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an investigation of dual stator winding induction machines

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Pole 1<br />

Pole 2<br />

Figure 10.3 Diagram <strong>of</strong> pole placement using Butterworth method<br />

ω0<br />

The zeros <strong>of</strong> tr<strong>an</strong>sfer function c<strong>an</strong> also greatly influence the system perform<strong>an</strong>ce. It is<br />

well known that when <strong>an</strong>y zero <strong>of</strong> a tr<strong>an</strong>sfer function <strong>of</strong> a system has a positive real part<br />

(the system is non-minimum phase), the closed-loop perform<strong>an</strong>ce is compromised as the<br />

right half-pl<strong>an</strong>e zero induces <strong>an</strong> additional phase shift <strong>of</strong> -180. The determination <strong>of</strong><br />

controller parameters should ensure the minimum phase system requirement.<br />

The design methodology <strong>of</strong> the Butterworth method requires that none <strong>of</strong> the terms in<br />

the denominator is missing. This becomes the limitation for the controller determination.<br />

The reason for this limitation is simple. For example, the second order Butterworth<br />

polynomial is given as:<br />

2<br />

2<br />

S + 2ω<br />

S + ω = 0<br />

(10.45)<br />

0<br />

0<br />

The absence <strong>of</strong> <strong>an</strong>y term in (10.45) leads to the conclusion that ω 0 has to be zero,<br />

which yields unreasonable controller parameters. On the other h<strong>an</strong>d, zero value for ω 0<br />

me<strong>an</strong>s that the poles <strong>of</strong> the controllers overlap the original point, which makes the system<br />

unstable for practical purposes.<br />

356<br />

o<br />

45

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