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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 />

From Fig. 2.8, it can be seen that<br />

M is maximum when torque angle is 90 < < 180<br />

e<br />

The relevant torque equation in this mode <strong>of</strong> operation becomes from (2.55).<br />

<br />

δ <br />

I<br />

.<br />

The steady state voltage equations can be written using the current vector amplitude<br />

I<br />

s<br />

and the torque angle δ<br />

I<br />

as:<br />

U = R I cosδ<br />

+ p Ω L I sinδ<br />

(2.73a)<br />

sd s s I b m q s I<br />

U = R I sinδ<br />

− p Ω L I cosδ<br />

+ p Ω Ψ (2.73b)<br />

sq s s I b m d s I b m PM<br />

The amplitude <strong>of</strong> stator voltage vector can be calculated from equation (2.70) and<br />

amplitude <strong>of</strong> stator flux vector from (2.71). The active and reactive power and also the<br />

power factor can be obtained from equations (2.41),(2.46), (2.47).<br />

Unity power factor (UPF) control<br />

Under this control strategy there is no phase different between the current vector and the<br />

voltage vector. Hence, power factor angle φ (see Fig. 2.13) becomes zero. Since only<br />

active power is supplied to the machine under unity power factor operation, the VA<br />

rating requirement <strong>of</strong> the inverter can be reduced.<br />

q − axis<br />

U s<br />

φ = 0<br />

I s<br />

δ I<br />

d − axis<br />

Figure 2.13. Current vector and permanent magnet flux vector under unity power factor<br />

operation (UPFC).<br />

Ψ PM<br />

In this case when φ = 0 we have the relationship:<br />

U<br />

U<br />

sq<br />

sd<br />

Isq<br />

= = tanδ<br />

I<br />

(2.74)<br />

I<br />

sq<br />

Substituting the voltage equations (2.69a-b) into (2.71) and made some simplifying, we<br />

can obtain:<br />

I L −L −Ψ + L I = (2.75)<br />

2<br />

s<br />

(<br />

d q)cos δI PM<br />

cosδI q s<br />

0<br />

27

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