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318              Chapter 5  The Performance  of  Feedback  Control Systems






                            L, >  0.707
                              and






           FIGURE 5.15
           Specifications and
           root locations on
           the s-plane.


                            we require that  the real part  of the complex poles of  T(s)  be

                                                            fan  ^  I-
                            This  region  is  also  shown  in  Figure  5.15. The  region  that  will  satisfy  both  time-
                            domain requirements  is shown cross-hatched on the s-plane  of Figure 5.15.
                               When   the  closed-loop  roots  are  r\  =  — 1 +  /1  and  ?\  =  - 1 - ) 1 ,  we  have
                              =  4 s and  an overshoot  of 4.3%. Therefore,  £  =  l / v 2  and  co t,  =  l/£  =  V  2. The
                            T s
                            closed-loop transfer  function  is
                                                 G(s)          K               0)7,
                                        T(s)               2             2
                                                                                      2'
                                               1  +  G(s)  s  +  ps  +  K  s  +  2fa ns  + (of,
                                                      2
                            Hence, we require  that  K  =  w , =  2 and p  -  2£io„ =  2. A  full comprehension  of the
                            correlation between  the closed-loop root location  and the  system  transient  response
                            is important to the system analyst and designer. Therefore, we shall consider the mat-
                            ter more completely in the following  sections.  •

                            EXAMPLE  5.2  Dominant poles of  T(s)

                            Consider  a system with  a closed-loop  transfer  function

                                                                   — (s  +  a)
                                             Y{s)
                                                  =  T{s)  =
                                                                           2
                                             R(s)          (s 2  +  2(a> Hs  +  <o „)(\  +  rs)
                            Both  the zero  and  the  real pole  may  affect  the  transient  response.  If  a  »  fan  a n  d
                            T  «  \/fa u,  then the pole and zero will have  little  effect  on the step response.
                               Assume  that  we have
                                                             62.5(4'  +  2.5)
                                                 T(s)  =  2
                                                        (,v  +  6A-  +  25)(s  +  6.25)
                            Note  that  the DC  gain  is equal  to  1 (T(0)  =  1), and  we  expect  a zero  steady-state
                            error  for  a  step  input. We  have  £a>„ =  3, T  =  0.16,  and  a  =  2.5. The  poles  and  the
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