section 6. dynamics of electric drive systems section 6 - dynamics... · dcm has two windings...
TRANSCRIPT
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Section 6. Dynamics of Electric Drive Systems
1
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2
Review of steady state analysis of DC machine Dynamics of Separately Excited (SE) DC machine
Dynamics of Synchronous Machine (SM)
Rotor flux oriented control (RFOC) of SM
Dynamics of Induction Machine (IM)
Rotor Flux Oriented (FOC) Vector Control of IM
Outlines
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3
Review of steady state analysis of DC machine Review of dynamics of Separately Excited (SE) DC machine
Dynamics of Synchronous Machine (SM)
Rotor flux oriented control (RFOC) of SM
Dynamics of Induction Machine (IM)
Rotor Flux Oriented (FOC) Vector Control of IM
Outlines
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Review of DC Machine Steady-States
4
Steady-state analysis (Va, ωm, Ia)
a a a E mV R I K
e T aT K I
c
a am e
E E T
V RT
K K K
If = CONST
Slope-Intercept Form
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Review of DC Machine Steady-States
5
Steady states for field weakening (Va=CONST)
' ' ' 2
a am e
E E T
V RT
K K K
'a a a E f f mV R I K K I
'
e t f f aT K K I I
CONSTaV
f fK I
A
B
TL
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6
Review of steady state analysis of DC machine Dynamics of Separately Excited (SE) DC machine
Dynamics of Synchronous Machine (SM)
Rotor flux oriented control (RFOC) of SM
Dynamics of Induction Machine (IM)
Rotor Flux Oriented (FOC) Vector Control of IM
Outlines
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7
aa a a a E m
div R i L K
dt
Lmm
TaT TDdt
dJiKT
Electric equation in the armature circuit
Motion equation
Dynamics of the Separately Excited DC Motor
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8
aa a a a E m
div R i L K
dt
τa=La/Ra
d/dt=>s
a aa a a
a
V ( s ) E ( s )s I ( s ) I ( s )
R
Va(s)
Ea(s)
Ia(s) +
a
a
1 / R
1 s
a
a a a
a
1/ RI ( s ) V ( s ) E ( s )
1 s
Dynamics of the Separately Excited DC Motor
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9
Lmm
TaT TDdt
dJiKT
)s(T)s(D)s(sJ)s(IK)s(T LmmTaT
d/dt=>s
DsJ
)s(T)s(IK
DsJ
)s(T)s(T)s(
T
LaT
T
Lm
Dynamics of the Separately Excited DC Motor
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10
KT DsJ
1
T
KE
Va(s)
Ea(s)
Ia(s)
T (s)
TL(s)
m(s) a
a
1 / R
1 s
DsJ
)s(T)s(IK
DsJ
)s(T)s(T)s(
T
LaT
T
Lm
a
a a a
a
1/ RI ( s ) V ( s ) E ( s )
1 s
Dynamics of the Separately Excited DC Motor
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11
a
1
1 s
TJ
Ds
1
ref(s) Ia(s)
TL(s)/JT(s)
m(s)
E
1
K
m(s)
aT
TE
RJ
KK Va
+
a Tm
E T
R J
K K a
a
a
L
R
τm >> τa Current changes much faster than the speed
aV s
Case A: Purely inertia load with D 0 and TL 0
Case B: Inertia load with viscous friction and TL 0
Case C: Effect of load torque on motor dynamics
Dynamics of the Separately Excited DC Motor
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Case A: Purely inertia load with D 0 and TL 0
Va(s)
ref
m
a
1 /
1 s s
m
E
1
K
m
m E a mE
2
a a m a a m
1 / K1 / K
V 1 s s 1 s s / 1 /
0s2s 2nn
2 n
a m
1
m
a
1
2
12
Natural frequency Damping coefficient
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Step Response of a Second-Order System
13
0 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4 0.45 0.5-0.5
0
0.5
1
1.5
2
2.5
Time(sec)
