Page 349 - Modern Control Systems
P. 349

Section  5.6  The Steady-State  Error of  Feedback  Control  Systems  323


                                    tf(.v)  O — • •








                                                     (a)


                                           Controller          Process
                                  "^  E a(s)
                        «(.0                 G c{s)             0(5)            •  n.s)
                                   L

       FIGURE  5.18
       Closed-loop control
       system with unity
       feedback.                                     (b)



                       It  is the  form  of  the  loop  transfer  function  G c(s)G(s)  that  determines  the  steady-
                       state error. The loop transfer  function  is written in general form as

                                                              M
                                                           Kl[{s  +  zd
                                               G c(s)G(s)  = —f          ,                (5.24)
                                                           ^ri(*  +  Pk)
                                                             A- =  l
                       where  Y\.  denotes the product  of the factors  and n  ^  0, p k  #  0 for any 1  <  /  <  M
                       and i  <  k  ^  Q. Therefore, the loop transfer  function  as s approaches zero depends
                        on  the  number  of  integrations, N.  If  N  is  greater  than  zero,  then  lim  G c(s)G(s)
                        approaches infinity, and the steady-state error approaches zero. The number  of inte-
                       grations  is  often  indicated  by  labeling  a system  with  a type  number that  simply is
                       equal to N.
                           Consequently, for a type-zero system,  TV  =  0, the steady-state error is



                                                                                          (5.25)
                                         C-cc
                                              1  +  G c(0)G(0)      u     Q   •
                                                              l  + #11*//UP*
                                                                    /=1  k = l
                       The constant G c(0)G(0) is denoted by K„, the position error constant, and is given by



                                                   K p  =  lim  G C (J)G(J).
                                                        s—»0
   344   345   346   347   348   349   350   351   352   353   354