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0066_Frame_C20.fm  Page 105  Wednesday, January 9, 2002  1:44 PM










                                                                               Load
                                                                            T
                                                          bs Magnetic Axis   L
                                                                           B m
                                                                   as′  ω r  T ,  e
                                                                     Stator  Quadrature Magnetic Axis
                                 u cs  +             u bs  +                   ω
                                        r           r       cs   Rotor    bs
                                        s            s                            t
                                                                                     d
                                            L ss  L ss                          θ = ∫ ω (τ ) τ + θ 0
                                                                                  0 t
                                       i             i bs
                                       cs
                                                                               as Magnetic Axis
                                               N s
                                               L
                                                ss
                                           i               bs′             cs′
                                           as
                                               r s
                                                                   as
                                                    cs Magnetic Axis     Direct Magnetic Axis
                                            u as  +
                       FIGURE 20.130  Three-phase synchronous reluctance micromotor.
                       Three-Phase Synchronous Reluctance Micromotors: Modeling and Analysis
                       Our goal is to address and solve a spectrum of problems in analysis, modeling, and control of synchronous
                       reluctance micromachines. The electromagnetic features must be thoroughly analyzed before attempt to
                       control micromotors. In fact, electromagnetic features significantly restrict the control algorithms to be
                       applied. Depending upon the conceptual methods employed to analyze synchronous reluctance micro-
                       machines, different control laws can be designed and implemented using ICs. Analysis and control of
                       synchronous reluctance micromotors can be performed using different modeling, analysis, and optimi-
                       zation concepts. Complete lumped-parameter mathematical models of synchronous reluctance micro-
                       motors in the machine (abc) and in the quadrature, direct, and zero (qd0) variables should be developed
                       in the form of nonlinear differential equations. In particular, the circuitry lumped-parameters mathe-
                       matical model is found using the Kirchhoff’s voltage law. We have, see Fig. 20.130,

                                                     u abcs =  r s i abcs +  dy abcs
                                                                  --------------
                                                                   dt

                       where u as , u bs , and u cs  are the phase voltages; i as , i bs , and i cs  are the phase currents; ψ as , ψ bs , and ψ cs  are the
                       flux linkages,


                                                                      r s 00
                                                y abcs =  L s i abcs ,  r s =  0 r s 0

                                                                      00 r s

                                                                                            
                                                                   
                               L ls +  L m –  L ∆m cos ( 2q r )  –  1  L ∆m cos 2 q r –  1    –  1  L ∆m cos 2 q r +  1  
                                                                                --L m –
                                                                        --p
                                                                                                --p
                                                       --L m –
                                                       2               3      2              3 
                                           
                                                                    
                        L s =  –  1  L ∆m cos 2 q r –  1    L ls +  L m –  L ∆m cos 2 q r –  2    –  1  L ∆m cos 2 q r +  p)
                                                                                             (
                                                                                --L m –
                                                                        --p
                                                --p
                               --L m –
                               2               3                     3      2
                               1               1      1                                       2  
                                                                    (
                             –  --L m –  L ∆m cos 2 q r +  --p  –  --L m –  L ∆m cos 2 q r + p)  L ls +  L m –  L ∆m cos 2 q r +  --p
                                           
                                                                                             
                               2                3      2                                        3 
                                                    -- L md –(
                            -- L mq +(
                       L m =  1    L md )  and  L ∆m =  1  L mq )
                            3                       3
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