Page 269 - Modern Control Systems
P. 269

Section 4.4  Disturbance Signals in a Feedback Control System       243
                         radar  antennas  are  subjected  to  wind  gusts; and  many  systems generate  unwanted
                         distortion  signals due to nonlinear  elements. The benefit  of feedback  systems is that
                         the effect  of distortion, noise, and unwanted disturbances can be effectively  reduced.

                         Disturbance   Rejection
                         When R(s)  =  N(s)  =  0, it follows from Equation  (4.4) that
                                                                     G(s)
                                          E(s)  =  S(s)G(s)T d(s)          Us)-
                                                                   1  +  L(s)
                         For a fixed  G(s) and a given 7^(^), as the loop gain L(s)  increases, the effect  of T d(s)
                         on the tracking error decreases. In other words, the sensitivity function  S(s) is small
                         when the loop gain is large. We say that large loop gain leads to good disturbance re-
                         jection. More precisely, for  good disturbance  rejection, we require a large loop gain
                         over the frequencies  of interest  associated with the expected disturbance signals.
                             In  practice, the  disturbance  signals  are  often  low  frequency.  When  that  is  the
                         case, we say that we want the loop gain to be large at low frequencies. This is equiv-
                         alent  to  stating that  we want to  design  the  controller  G c(s)  so that  the  sensitivity
                         function  S(s) is small at low frequencies.
                             As a specific example of a system with an unwanted disturbance, let us consider
                         again the speed control system for  a steel rolling mill. The rolls, which process steel,
                         are  subjected  to  large  load  changes  or  disturbances. As  a steel bar  approaches  the
                         rolls (see Figure 4.6), the rolls are empty. However, when the bar engages in the rolls,
                         the load on the rolls increases immediately to a large value. This loading effect  can be
                         approximated  by a step change of disturbance torque. Alternatively, the response can
                         be seen from  the speed-torque curves of a typical motor, as shown in Figure 4.8.
                             The  transfer  function  model  of  an  armature-controlled  DC motor  with  a load
                         torque  disturbance  was  determined  in  Example  2.5  and  is  shown  in  Figure  4.7,
                         where it  is assumed  that  L a  is negligible. Let  R(s)  =  0 and  examine E(s)  =  — a)(s),
                         for a disturbance T (!(s).


                                                         Rolls
                                                        0
                                     Steel bar
                              AAftM^

        FIGURE 4.6                                      ©
                                     Conveyor
        Steel rolling mill.
                                                         Disturbance



                                          1  W        r„,(.*)  t  T L(S)
                         W                                                   t  »  <o(s)
        FIGURE 4.7                                                   Js  + b     Speed
        Open-loop speed
        control system
        (without tachometer          Motor back electromotive  force
        feedback).
   264   265   266   267   268   269   270   271   272   273   274