Modern Control Engineering

(Chris Devlin) #1
488 Chapter 7 / Control Systems Analysis and Design by the Frequency-Response Method

Nonminimum-Phase Transfer Functions. If, at the high-frequency end, the com-


puted phase lag is 180° less than the experimentally obtained phase lag, then one of the


zeros of the transfer function should have been in the right-half splane instead of the


left-halfsplane.


If the computed phase lag differed from the experimentally obtained phase lag by a


constant rate of change of phase, then transport lag, or dead time, is present. If we assume


the transfer function to be of the form


whereG(s)is a ratio of two polynomials in s, then


where we used the fact that constant. Thus, from this last equation, we


can evaluate the magnitude of the transport lag T.


lim


vSq

/G(jv)=


= 0 - T=-T


= lim


vSq

d


dv


C/G(jv)-vTD


lim


vSq

d


dv


/G(jv)e-jvT= lim


vSq

d


dv


C/G(jv)+ /e-jvTD


G(s)e-Ts


(a)

0


  • 20


20 log K


  • 40

    • 40




dB

v =K v =K

v in log scale

(b)

(c)

0


  • 20

    • 20

      • 20





  • 20

  • 40

  • 40

  • 40

  • 40


dB

v in log scale

0

dB

v in log scale

0

dB

v in log scale

0

dB

v in log scale

v = K v = K

Figure 7–87
(a) Log-magnitude
curve of a type 0
system; (b) log-
magnitude curves of
type 1 systems;
(c) log-magnitude
curves of type 2
systems. (The slopes
shown are in
dBdecade.)

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