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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 />

Referring to Fig. 2.7, stator flux components in rotor reference frame can be written as:<br />

where:<br />

Ψ = Ψ cos = LI +Ψ (2.56a)<br />

sd s<br />

δ Ψ d sd PM<br />

Ψ = Ψ sin = LI<br />

(2.56b)<br />

sq s<br />

δ Ψ q sq<br />

Ψ<br />

s<br />

is stator flux linkage amplitude, Ψ<br />

PM<br />

is rotor permanent magnet and δ Ψ<br />

is<br />

torque angle (angle between stator flux linkage vector and rotor permanent magnets flux<br />

vector).<br />

q−<br />

axis<br />

I sq<br />

Ψ sd<br />

Ψ PM<br />

I s<br />

Ω s<br />

Ψ s<br />

Ψ<br />

sq<br />

= LqI<br />

sq<br />

LI<br />

d<br />

sd<br />

δ Ψ<br />

I sd<br />

d<br />

− axis<br />

Ψ<br />

sd<br />

= LI<br />

d sd<br />

+ΨPM<br />

Figure 2.7. Rotor permanent magnet flux vector and stator flux linkage vector in rotor reference<br />

frame.<br />

From (2.56a) and (2.56b) the I<br />

sd<br />

and Isq<br />

can be obtained as:<br />

I<br />

I<br />

sd<br />

sd<br />

Ψs<br />

cosδ Ψ<br />

−ΨPM<br />

= (2.57a)<br />

L<br />

d<br />

Ψs<br />

sinδ = Ψ<br />

(2.57b)<br />

L<br />

q<br />

Substituting current components (2.57a), (2.57b) into equation (2.51), one can obtain<br />

another useful torque expressions:<br />

M<br />

e<br />

3 Ψ sin<br />

2 s<br />

ΨPM<br />

δΨ Ψs<br />

( Lq<br />

−Ld)sin2δ<br />

Ψ<br />

= pb[ −<br />

]<br />

2 Ld 2LdL<br />

<br />

q<br />

<br />

Mes<br />

M<br />

er<br />

(2.58)<br />

where:<br />

Ψ<br />

s<br />

stator flux linkage amplitude, and Ψ<br />

PM<br />

rotor flux, δ Ψ<br />

is torque angle, M<br />

es<br />

-<br />

synchronous torque,<br />

M<br />

er<br />

- reluctance torque.<br />

21

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