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The Stability of Linear Feedback Systems

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5.3 <strong>The</strong> Relative <strong>Stability</strong> <strong>of</strong> <strong>Feedback</strong> Control <strong>Systems</strong><br />

219<br />

"•<br />

,<br />

"<br />

"<br />

I<br />

• ,<br />

" "' ,,<br />

'.<br />

10<br />

Figure 5.6. Root locations in the s-planc.<br />

uation lie in the right half<strong>of</strong> the s-plane. However, if the system satisfies<br />

th_Hurwitz criterion and is absolutely stable, it is desirable to determine<br />

;ve srabilily; that is, it is necessary to investigate the relative damping <strong>of</strong><br />

root <strong>of</strong>the characteristic equation. Thc relative stability <strong>of</strong>a system may be<br />

as the property that is measured by the relative settling times <strong>of</strong>each root<br />

. <strong>of</strong>roots. <strong>The</strong>refore relative stability is represented by the real part <strong>of</strong>each<br />

Thus root'! is relatively more stable than the roots,,, 'I as shown in Fig.<br />

1be relative stability <strong>of</strong>a system can also be defined in terms <strong>of</strong> the relative<br />

coefficients f <strong>of</strong> each complex root pair and therefore in terms <strong>of</strong> the<br />

<strong>of</strong>response and overshoot instead <strong>of</strong>settling time.<br />

Hence the investigation <strong>of</strong> the relative stability <strong>of</strong> each root is clearly necesbecause,<br />

as we found in Chapter 4, the location <strong>of</strong> the closed-loop poles in<br />

'"Plane determines the performance <strong>of</strong> the system. Thus it is imperative that<br />

ioe:xamine the characteristic equation q(s) and consider several methods for<br />

determination <strong>of</strong> relative stability.<br />

use the relative stability <strong>of</strong> a system is dictated by the location <strong>of</strong> the<br />

<strong>of</strong>the characteristic equation, a first approach using an s-plane formulation<br />

extend the Routh-Hurwitz criterion to ascertain relative stability. This can<br />

ply accomplished by utilizing a change <strong>of</strong> variable, which shifts the s-plane<br />

in order to utilize the Routh-Hurwitz criterion. Examining Fig. 5.6, we notice<br />

a ~ft <strong>of</strong> the vertical axis in the s-plane to -(11 will result in the roots 'I, 'I<br />

on the shifted axis. <strong>The</strong> correct magnitude to shift the vertical axis<br />

be btained on a trial-and-error basis. <strong>The</strong>n, without solving the fifth-order<br />

iaI q(s), one may determine the real part <strong>of</strong> the dominant roots,,, 'I'<br />

Example 5.6 Axis shift<br />

the simple third-order characteristic equation<br />

q(s) ~ s' + 4s' + 6s + 4. (5.17)<br />

Y! one might shift the axis other than one unit and obtain a Routh-Hurwitz<br />

\\>tth~ut a zero occurring in the first column. However, upon setting the<br />

vanable Sn equal to s + I, we obtain<br />

"<br />

(5.18)

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