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DSP Implementation of an Improved DTC Technique for Induction ...

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switching Table 1, dψ = 1 <strong>an</strong>d dψ = 0 indicates the stator flux needs to be increased <strong>an</strong>d reduced respectively.<br />

Similarly, dT = 1 indicates the motor torque needs to be increased, <strong>an</strong>d dT = 0 <strong>an</strong>d dT = -1 indicate the torque needs<br />

to be reduced slowly <strong>an</strong>d quickly respectively. Speed control is achieved using a PI controller. In a <strong>DTC</strong> drive, as<br />

shown in Figure 1, the torque reference is also obtained from the PI speed controller.<br />

Table 1 Stator Voltage Switching Table.<br />

<strong>Induction</strong> Motor Model in the Stationary Reference Frame<br />

The stationary reference frame induction motor model, with stator <strong>an</strong>d rotor fluxes as state variables, is defined by<br />

equation (1) <strong>an</strong>d <strong>for</strong>ms the basis <strong>for</strong> the simulation results in this paper.<br />

d<br />

dt<br />

⎡<br />

⎢<br />

⎣<br />

s<br />

r<br />

⎡ Rs<br />

⎢ −<br />

⎤<br />

⎢<br />

s<br />

⎥ =<br />

⎦ ⎢ Rr<br />

M<br />

⎢<br />

⎣ s<br />

Lr<br />

Rs<br />

M ⎤<br />

⎥<br />

s<br />

Lr<br />

⎥<br />

⎡<br />

⎛ R ⎢<br />

r ⎞⎥<br />

j ⎣<br />

⎜ r −<br />

⎟<br />

⎟⎥<br />

⎝<br />

r ⎠⎦<br />

s<br />

r<br />

⎤ ⎡1⎤<br />

⎥ + ⎢ ⎥V<br />

⎦ ⎣0⎦<br />

where s <strong>an</strong>d r are stator <strong>an</strong>d rotor flux space vectors, s V is stator voltage space vector, s R <strong>an</strong>d R r are the<br />

stator <strong>an</strong>d rotor resist<strong>an</strong>ces, L s <strong>an</strong>d L r are stator <strong>an</strong>d rotor self-induct<strong>an</strong>ces, M is the mutual induct<strong>an</strong>ce,<br />

2<br />

= 1 - M Ls<br />

Lr<br />

is the leakage coefficient <strong>an</strong>d r<br />

calculated from equations (2) <strong>an</strong>d (3) respectively.<br />

i<br />

i<br />

ds<br />

qs<br />

2<br />

s<br />

is rotor <strong>an</strong>gular speed. Stator dq current components are<br />

ds − md<br />

= (2)<br />

L − M<br />

s<br />

qs − mq<br />

= (3)<br />

L − M<br />

s<br />

X aq X aq<br />

X aq X aq<br />

where, md = ds +<br />

dr , mq =<br />

qs +<br />

qr<br />

L − M L − M<br />

L − M L − M<br />

s<br />

<strong>an</strong>d [ ] 1 −<br />

X = ( 1/M + 1/ ( L − M ) + 1/ ( L − M ) .<br />

aq<br />

dψ dT N1 N2 N3 N4 N5 N6<br />

1 V2(110) V3(010) V4(011) V5(001) V6(101) V1(100)<br />

1 0 V7(111) V0(000) V7(111) V0(000) V7(111) V0(000)<br />

-1 V6(101) V1(100) V2(110) V3(010) V4(011) V5(001)<br />

1 V3(010) V4(011) V5(001) V6(101) V1(100) V2(110)<br />

0 0 V0(000) V7(111) V0(000) V7(111) V0(000) V7(111)<br />

-1 V5(001) V6(101) V1(100) V2(110) V3(010) V4(011)<br />

s<br />

r<br />

r<br />

s<br />

The electromagnetic torque c<strong>an</strong> be expressed in terms <strong>of</strong> stator flux <strong>an</strong>d current as shown in equation (4)<br />

( i i )<br />

⎛ 3 ⎞⎛<br />

P ⎞<br />

Te = ⎜ ⎟⎜<br />

⎟ ds qs −<br />

⎝ 2 ⎠⎝<br />

2 ⎠<br />

qs ds<br />

where P is the number <strong>of</strong> poles in the induction motor.<br />

Compensation <strong>of</strong> the Effect <strong>of</strong> the Stator Voltage-Drop<br />

A major problem in the application <strong>of</strong> <strong>DTC</strong> at low motor speed is the effect <strong>of</strong> the IsRs voltage drop. In order to<br />

improve flux control at low speed, optimum switching vector selection <strong>an</strong>d a technique that eliminates the effects<br />

<strong>of</strong> the IsRs voltage drop in the machine stator is there<strong>for</strong>e considered.<br />

Figure 2 shows the switching voltage space vectors <strong>an</strong>d stator resist<strong>an</strong>ce voltage drop. It c<strong>an</strong> be seen that at high<br />

speed, the amplitude <strong>of</strong> the stator voltage vector sh V is large <strong>an</strong>d the voltage drop across R s is relatively small <strong>an</strong>d<br />

c<strong>an</strong> be neglected, as shown in Figure 2(a). However, it c<strong>an</strong> be seen from Figure 2(b) that, at low speed, the voltage<br />

drop across s R may be the major portion <strong>of</strong> measured terminal voltage V sl . Moreover, as the temperature <strong>of</strong> the<br />

r<br />

(1)<br />

(4)

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