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

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<strong>Direct</strong> <strong>Torque</strong> <strong>Control</strong> <strong>with</strong> <strong>Space</strong> <strong>Vector</strong> <strong>Modulation</strong><br />

5.2.2 Digital torque control loop<br />

The considered torque control loop is shown in Fig. 5.15.<br />

Ψ s _ ref<br />

M e _ ref<br />

−<br />

<strong>Torque</strong><br />

controller<br />

PI<br />

∆δ Ψ<br />

Reference<br />

flux generator<br />

In stator frame<br />

Ψ<br />

s α _ ref<br />

Ψ<br />

s β _ ref<br />

−<br />

∆Ψ sα<br />

−<br />

∆Ψ sβ<br />

Flux<br />

controllers<br />

In stator frame<br />

U<br />

s α _ ref<br />

U<br />

s β _ ref<br />

M e<br />

θ Ψs<br />

Ψ sα<br />

Ψ sβ<br />

Figure 5.15. <strong>Torque</strong> control loop <strong>with</strong> PI controller.<br />

Based on the equation (5.9a-b and 5.10a-b) the stator flux errors in α,<br />

β coordinates can<br />

be calculated as:<br />

∆Ψ<br />

α<br />

= Ψ cos( θ + ∆δ ) − Ψ cos θ = Ψ [cos( θ + ∆δ ) − cos θ ]<br />

s s_ ref Ψs Ψ s_ ref Ψs s_<br />

ref Ψs Ψ Ψs<br />

(5.21a)<br />

∆Ψ<br />

β<br />

= Ψ sin( θ +∆δ ) − Ψ sin θ = Ψ [sin( θ +∆δ ) − sin θ ]<br />

s s_ ref Ψs Ψ s_ ref Ψs s_<br />

ref Ψs Ψ Ψs<br />

(5.21b)<br />

Assuming that for small changes <strong>of</strong> ∆δ Ψ<br />

the cos ∆δ Ψ<br />

≅ 1and sin ∆δ Ψ<br />

≅∆ δ<br />

Ψ<br />

, the equations<br />

(5.21a) and (5.21b) are given by:<br />

∆Ψ<br />

α _<br />

= − Ψ<br />

_<br />

∆ δ sinθ<br />

(5.22a)<br />

s ref s ref Ψ Ψs<br />

∆Ψ<br />

β _<br />

= Ψ<br />

_<br />

∆ δ cosθ<br />

(5.22b)<br />

s ref s ref Ψ Ψs<br />

In order to design the PI torque controller the following assumption are made:<br />

• stator flux vector position θ Ψ s<br />

and rotor flux vector position θ<br />

r<br />

are equal zero. It<br />

correspond to situation, when those two flux vectors lie along theα axis,<br />

• the reference stator flux amplitude is equal value <strong>of</strong> permanent magnet flux<br />

Ψ<br />

s _ ref<br />

=Ψ<br />

PM<br />

,<br />

• stator resistance is neglected.<br />

Therefore, the error stator fluxes in α,<br />

β coordinates are calculated as:<br />

∆Ψ = , (5.23a)<br />

sα<br />

_ ref<br />

0<br />

79

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