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Direct Torque Control with Space Vector Modulation (DTC-SVM) of ...

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<strong>Control</strong> methods <strong>of</strong> PM Synchronous motor<br />

For many years the CTA control ( I<br />

_<br />

= 0 ) method has been a popular technique for a<br />

sd<br />

ref<br />

long time because <strong>of</strong> simple control. This method was dedicated for surface permanent<br />

magnet synchronous motor (SPMSM), where the magnetic saliency does not exist<br />

[126]. So the maximum torque per ampere is obtained, when stator current vector is<br />

shifted in respect to rotor flux vector 90 degree. However, in IPMSM, maximum torque<br />

per ampere is obtained <strong>with</strong> torque angle more than 90 degree. This is because <strong>of</strong><br />

existence <strong>of</strong> reluctance torque component due to magnetic saliency (see subchapter<br />

2.2.2). Therefore, the I<br />

sd_<br />

ref<br />

should be negative value [44].<br />

The main question is how or in which manner produce the reference currents in d-q<br />

frame. Its leads to many realization <strong>of</strong> current control structure. Among them generally<br />

we can distinguish two structures <strong>of</strong> current control loop. One <strong>of</strong> them is hysteresis<br />

based control (Fig.4.7a) [3,52] and the second one is PI based current controllers<br />

(Fig.4.7b).<br />

Hysteresis based current control has following disadvantage such as [3]:<br />

• measurement <strong>of</strong> three phase currents are required,<br />

• three independent hysteresis current controllers are required,<br />

• variable switching frequency is achieved,<br />

• fast sampling time is required.<br />

All this listed above disadvantage can be eliminate, when the PI current control are<br />

used. This structure are mostly used in industrial application (Fig. 4.7b).<br />

a)<br />

U DC<br />

M e _ ref<br />

Fig. 4.5<br />

I d _ ref<br />

I q _ ref<br />

d,q/ABC<br />

I A _ ref<br />

I B _ ref<br />

I C _ ref<br />

−<br />

−<br />

S A<br />

S B<br />

S C<br />

Inverter<br />

current<br />

feedback<br />

−<br />

I A current<br />

I<br />

sensors<br />

B<br />

I C<br />

rotor<br />

position<br />

sensor<br />

PMSM<br />

56

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