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an investigation of dual stator winding induction machines

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K <strong>an</strong>d K iqs1<br />

are the controller parameters for q-axis current controller), the tr<strong>an</strong>sfer<br />

pqs1<br />

functions <strong>of</strong> the state variables are:<br />

V<br />

V<br />

λ<br />

λ<br />

λ<br />

λ<br />

I<br />

I<br />

I<br />

I<br />

2<br />

dc<br />

* 2<br />

dc<br />

qr1<br />

*<br />

qr1<br />

dr1<br />

*<br />

dr1<br />

qs1<br />

*<br />

qs1<br />

ds1<br />

*<br />

ds1<br />

=<br />

=<br />

=<br />

1 2<br />

CS<br />

2<br />

S<br />

S<br />

2<br />

2<br />

⎛<br />

+ ⎜ K<br />

⎝<br />

K<br />

pdc<br />

⎛ 1<br />

+ ⎜<br />

⎝ R<br />

K<br />

K<br />

⎛<br />

+ ⎜ K<br />

⎝<br />

pqr1<br />

pqr1<br />

pdr1<br />

pdr1<br />

L<br />

S + K<br />

+ K<br />

S + K<br />

r<br />

+<br />

L<br />

r<br />

+<br />

L<br />

r1<br />

r1<br />

S + K<br />

r1<br />

r1<br />

idc<br />

pdc<br />

iqr1<br />

⎞<br />

⎟<br />

⎟S<br />

+ K<br />

⎠<br />

⎞<br />

⎟<br />

⎟S<br />

+ K<br />

⎠<br />

idr1<br />

⎞<br />

⎟<br />

⎟S<br />

+ K<br />

⎠<br />

iqr1<br />

idr1<br />

idc<br />

298<br />

(8.41)<br />

(8.42)<br />

(8.43)<br />

K pqs1S<br />

+ Kiqs1<br />

= (8.44)<br />

2 ⎛ K pqs1<br />

r ⎞ K<br />

1<br />

iqs1<br />

S + ⎜ + S +<br />

Lσ<br />

1 L ⎟<br />

⎝<br />

σ1<br />

⎠ Lσ<br />

1<br />

K pds1S<br />

+ Kids1<br />

= (8.45)<br />

2 ⎛ K pds1<br />

r ⎞ 1 Kids1<br />

S + ⎜ + S +<br />

Lσ<br />

1 L ⎟<br />

⎝<br />

σ1<br />

⎠ Lσ<br />

1<br />

The Butterworth method is applied to design the parameters <strong>of</strong> the controllers, in<br />

which the gain parameters are selected to locate the eigen-values <strong>of</strong> the tr<strong>an</strong>sfer functions<br />

uniformly in the left half <strong>of</strong> the s-pl<strong>an</strong>e, on a circle <strong>of</strong> radius ω 0 , with its center at the<br />

origin [8.2]. The second order Butterworth polynomial c<strong>an</strong> be expressed as:<br />

2<br />

2<br />

S + 2ω<br />

S + ω = 0<br />

(8.46)<br />

0<br />

0<br />

The values <strong>of</strong> ω 0 for different controllers should be properly chosen. Generally, the<br />

inner loop controller should have a value <strong>of</strong> ω 0 that is about 10 times higher th<strong>an</strong> the one<br />

in the outer control loop. Controller parameters are calculated by comparing the

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