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90   MECHATRONICS
                                           Im(G(j   ))ω                     Im(G(j   ))
                                                                                 ω
                                                                         1/GM
                                          1/GM

                                     –1
                                                                                            ω
                                                           ω
                                                       Re(G(j   ))     –1   PM < 0      Re(G(j   ))
                                     PM > 0


                                            (a)                                 (b)


                               1.1                                 dB

                               100
                               10                                  20
                                                                           1/GM
                                1                                   0
                                               1/GM        log ω                   0   1    2  log ω
                                                             10                                  10
                               0.1                                –20
                              0.01                                –40











                                                           log ω                               log ω
                                                             10                                  10
                               –90                                –90
                                       PM
                              –180                                –180
                                                                                    PM < 0
                              –270                                –270
                                            (c)                              (d)
                              FIGURE 2.34: Gain margin and phase margin measures in Nyquist plots (a and b) and Bode
                              plots (c and d).


                              another value, an n set of roots can be solved for every value of the parameter a .Ifweplot
                                                                                            i
                              the roots on the complex s-plane, we end up with the graphical representation of the locus
                              of the roots of the algebraic equation as one of the parameters in the equation varies. This
                              is the basic functionality of the root locus method. Clearly, this can be done numerically
                              by a computer algorithm.
                                   Let us consider the feedback control system shown in Figure 2.35. The closed loop
                              system transfer function is
                                                           y(s)   KG(s)
                                                              =                                  (2.94)
                                                           r(s)  1 + KG(s)
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