Page 90 - Modern Control Systems
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64              Chapter 2  Mathematical  Models of Systems













                                                                              •  Time


                                                        Underdamped case
           FIGURE 2.12
           Response of the
           spring-mass-
           damper system.


                           where  6  =  cos  l  £. Therefore,

                                                             yo   :eJ(ir/2-0)
                                                     ko  =                                    (2.36)
                                                         2V1 -  ('
                                                    2
                           Finally, letting p  =  V l  -  £ , we find  that
                                              1
                                      y{t)  =  k^ '  +  k 2e^
                                                yo    ( eiifi-TTi2) e-c^ ej^,fit  +  e/(V2-0) e-w e-M,/3r\
                                            2V1 -   i 1
                                                yo    fw              2
                                                                           6).
                                                                        +
                                                                .
                                                            v~„
                                              r     = :e- '''sin(ft> nVl .  -  £ f - • - , .  (2.37)
                                                                     ,
                                             viw   2
                           The solution, Equation (2.37), can also be obtained using item 11 of Table 2.3. The tran-
                           sient  responses  of  the  overdamped  (£  >  1)  and  underdamped  (£  <  1)  cases  are
                           shown in Figure 2.12. The transient response that occurs when t,  <  1 exhibits an oscil-
                           lation in which the amplitude decreases with time, and it is called a damped oscillation.
                               The relationship between  the s-plane  location  of the poles and zeros and  the
                           form  of  the  transient  response  can  be  interpreted  from  the  s-plane  pole-zero
                           plots. For  example, as seen  in Equation  (2.37), adjusting  the  value  of  £G>„ varies
                           the  e~^ J  envelope, hence  the  response  y(t)  shown  in Figure  2.12. The  larger  the
                           value  of  £,oi n,  the  faster  the  damping  of  the  response, y(t).  In  Figure  2.9, we  see
                                                                                                  2
                                                                                           V
                           that  the  location  of  the  complex  pole  ^  is  given  by  s^  =  —£o) n +  j(o„ i  -  c .
                           So, making  £a) n larger  moves  the pole  further  to the  left  in the 5-plane. Thus, the
                           connection  between  the location  of the pole  in the 5-plane  and the step  response
                           is  apparent—moving  the  pole  ^  farther  in  the  left  half-plane  leads  to  a  faster
                           damping  of  the  transient  step  response.  Of  course,  most  control  systems  will
                           have more  than  one  complex pair  of  poles, so  the  transient  response  will be  the
                           result  of the contributions  of all the poles. In fact, the magnitude  of the  response
                           of  each  pole,  represented  by  the  residue,  can  be  visualized  by  examining  the
                           graphical  residues  on  the  s-plane.  We  will  discuss  the  connection  between  the
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