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222              Chapter 3  State Variable  Models

                  = 0.5.  (a)  Determine  the  closed-loop  transfer
               K y                                           (a)  Determine  a state variable model.
               function                                      (b)  Determine  $(0, the state transition matrix.
                              Tis)  (o(s)                P3.13  Consider  again  the  RLC  circuit  of  Problem
                                    = m                      P3.1  when  R  =  2.5, L  =  1/4.  and  C  =  1/6.  (a)  De-
               (b) Determine  a state variable representation, (c) De-  termine whether the system  is stable by finding  the
               termine the characteristic equation obtained  from  the  characteristic  equation  with  the  aid  of  the  A  ma-
               A matrix.                                     trix.  (b)  Determine  the  transition  matrix  of  the
                                                             network,  (c) When  the initial inductor  current  is 0.1
           P3.10  Many control  systems  must  operate  in  two  dimen-  amp,  v c(0)  = 0,  and  v(t)  = 0,  determine  the  re-
               sions, for  example, the  x-  and  the  y-axes.  A  two-axis  sponse  of  the  system,  (d)  Repeat  part  (c)  when  the
               control system is shown in Figure P3.10, where a set of   initial  conditions  are  zero  and  v(t)  =  E,  for  t  >  0,
               state variables is identified.The  gain of each axis is Ki   where  E is a constant.
               and  K 2,  respectively, (a)  Obtain  the  state  differential
               equation,  (b)  Find  the  characteristic  equation  from  P3.14  Determine a state variable representation for a sys-
               the  A  matrix,  (c) Determine  the  state  transition  ma-  tem with  the transfer  function
               trix for  Ki  =  1 and K 2  = 2.
                                                                                   s  + 50
           P3.ll  A system is described by                         =  T(s)  =  A  3    2
                                                               R(s)        s  +  12s  +  IO5  +  34s  + 50'
                             x  =  Ax  +  Bu
               where                                     P3.15  Obtain  a block diagram  and  a state variable repre-
                                                             sentation  of this system.
                             1  -2~     V
                       A  =  2     ,B  =  u                       y(s)            U(s  +  4)
                           L   -3 J     L J                           =     =
                                                                  R(s)   ^    s 3  +  io.v 2  +  31s  +  16'
               and  X](0)  =  x 2(0)  =  10.  Determine  x {(t)  and  x 2(t).  P3.16  The dynamics  of a controlled  submarine  are  signifi-
           P3.12  A system is described by its transfer  function  cantly  different  from  those  of  an  aircraft,  missile,  or
                                                            surface  ship. This  difference  results  primarily  from
                     Y(s)  _         8(5  +  5)
                           T(s)  =                           the moment  in  the vertical plane due  to  the  buoyancy
                     R~(s)                                  effect. Therefore, it is interesting to consider the control




                            R.O—+                                   +—Or,



                            K2O                                     "*—0 2



                                                   (a)





                                                                    •  y,(s)




                                                                 1—*-  >Uv)
           FIGURE  P3.10
           Two-axis system.
           (a) Signal-flow
           graph, (b) Block
           diagram model.                          (b)
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