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278              Chapter 4  Feedback  Control System  Characteristics

                               The  loop  gain  L(s)  =  G c(s)G(s)  plays  a  fundamental  role  in  control  system
                            analysis. Associated  with  the  loop  gain  we  can  define  the  sensitivity  and  comple-
                            mentary  sensitivity functions  as
                                                        1        . - -     L(s)
                                              S(s)            and  C(s)  =
                                                     1  +  L(s)          1  +  L(sY
                            respectively. The tracking error  is given  by
                                           E(s)  =  S(s)R(s)  -  S(s)G(s)T d(s)  +  C(s)N(s).
                            In order  to minimize the tracking error, E(s), we desire  to make  S(s) and  C(s) small.
                            Because  the  sensitivity  and  complementary  sensitivity  functions  satisfy  the  con-
                            straint

                                                        S(s)  +  C(s)  =  1,
                            we  are  faced  with  the  fundamental  trade-off  in  control  system  design  between
                            rejecting  disturbances  and reducing sensitivity to plant  changes on the one  hand,
                            and  attenuating measurement  noise on the other  hand.
                               The  benefits  of feedback  can  be illustrated  by considering  the system  shown  in
                            Figure 4.38(a). This system can be considered  for  several values  of gain K. Table  4.5
                            summarizes  the  results  of  the  system  operated  as  an  open-loop  system  (with  the
                            feedback  path  disconnected)  and  for  several  values  of  gain,  K, with  the  feedback
                            connected. It  is clear  that  the  rise  time  and  sensitivity  of the  system  are reduced  as





                                 R(s)                                       **  Y(s)



                                                        (a)

                                1.40






                                                                                K=  1.0
                           e(t)
                                                                                K=  10


           FIGURE  4.38
           (a) A single-loop
           feedback control
           system, (b) The
           error response for a
           unit step
           disturbance when
           R(s)  =  0.
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