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314              Chapter  5  The  Performance  of  Feedback  Control  Systems

                                                               '
                              1.6  o)„  =  lOrad/s
                              1.4  1        /~   >
                                                  rV°»  =  1 rad/s
                              1.2   1  i  ^ . / .  i  \             .  _.  :. .  ,
                            <D    1  /i\  /
                           "2  i n
                            §  0.8
                                   V   J  V
                           <
                              0.6
                                    "j7"'1  ""':                        j
                              0.4
                                    /    i
          FIGURE  5.10        0.2                 i                     1
          The step response       /:   -f ^
          for l  =  0.2 for    0                  '                     i
          oj n =  1  and                          4   5   6                 10
          u> n  =  1 0 .                            Time (s)





                               1.0
                                  ^ = OJ/ /f=l
                              0.8
                             alitude   p                  <w„  =  5 rad/s


                            1
                              0.4


                              0.2
          FIGURE  5.11
          The step response    0
          for a) n =  5 with           0.5    1.0    1.5   2.0    2.5    3.0
          £  =  0.7 and (=  1.                     Time (s)


          5.4  EFFECTS OF A THIRD     POLE AND A ZERO ON THE       SECOND-ORDER
              SYSTEM    RESPONSE

                           The  curves  presented  in  Figure  5.8  are  exact  only  for  the  second-order  system  of
                           Equation  (5.8). However, they provide  a remarkably  good  source  of data  because
                           many  systems  possess  a dominant pair  of roots, and  the  step response  can  be esti-
                           mated  by utilizing Figure 5.8. This approach, although an approximation, avoids the
                           evaluation  of the inverse Laplace transformation  in order to determine the percent
                           overshoot  and  other  performance  measures. For example, for  a third-order  system
                           with a closed-loop transfer  function

                                                                  1
                                                 T(s)                                         (5.18)
                                                        (r  +  2£s +  l)(ys  +  1)
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