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The Stability of Linear Feedback Systems

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,<br />

5.6 Summary<br />

225<br />

2<br />

"<br />

06<br />

o<br />

o<br />

so 70<br />

100 126 ISO<br />

K<br />

Figure 5.8. <strong>The</strong> stable region.<br />

ell is equal to 23.8% <strong>of</strong> A, we require that Ka = 42. This can be satisfied<br />

the selected point in the stable region when K = 70 and a = 0.6, as shown in<br />

5.8. Of course, another acceptable design would be attained when K = 50<br />

G - 0.84. We can calculate a series <strong>of</strong>possible combinations <strong>of</strong> K and a that<br />

utisfy Ka = 42 that lie within the stable region, and all will be acceptable<br />

solutions. However, not all selected values <strong>of</strong> K and a will lie within the<br />

region. Note that K cannot exceed 126.<br />

Summary<br />

chapter we have considered the concept <strong>of</strong>the stability <strong>of</strong>a feedback cont)'Item.<br />

A definition <strong>of</strong>a stable system in terms <strong>of</strong>a bounded system response<br />

':'Ottined and related to the location <strong>of</strong> the poles <strong>of</strong> the system transfer fune­<br />

In the s-plane.<br />

<strong>The</strong> Routh-Hurwitz stability criterion was introduced and several examples<br />

~idered. <strong>The</strong> relative stability <strong>of</strong>a feedback control system was also con­<br />

• In terms <strong>of</strong>the location <strong>of</strong>the poles and zeros <strong>of</strong>the system transfer func­<br />

~ the s-plane. Finally, the determination <strong>of</strong> the roots <strong>of</strong> the c-haracteristie<br />

on was considered and the Newton-Raphson method was illustrated.<br />

• A sYStem has a characteristic equation 5 l + 3Ks l<br />

<strong>of</strong>K for a stable system.<br />

K :> 0.53<br />

+ (2 + K)s + 4 = O. Determine

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