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70    Chapter  Two

               also known as the characteristic equation, determines its tracking
               performance, disturbance rejection, and stability properties. Several
               design criteria can be defined for the loop gain L(s):

                  1.  Disturbance rejection: From Eq. (2.83) we can observe that
                      improved suppression of the negative influence of distur-
                      bances W(s) on the performance of the controlled system is
                      obtained when

                                      |(Ljω>> 1                     (2.88)
                                          )|
                      The larger | (Ljω )|, the better the influence of  W(s) will be
                      attenuated.
                  2.  Noise filtering: From Eq. (2.84) we can derive that the influ-
                      ence of sensor noise V(s), which contaminates the measured
                      output signal Y (s), will be minimized when
                                   m
                            |( ) ( )|<<  1   or  |(jω )|<< 1        (2.89)
                                  s
                                C
                            Gs
                                                L
                                       Hs
                                      |( )|
                       The better the sensor noise V(s) is filtered out, the more accu-
                      rate the measured signal Y (s) becomes.
                                            m
                         Apart from sensor noise, the measured signal Y (s) can also
                                                               m
                      be contaminated by unknown disturbance signals, generated
                      by unmodeled high-frequency dynamics of the system. The
                      better these are filtered out, the less influence these will have
                      on the controlled output Y(s). Badly filtered unmodeled high-
                      frequency dynamics can distort  Y (s) so severely that the
                                                    m
                      feedback system becomes unstable. This phenomenon is
                      called observation spillover.
                  3.  Reference tracking: From Eq. (2.81), the conditions can be calcu-
                      lated for which the output signal Y(s) will follow the reference
                      signal R(s) accurately:

                               | (Gjω )|≈ 1  or  | (jω )|>> 1       (2.90)
                                             L
                                 c
                  4.  Input limitation: The actuator signal,  U(s), is sometimes
                      restricted (e.g., maximal available power, or maximal actua-
                      tor speed); therefore, U(s) has to be kept as small as possible.
                      From Eq. (2.85) we can derive that this is obtained when


                                Cj ( ω )
                                         Cj ) ( ω
                               1+  Lj ( ω )  = |( ω  S j )|<<  1    (2.91)
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