Direct Torque Control with Space Vector Modulation (DTC-SVM) of ...
Direct Torque Control with Space Vector Modulation (DTC-SVM) of ...
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 />
Ld + Lq Lq −Ld j2( θr θK) j( θr θK)<br />
Ψ<br />
sK<br />
= ( ) IsK − ( ) I ∗ sK<br />
e − +Ψ<br />
PM<br />
e<br />
− (2.20)<br />
2 2<br />
Stator fixed system ( α,<br />
β )<br />
Taking the angular speed <strong>of</strong> the reference frame to be Ω<br />
K<br />
= 0 and θ<br />
K<br />
= 0 , the set <strong>of</strong><br />
synchronous machine vector equations (2.19) and (2.20) my be written as:<br />
U<br />
d Ψ<br />
sαβ<br />
sαβ<br />
= Rs<br />
Isαβ<br />
+ (2.21)<br />
dt<br />
Ld + Lq Lq −Ld ∗ j2θr<br />
jθ<br />
r<br />
Ψ<br />
sαβ = ( ) I<br />
sαβ − ( ) Isαβ<br />
e +Ψ<br />
PM<br />
e<br />
(2.22)<br />
2 2<br />
Substituting to above equations the following expressions for complex vectors<br />
U U jU<br />
= s sα<br />
+ , αβ sβ<br />
s sα<br />
sβ<br />
I αβ = I + jI , Ψ αβ =Ψ<br />
sα<br />
+ jΨ sβ<br />
and splitting into real and<br />
s<br />
imaginary parts one can obtain the scalar form <strong>of</strong> the machine equations in stationary<br />
α,<br />
β reference frame:<br />
U<br />
U<br />
dΨ<br />
dt<br />
sα<br />
sα<br />
= RsIsα<br />
+ (2.23a)<br />
dΨ<br />
sβ<br />
sβ<br />
= RsIsβ<br />
+ (2.23b)<br />
dt<br />
Ld + Lq Lq −Ld Lq −Ld<br />
( cos2 θ ) Is<br />
( )sin2θ Is<br />
cosθ<br />
2 2 2<br />
Ψ = − − +Ψ (2.24a)<br />
sα r α r β PM r<br />
Lq − Ld Ld + Lq Lq −Ld<br />
Ψ<br />
sβ =− ( )sin 2 θrIsα + [( ) + ( )cos2 θr] Isβ<br />
+Ψ<br />
PM<br />
sinθ<br />
(2.24b)<br />
r<br />
2 2 2<br />
Note, that in the flux-current equations (2.24a and b) still we can observe that value <strong>of</strong><br />
inductances depends on rotor position θ<br />
r<br />
.<br />
Stator flux fixed system ( x,<br />
y )<br />
In order to take advantage <strong>of</strong> the set <strong>of</strong> equations (2.19) and (2.20) in rotating coordinate<br />
system, one assumes that the coordinate system rotates <strong>with</strong> the stator flux linkage<br />
angular speed Ω<br />
K<br />
=Ω<br />
Ψ<br />
and θK<br />
= θ Ψ<br />
. As a<br />
sx s<br />
Ψ =Ψ , δ = −( θ − θ )<br />
Ψ<br />
r<br />
Ψ<br />
d Ψ<br />
U R I j<br />
dt<br />
sxy<br />
sxy<br />
=<br />
s sxy<br />
+ + ΩΨsΨ (2.25)<br />
sxy<br />
Ld + Lq Lq −Ld ∗ − j2δΨ<br />
− jδΨ<br />
Ψ<br />
sxy<br />
= ( ) Isxy − ( ) Isxy<br />
e +Ψ<br />
PM<br />
e<br />
(2.26)<br />
2 2<br />
14