Page 270 - Modern Control Systems
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244              Chapter 4  Feedback Control System Characteristics

                                •
                             300
                           •3       V .  /-
                           S  200    ^  X«%,,
                            eed   />
                           CO  100  vf ^
          FIGURE 4.8           0                    ^ — •
          Motor                        10     20     30
          speed-torque                 Motor torque (N-m)
          curves.

                              The change in speed due to the load disturbance is then

                                                                   1
                                            £"(5)  =  -co(s)  =              Us).             (4.26)
                                                           Js  + b  +  K mK b/R a
                           The  steady-state  error  in  speed  due  to  the  load  torque, T<i(s)  = D/s,  is  found  by
                           using the final-value  theorem. Therefore, for  the open-loop system, we have

                                                                         1          D
                                       \im E(t)  =  musECs)  =  lim s—  :  „  „  ,„  —
                                            v
                                       ,-,00  '  ,_»o  v  }  *-o  Js  +  b       \  s
                                                      D                + K mK b/R a
                                                              =  -wo(oo).                     (4.27)
                                                 b  +  K mK b/R a
                              The closed-loop speed control system is shown in block diagram form in Figure 4.9.
                           The  closed-loop  system  is  shown  in  signal-flow  graph  and  block  diagram  form  in
                           Figure 4.10, where G x(s)  = K aK m/R a,  G 2(s)  =  1/(/5  +  b), and H(s)  = K t  +  K b/K a.
                           The error, E(s)  =  —<o(s),  of the closed-loop system  of Figure 4.10 is:
                                                                 G 2(s)
                                            E(s)  =  -<o(s)  =               Us)-             (4.28)
                                                           1  +  G l(s)G 2(s)H(s)
                           Then, if GiG 2H(s)  is much greater than 1  over the range  of s, we obtain the approx-
                           imate result

                                                    E(s)*           Us).                     (4.29)
                                                           G^His)



                                                                        TM)

                                 + ^  EjLs)
                           R(s)   + 0                                                        +>  (O(S)





          FIGURE  4.9
         Closed-loop  speed
         tachometer control
         system.
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