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Electric Generators and their Control for Large Wind Turbines               223


                                        Machine-side   Grid-side
                       Blade             converter     converter
                                                 DC link
                       Gearbox                                                Grid
                               CRIG
                                                                 Filter

                             ω r
                                   i abcs  v abcs  PWM  V DC  PWM
                                                                 i abc
                                                                 v abc
                                   P* grid     Control center
                                    *
                       Turbine angle  Q grid                     V* DC

            FIGURE 9.12  CRIG controlled to the grid through an AC–DC–AC converter.



            a notably lower stress on the wind tower. The stall control may have an advantage in terms of lower
            complexity and drive cost but requires the CRIG to be designed for maximum power at lower speed
            and higher torque.

            9.3.2  CRIG Circuit Model and Performance

            In order to model the CRIG, the space phasor of the model is considered for a three-phase CRIG in
            general coordinates (for motor mode consideration of signs) [3]:

                           dψ s  =  R is − V s +  jωψ ;  ψ =  L is +  L ir;  L s =  L sl +
                            dt    s         b  s  s   s    m            L m           (9.18)
                           dψ r  =  R ir − (       ψ  =  L  L             L
                                      j ω
                                             r r
                                                r
                            dt    r      b ω− )ψ ;  r   r r i +  m s i ;  r L =  rl L +  m
                                       3         *
                                   T e =  p 1 Im ψ s ( )
                                                I s < 0 forgenerating
                                       2
              In dq synchronous coordinates (ω  = ω ), for rotor flux orientation, (9.18) becomes
                                             1
                                         b
                   ( R s +− +  j ) ) − V s = − (  jω 1 +  p)  L m  ψ ;  ψ s  =  Li sd +  jL i q ;  is =  i d + jji q
                       (
                         p
                                    is
                             ω 1
                                L sc
                                                                      sc
                                                        r
                                                    L r
                                                                                      (9.19)
                                        R r        3
                     L m          L m                    (   L sc)
                                                                     ω
                                      p
                           
                   R r  is =−  jSω 1  −+     ψ ;  T e =  p L s −  ii ; ω 1 =  ω + S ω 1
                                                                           r
                                                        1
                                                                 dq
                                              r
                      L r        L r    L r        2
            where i , i  are stator current components in the rotor flux coordinates. The vector (space phasor)
                  d
                    q
            diagram for the steady state is illustrated in Figure 9.13.
              Also, for steady state,
                                V s =  IR s +  jωψ ;  ψ r =  L i d ;  i q = − Sω 1  L r  i d
                                            1
                                     s
                                                      m
                                              s
                                                                   R r                (9.20)
                                            0  =  R r ir +  jSωψ r
                                                        1
              In rotor flux coordinates, i s = i d +  ji q ; ψ r  = ψ dr ; ψ qr = 0.
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