Input
output
n=20 =0
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.80
0.5
1
1.5
2
=0.1 =0.5 =1 =2 =4
n=20
Undamped Natural frequency 10Hz
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2
1 2
2 2
1 1 1, 1 4
2 2
1 1 1 1 1 1 1 21 4 2
2 2 2 2
1 1,
a a m
a
a a m m
a a a m
m a
s s
Case A: Purely inertia load with D 0 and TL 0
14
T a Tm E
a a m
a m
K / L J 1 / K
V s 1 s 11 1s s
Closed-loop poles are obtained by solving the
characteristic equation (denominator of TF = 0)
a m
using the indentity if x
1 x 1 x 12
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Case B: Inertia load with viscous friction and TL 0
=
m T
a a a T E T
T T a
2
T a a T E T T a a a
K
V sL R J s D K K
K J L
s D J R L s D J K K J R R L
1 1n
a m T
D
J
1 1
2n
a T
D
J
15
Standard second order transfer characteristic
T
mTa
K
DsJI
mmTaTm DsJIKT
mEaaaa KIRsLV
1 a1 m
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Case C: Effect of load torque on motor dynamics
TL m
Va = 0
+
+
Ea
KE Ia 1 /
1
a
a
R
s
KT
T
T
1
J s D
16
Va = CONST
Small perturbations in TL
1
1
m a
E TLa T
a
s
K KT s J s DR
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17
Va=50V; 1 Nm load applied @ 1s
0 0.5 1 1.5 20
1
2
Load t
orq
ue(N
m)
0 0.5 1 1.5 20
200
400
time(sec)
Speed(r
pm
)Case C: Effect of load torque on motor dynamics
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Dynamics of field controlled separately excited DC motor
if
Rf Lf
vf Va
Ia
m
(s)Tf fmf f a Tf f T m m
T
K IdT K i i K I J D
dt J s D
( )( )
f f
f f f f f
f f
di V sv R i L I s
dt R sL
Tfm
f f f T
Ks
V s R L s J s D
18
E T f fK K K i
m
f
s?
V s
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Dynamics of field controlled separately excited DC motor
19
dt
diLiRv
fffff
fv fi
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Dynamics of field controlled separately excited DC motor
20
Va =200V, If =0.2A 0.1A at 10 sec. wm = 160 rpm 300 rpm
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Position response with inner current control
a
1
1 sKT
T
1
J s D
1
s
q
KE
Va
Ea
+
-
Ia T
21
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Dynamics of separately excited DC motor
22
• The nonlinear model results in a two-input (Va, If), one-output (wm) map, having a disturbance input TL.
• Field (If) control with constant armature current (Ia); torque decreases with the increase of speed (field weakening).
• Armature current control by adjusting the armature voltage with a constant field (constant torque).
• Exceeding rated voltages accelerates ageing of conductor insulation, field weakening is used to increase the speed further.
• Open loop control. Exact values of armature voltage and field need to be known in order to obtain the expected speed. They are load dependent.
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Example I: Compare the dynamics of two SE DC motors
23
Parameters Motor 1 Motor 2
Rated power (kW) 0.75 75
Rated speed (r/min) 500 1750
Ra (Ohm) 7.56 0.0114
La (H) 0.055 0.0011
KE (V/rad/s) 4.23 1.27
JL, Jm (kgm^2) 0.068 1.82
The torque-speed characteristic of the load is a straight line through the origin and the rated load point.
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Example I: Compare the dynamics of two SE DC motors
24
Compare the un-damped natural frequencies ωn, the damping ratio ξ and the time constants Ta (or τa) and Tm
(or τm ) of the two motors.
