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Appendix B                                                      199

               find the range of the proportional gain that is effective in control of the eigen-
               values. It might be in the range of smaller than one, greater than one, thousands
               or millions. With a few trials you should be able to find the interesting ranges.
               Plot the root locus as gain changes. Select quite a large gain and introduce the
               derivative gain for each of the values of gain. The derivative term must increase
               the damping of some of the eigenvalues. Therefore, you should be able to find
               a trend when both the proportional gain and derivative gains are changed. Add
               the integral term and change its value for several values of proportional and
               derivative gain. Observe the root locus and find the most suitable parameters
               of PID gains. For the best performance, you should consider the transient re-
               sponse, steady state error for step input and speed of response. You should
               compare the complexity of such a system when solved with classical feedback
               control theory or with state space approach.
            25.  It would be interesting to compare the capability of state variable control and
               classical feedback control theory. Consider the problem 24. Instead of PID con-
               trol strategy, it is required to use a state variable feedback control strategy. This
               is shown below. An integrator has been added to make sure that zero steady
               state error is achieved.


                    θ i  +     1                 1                      θ o
                       -        s       s  + 120s +14500s + 250000
                                        3



                                                 K

                                              Gain Vector  State Variables

               Transform the above open loop transfer function to state space form. Check the
               controllability of the system. If controllable, design the state variable feedback
               control strategy and take the gain vector as negative feedback as shown in the
               above diagram. Select the gains such that all four eigenvalues move to the fol-
               lowing position,
                                     s :=− 50 50i+
                                     1
                                     s :=− 50 50i−
                                      2
                                     s :=− 100 100i+
                                      3
                                     s :=− 100 100i−
                                      4
               The above eigenvalues have been chosen arbitrary which gives two second
               order oscillatory motions with a damping ratio of 0.7. The slower eigenvalues
               of course dominate the response.
               Determine the steady state error to show that indeed it is zero. Compare the
               result of this problem with the previous problem and discuss the advantage and
               disadvantage of state variable feedback control strategy.
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