotaating mass of sm moother tha the othe one and it's power an er r 5
  • 6. A New Method of Maximum Power Point Tracking for DFIG Based Wind Turbine 25th International Power System Conference quality is better, too. Another drawback of outputs of this algorithm are shown. In fig. 9, suggested mppt algorithm in [3]. the amplitude of λ, is shown which according to fig. 2 should be about 7.2. fig. 10, shows the rotational speed of WT's rotor. Fig.11, illustrates the electrical torque of generator. Fig. 12, presents the mechanical input power (bolt one) which delivered by the WT's shaft and electrical produced power delivered to the utility grid. In these simulations, demanded reactive power is supposed to be zero. As can be seen in fig. 12, the generated electrical Fig. 7 profile of wind speed, applied for comparison power has an overshoot at time 70s, and an Fig. 8 comparison of produced power by proposed Fig. 11 generated electrical torque of WT. mppt algorithm (the bolt one) and the mppt algorithm suggested in [3]. Fig. 12 mechanical (bolt line) and electrical (thin line) power. Fig. 9 amplitude of λ. Fig. 13 terminal out coming d and q currents. Fig. 10 rotational speed of WT's rotor. undershoot at time 150 s. these are because of Now that the superiority of proposed the kinetic energy stored in rotating mass algorithm has been unfolded, the other which unleashes during reduction in rotational speed, and stores during increment 6
  • 7. A New Method of Maximum Power Point Tracking for DFIG Based Wind Turbine 25th International Power System Conference . this affects terminal currents shown in fig. Ind. Electron. Soc., vol. 48, pp. 786–793, 13, which exposes terminal out coming d and Aug. 2001. q currents. [3] R. Datta and V.T. Ranganathan," A Method of Tracking the Peak Power Points for a Variable Speed Wind Energy 5. CONCLUSION Conversion System", IEEE Trans, energy Different operating and controlling regions of conversion, VOL. 18, NO. 1, MARCH 2003 DFIG based wind turbine from viewpoints of [4] Ion Boldea, Variable Speed Generators. rotor speed, generated power, tip speed ratio Boca Raton, FL: Taylor & Francis, 2006. (λ) and the angle of blades of the wind [5] Hee-Sang Ko, Gi-Gab Yoon, and Won- turbine's rotor, is studied and classified. Based Pyo Hong, "Active Use of DFIG-Based on these regions, a new simple method of Variable-Speed Wind-Turbine for Voltage maximum power point tracking algorithm is Regulation at a Remote Location," IEEE presented which is based on Δω of rotor. This Trans, Power systems, VOL. 22, NO. algorithm applied to model of a typical DFIG 4,pp. 1916-1925, NOVEMBER 2007 based WT in MATLAB/simulink, and results [6] B. Beltran, M.E.H. Benbouzid and T. Ahmed-Ali, " High-Order Sliding Mode proves the efficiency of new method. Control of a DFIG-Based Wind Turbine for Power Maximization and Grid Fault Tolerance " Electric Machines and Drive APENDIX Conference, 2009 Wind turbine and generator data: [7] Xuemei Zheng, Lin Li, Dianguo Xu and Drive train: Jim Platts, "Sliding Mode MPPT Control Jgen=121.5, Jwt=6.41e6, of Variable Speed Wind Power System" Kse=1.4035e4, De=500e3, Power and energy engineering conference, Kgear=168.3 APPEEC, 2009 [8] Changhong Shao, Xiangjun Chen and Generator: Zhonghua Liang, " Application Research of Maximum Wind-energy Tracing Controller Based Adaptive Control P=4, ns=20, nr=80, Strategy in WECS", IPEMC 2006 f=50Hz, Van=690V [9] Baike Shen, , Bakari Mwinyiwiwa, Sb=2.5MW, Rs=4.29e-3, Yongzheng Zhang, , and Boon-Teck Ooi," Ls=0.257e-3, Rr=7.68e-2, Sensorless Maximum Power Point Lr=4.858e-3, Lm=8.0428e-3 Tracking of Wind by DFIG Using Rotor Position Phase Lock Loop (PLL)" IEEE Wind turbine: Trans, power electronics, VOL. 24, NO. 4, APRIL 2009 [10] A. Petersson " Analysis, Modeling and Slip(Smax)=0.25, Control of Doubly-Fed Induction cut-in wind speed: 4 m/s, Generators for Wind Turbines", Ph.D. cut-out wind speed: 22 m/s, dissertation, Dept. of Energy and rated wind speed:12m/s, Environment, Univ. Chalmers, Goteborg, turbine rotor radius: 41.5m Sweden 2005 [11] E. Hau, Wind turbines. Berlin, REFERENCE Germany: Springer, 2006 [1] T. Ackermann, Wind Power in Power [12] F.B. Bianchi, H. De Battista, Wind Systems. New York, UK: John Wiley & Turbine Control Systems. Berlin, Sons, 2005. Germany: Springer, 2007 [2] R. Datta and V. T. Ranganathan, “A [13] F. Iov, A. D. Hansen, P. Sørensen, F. simple position sensorless algorithm for Blaabjerg, "Wind Turbine Blockset in rotor side field oriented control of wound Matlab Simulink". Aalborg University, rotor induction machine,” IEEE Trans. Denmark: March 2004 7