TL
ω Nm / rad / sT 14.3
D 0.27352.3
rated
P 750T 14.3 Nm
52.3
2T m LJ J J 2 0.068 0.136 kgm
aa
a
L0.0073
R
a Tm
E T
R J0.0575
K K
n
a m T
1 1 D51.54 rad/s
J
n a T
1 1 D1.348
2 J
For Motor 1:
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Example I: Compare the dynamics of two SE DC motors
25
Parameters Motor 1 Motor 2
Electrical time constant, τa (s) 0.0073 0.0965
Mechanical time constant, τm (s) 0.0575 0.246
Natural frequency, ωn (rad/s) 69.49 9.11
damping ratio, ξ 1.348 0.582
0 0.5 1 1.5
0
4000
8000
Torq
ue(N
m)
0 0.5 1 1.5
0
1000
2000
Time(sec)
Speed(r
pm
)
0 0.5 1 1.5
0
50
100
150
200
Am
atu
re V
oltage(V
)
speed
Armature voltage
0 0.5 1 1.5
0
20
40
60
80
Torq
ue(N
m)
0 0.5 1 1.5
0
100
200
300
400
Time(sec)
Speed(r
pm
)
0 0.5 1 1.5
0
50
100
150
200
Am
atu
re V
oltage(V
)
speed
armature voltage
Under-damped response Over-damped response
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Closed loop control of separately excited DC motor
26
Speed control (200rpm),
If=0.2A The armature current exceeds the current limit of the DC motor during the transient (10-10.2 sec).
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Closed loop control of separately excited DC motor
27
Speed control (200rpm) Field current control (0.20.1A) The armature current exceeds the limit during the speed transient.
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Closed loop control of separately excited DC motor
28
Speed control (200rpm) Field current control (0.2A) Armature current control (maximum armature is limited within 20A)
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29
Review of steady state analysis of DC machine Review of dynamics of Separately Excited (SE) DC machine
Dynamics of Synchronous Machine (SM)
Rotor flux oriented control (RFOC) of SM
Dynamics of Induction Machine (IM)
Rotor Flux Oriented (FOC) Vector Control of IM
Outlines
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Representation of SM in the rotor reference frame
33
• The steady-state equivalent circuit of SM does not address the dynamics of the motor in the transient state.
• The equation of torque developed earlier does not have a direct or linear relationship with instantaneous values of stator current.
Ef
jXs=jLs I
V0
3sin
f
s s
pVET
X
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Recall Questions
34
• Write the equations of the balanced three-phase currents in the stator windings of SM? Draw the waveform of 3-ph currents (amplitude=1, 50Hz).
• How are the 3-ph windings placed physically?
The 3-ph windings are displaced physically by 120° from each other
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Representation of the synchronous machine in the rotor reference frame
Purpose: We seek to express the developed torque and flux in terms
of some instantaneous currents, as for the DC machine. This is not
possible with steady-state equivalent circuit models.
a
a’
b
b’
c
c’θ
ia
ib
ic
ea
eb
ec
Axis of
phase ‘a’
mmf
d-axis;
axis of
rotor mmf
q-axis;
orthogonal
to d-axis
35
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Representation of the synchronous machine in the rotor reference frame
36
What are the differences between a DC motor and a SM? 1. DCM has two windings (field and armature in a SE DC motor) SM has three-phase stator windings. Solution: Convert three-phase quantities of SM into two phase quadrature quantities (fictitious). 2. DCM driven by DC and the AC machine is by AC (three-phase SINE balance) We need to convert vectors in two-phase orthogonal stationary system into orthogonal rotating reference frame, where the quantities are DC values. abc (3-ph AC)α-β (2-phase AC)d-q (2-ph DC)
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Warm-up Question I (Clarke Transformation)
37
Consider the case of balanced three-phase stator currents
1 11
2 2
3 30
2 2
1 1 1
2 2 2
sa
b s
c s
cos( t)i
i cos( t 120 )
i cos( t 120 )
Find two-phase orthogonal currents using the following
transformation matrix
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Warm-up Question I
38
Three-phase to two-phase transformation
sa b c
a
b b c s
c0
a b c
1 1 31 cos( t)i 0.5i 0.5i2 2 2i i3 3 3 3
i 0 i i i sin( t)2 2 2 2
ii 1 1 1 1 0i i i
2 2 2 2
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Warm-up Question II
39
Find a factor in front of the transformation matrix to make the 2-ph currents have the same amplitude as 3-ph currents?
