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320              Chapter 5  The Performance of  Feedback Control Systems

                               The  time  constant  for  the  exponential  decay  is  T =  l/(£&>„)  in  seconds. The
                            number  of cycles of the damped  sinusoid during one time constant is

                                            (cycles/time)  X T =
                                                              27r£&)„  27rg(o n  2TT£

                            Assuming that the response decays in n visible time constants, we  have

                                                       cycles visible  =  -—-.                 (5.19)

                            For  the  second-order  system, the  response  remains  within  2%  of  the  steady-state
                            value after  four  time constants  {AT). Hence, n  =  4, and

                                                                         2 112
                                                            4(3   4(1  -  C )  .,  0.55
                                             cycles visible  =  —— =  ——     =* —7-            (5.20)
                                                           ITTC,     2TTQ       C
                            for  0.2  <  £ <  0.6.
                               As  an  example, examine  the  response  shown  in  Figure 5.5(a) for  £ =  0.4. Use
                            y{t)  =  0 as the first  minimum point  and count  1.4 cycles visible  (until the response
                            settles with 2% of the final value).Then  we estimate

                                                         0.55    0.55  nf%n
                                                        cycles   1.4

                            We can use this approximation  for systems with dominant complex poles so that
                                                                  (ol
                                                     T(s)
                                                            S  +  2t,03 nS  +  (*) n .2'

                            Then we are able to estimate the damping ratio £ from the actual system response of
                            a physical system.
                               An alternative method  of estimating £ is to determine the percent overshoot  for
                            the  step response  and  use Figure  5.8 to  estimate  £. For  example, we determine  an
                            overshoot  of 25%  for  £ =  0.4 from  the response  of Figure 5.5(a). Using Figure 5.8,
                            we estimate that £  =  0.4, as expected.


           5.5  THE s-PLANE   ROOT   LOCATION AND THE TRANSIENT        RESPONSE

                            The transient response of a closed-loop feedback control system can be described in
                            terms  of the location  of the poles  of  the transfer  function. The closed-loop  transfer
                            function  is written  in general as


                                                    ^    R(s)       A(5)    '

                            where A (s)  =  0 is the characteristic equation  of the system. For the single-loop sys-
                            tem  of  Figure  5.4,  the  characteristic  equation  reduces  to  1 +  G(s)  =  0.  It  is  the
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