Direct Torque Control with Space Vector Modulation (DTC-SVM) of ...
Direct Torque Control with Space Vector Modulation (DTC-SVM) of ...
Direct Torque Control with Space Vector Modulation (DTC-SVM) of ...
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Modeling and control modes <strong>of</strong> PM synchronous motor drives<br />
2.1.2 Instantaneous power and electromagnetic torque<br />
The three-phase star-connection system <strong>with</strong>out neutral wire is shown in Fig. 2.4. This<br />
is classical configuration for AC motor windings connections.<br />
A<br />
I sA<br />
U sAC<br />
U sAB<br />
B<br />
U sA<br />
Z sC<br />
Z sA<br />
U sAB<br />
Z sB<br />
C<br />
U sBC<br />
I sC<br />
U sC U sB<br />
I sB<br />
Figure 2.4. Three-phase star connection system <strong>with</strong>out neutral wire.<br />
For this configuration the expression for instantaneous active power supplied to load<br />
can be expressed as:<br />
P= UsAIsA+ UsBIsB+ UsCIsC<br />
(2.35)<br />
Introducing space vector definition, after some arrangement and taking into account the<br />
relation: I + I + I = 0, the equation (2.35) can be written as:<br />
sA sB sC<br />
3 ∗<br />
P= Re[ U<br />
sABC<br />
IsABC<br />
]<br />
(2.36)<br />
2<br />
For dq , frame, the equation (2.35) for the active power can be expressed as:<br />
3<br />
P= ( UsdIsd + UsqIsq<br />
)<br />
(2.37)<br />
2<br />
Substituting voltage equation (2.4) into (2.36), and adopting Ω<br />
K<br />
= pbΩmone obtains<br />
3 ∗ d Ψ<br />
[Re(<br />
sABC ∗ ∗<br />
P= RsIsABC IsABC + IsABC − jpbΩmΨ sABCIsABC<br />
)] (2.38)<br />
2<br />
dt<br />
Note that<br />
sABC<br />
sABC<br />
2<br />
s<br />
I I ∗ = I and:<br />
3 2 d Ψ<br />
[ Re(<br />
sABC ∗<br />
∗<br />
P= Rs Is + IsABC ) + Re( −jpbΩmΨ sABC<br />
IsABC<br />
)] (2.39)<br />
2<br />
dt<br />
d ΨsABC<br />
Hence, neglecting the losses in stator resistance R<br />
s<br />
and assuming that = 0 , the<br />
dt<br />
electromagnetic power is expressed:<br />
17