Page 41 - Servo Motors and Industrial Control Theory -
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2.6   Nyquist Plot                                              33


            Fig. 2.11   Nyquist plot for   1               1
            first order lag open loop
            transfer function
                                                          0.5


                                    Imag
                                            –1      –0.5       0    0.5      1


                                                         –0.5


                                     –1                   –1

                                            –1             Real              1


              Fig. 2.12   A unity feedback
            control system with second                   1
            order Lag open loop transfer   x  +     1       ξ              y
                                                       2
            function                                   s  – 2  s + 1
                                                  (ω ) 2   ω n
                                   –                n








                                              −
                                               1
                                       ϕ =− tan (τω )                    (2.16)
            The plot of frequency response of open loop transfer function, which is known as
            Nyquist plot is shown in Fig. 2.11. It can be seen that for first order lag transfer
            function the locus is a semi-circle. When ω = 0 the plot starts at point 1 and for
            frequency of large value the plot ends at zero indicating that this type of transfer
            function the system remains stable. The response to a unit step input is always over-
            damped. This is shown in Fig. 2.11.
              The Nyquist plot is located in the first quadrant measuring from the real axis
            clockwise showing that this kind of system is always stable.
              A system  with  a  second  order  lag  open  loop  transfer  function  is  shown in
            Fig. 2.12. It is assumed a unity gain and unity feedback.
              It was shown that the amplitude ratio and phase angle are given as
                                              1
                                   M =              2  2
                                             2 ) +
                                        (1 −  ω 2 2  4ζω                 (2.17)
                                            ω n    ω 2
                                                    n
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