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268              Chapter 4  Feedback  Control System  Characteristics

           4.9  CONTROL SYSTEM CHARACTERISTICS           USING CONTROL      DESIGN SOFTWARE

                            In  this section, the advantages  of feedback  will be illustrated  with two examples. In
                            the  first  example, we will introduce  feedback  control  to  a speed  tachometer  system
                            in  an  effort  to  reject  disturbances. The  tachometer  speed  control  system  example
                            can be found  in Section 4.5. The reduction  in system sensitivity to process variations,
                            adjustment  of  the  transient  response,  and  reduction  in  steady-state  error  will  be
                            demonstrated  using the English  Channel boring machine example  of Section 4.8.

                            EXAMPLE  4.5  Speed control system

                            The  open-loop  block  diagram  description  of  the  armature-controlled  DC  motor
                            with  a load  torque  disturbance  T d($)  is shown  in Figure 4.7. The values for  the vari-
                            ous parameters (taken from Figure 4.7) are given in Table 4.3. We have two inputs to
                            our system, V a(s)  and  T (l(s).  Relying on the principle  of superposition, which  applies
                            to our linear system, we consider  each input  separately. To investigate  the  effects  of
                            disturbances  on  the  system,  we  let  V a(s)  =  0  and  consider  only  the  disturbance
                            Td(s).  Conversely, to investigate  the response  of the  system  to a reference  input, we
                            let  T d(s)  =  0 and consider  only the input  V a(s).
                               The  closed-loop  speed  tachometer  control  system  block  diagram  is  shown  in
                            Figure 4.9. The values for  K a  and  K t  are  given in Table 4.3.
                               If  our  system  displays  good  disturbance  rejection,  then  we  expect  the  distur-
                           bance  T d(s)  to have  a small  effect  on  the  output  o){s). Consider  the  open-loop  sys-
                            tem in Figure 4.11 first. We can compute the transfer  function  from  Tj(s)  to (o(s) and
                            evaluate  the  output  response  to  a  unit  step  disturbance  (that  is, T (l(s)  =  1/s).  The
                            time response to a unit step disturbance  is shown in Figure 4.29(a). The script  shown
                           in Figure 4.29(b) is used to analyze the open-loop speed tachometer  system.
                               The open-loop  transfer  function  (from  Equation  (4.26)) is
                                                    <o(s)     - 1
                                                    W    =  27TT^ =      ^

                           where sys_o represents the open-loop transfer function  in the script. Since our  desired
                           value  of (o(t) is zero (remember  that  V a(s)  =  0), the steady-state error  is just the  final
                           value  of (o(t), which  we denote  by (o 0(t) to indicate open-loop. The steady-state  error,
                           shown  on  the  plot  in  Figure  4.29(a),  is  approximately  the  value  of  the  speed  when
                           /  =  7 seconds. We can obtain an approximate  value  of the steady-state error  by look-
                           ing at the last value in the output vector y 0, which  we computed  in the process of  gen-
                           erating the plot  in Figure 4.29(a). The approximate steady-state value  of (o (, is
                                                  <o„(oo)  «  (0,,(7) =  -0.66  rad/s.

                           The plot  verifies  that we have reached  steady state.



                            Table 4.3  Tachometer Control System  Parameters

                            R a      Km            J           b            K5         Kg      K t
                            i n      lONm/A        2kgm 2      0.5 Nms      0.1 Vs     54       lVs
   289   290   291   292   293   294   295   296   297   298   299