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

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Sensorless Speed <strong>Direct</strong> <strong>Torque</strong> <strong>Control</strong> <strong>with</strong> <strong>Space</strong> <strong>Vector</strong> <strong>Modulation</strong> (<strong>DTC</strong>-<strong>SVM</strong>)<br />

Therefore, for commercially manufactured drives are impractical and further a simple<br />

open loop based techniques will be considered.<br />

6.5.2 Back electromotive force (BEMF) technique<br />

This technique uses the back electromotive force to estimate the rotor speed [70]. The<br />

velocity signal could be integrated to generate a position estimate. However, this signal<br />

is sensitive to parameter variations and tends to drift and have <strong>of</strong>fset problem. Another<br />

problem <strong>with</strong> using BEMF to estimate position is that at zero speed the BEMF goes to<br />

zero and at low speed the signal to noise ratio can not be ignored.<br />

6.5.3 Stator flux based technique<br />

Generally, the calculation <strong>of</strong> rotor speed is based on the simple relationship:<br />

θ = θ − δ , (6.20)<br />

r Ψs Ψs<br />

where θ<br />

r<br />

is electrical position, θ Ψ s<br />

is stator flux position and δ Ψ s<br />

is torque angle.<br />

After differentiation equation (6.20) and taking into account that θ r<br />

= p b<br />

γ m<br />

the<br />

mechanical speed <strong>of</strong> PMSM rotor can be expressed as:<br />

⎛dθ<br />

⎜<br />

⎝ dt<br />

Ψs<br />

Ω<br />

m<br />

= −<br />

dδΨ<br />

⎞<br />

⎟/<br />

pb<br />

, (6.21)<br />

dt ⎠<br />

dθ s<br />

where Ω Ψ<br />

Ψs<br />

= is angular speed <strong>of</strong> stator flux vector and δ Ψ<br />

is torque angle.<br />

dt<br />

As we can observe form equation (6.21) in order to calculate the mechanical rotor speed<br />

it is necessary to calculate separately two components. One <strong>of</strong> them is angular speed <strong>of</strong><br />

stator flux vector Ω<br />

Ψs<br />

and the second one is change <strong>of</strong> the load angle d δ Ψ (see Fig.<br />

dt<br />

6.12).<br />

133

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