β
α
2/3 2 2 3 2i i
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Warm-up Question III (Park Transformation)
40
• Transform the two-phase (α-β) currents to another 2-ph (d-q) currents by the following matrix (θ is the rotor position).
d
q
0 0a b c
0 0a b c
m s
m s
i icos sin
i isin cos
i cos i cos 120 i cos 2402
3 i sin i sin 120 i sin 240
I cos( t )
I sin( t )
q q
q q
q q q
q q q
q
q
stq
d m
q m
i I cos( )
i I sin( )
cos sin
sin cos
q q
q q
2 2d q mi i I
Check the amplitude
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Warm-up Question III
41
• α-β: 2-ph AC currents on stationary reference frame • d-q: 2-ph DC currents on rotor reference frame.
30
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Representation of the synchronous machine in the rotor reference frame
42
abcαβ0 αβ0dq0
abc αβ0 dq0
Clarke Transformation Park Transformation
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Representation of the synchronous machine in the rotor reference frame
43
0 0
ds as
0 0qs bs
cs0s
cos cos 120 cos 240f f
2f sin sin 120 sin 240 f
3ff 1 1 1
2 2 2
q q q
q q q
Any three-phase sinusoidal set of quantities in the stator can be transformed to an orthogonal reference frame by
magnetic axis of the rotor
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Assumptions
stator windings are sine-distributed, balanced windings around the respective winding axes, (no zero or negative sequence)
the rotor field is cosine distributed about the rotor axis, (mutual inductance between stator and rotor varies as cosθ)
stator and rotor slots do not affect the mutual windings appreciably, (only consider mutual inductances between phase windings and stator and rotor windings)
magnetic saturation is negligible.
44
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What do we need to find for SM Dynamics
45
Voltage equations in rotor (d-q) ref. frame. Expectation: One voltage equ. for torque current control; the other for field control, like Va and Vf in DC machine.
Torque equation . A direct or linear relationship with instantaneous stator current, like Te=Kt·Ia in DC machine.
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Steps to Find Torque and Flux of SM
46
Rotor and stator flux linkages of SM on 3-ph ref. frame;
Transform the stator flux linkages to the rotor (d-q) ref. frame;
Machine voltage equations derived from flux linkage
equations;
Derive the equation of output power from instantaneous input
power;
Derivation of torque equation from output power and
mechanical speed.
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Step I:
53
Rotor and stator flux linkages of SM on abc ref. frame;
Transform the stator flux linkages to the rotor (d-q) ref. frame;
Machine voltage equations derived from flux linkage
equations;
Derive the equation of output power from instantaneous input
power;
Derivation of torque equation from output power and
mechanical speed.
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Winding self-inductances
aa A BL L L cos 2q
bb A BL L L cos 2 120q
cc A BL L L cos 2 240q
• Self inductance of each winding is λ/I of its own current; • It varies between max and min values according to the
position of the rotor. • Self-inductance goes through two cycles of variations for each
rev. of the rotor (2θ);
54
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Self inductance expressions [1]
q
gmin
gmax
2A s
min max
C 1 1L N
2 g g
2B s
min max
C 1 1L N
2 g g
2aas,min l s
max
1L L CN
g
2aas,max l s
min
1L L CN
g
oC rl4
[1] P. C. Krause, O. Wasynczuk, S. D. Sudhoff, S. Pekarek, Ch1, Analysis of Electric Machinery and Drive Systems, 3rd ed., Wiley-IEEE, 2013.
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Self-inductances
56
0 0.005 0.01 0.015 0.02 0.025 0.03 0.035 0.04
Time (s)
0
1
2
3
Laa
LA
LB
Laas
0° 90° 180° 270° 360°
0
q
aas A BL L L cos 2q
bbs A BL L L cos 2 120q
ccs A BL L L cos 2 120q
LA is independent on rotor position
LB is max value of inductance varying with rotor position
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57
Mutual inductances between phase windings
ab ba A B
1L L L L cos 2 30
2q
bc cb A B
1L L L L cos 2 90
2q
ca ac A B
1L L L L cos 2 150
2q
ab ba A BL L L cos(120 ) L cos 2 120q
bc cb A BL L L cos(120 ) L cos 2 120 120q
ca ac A BL L L cos( 240 ) L cos 2 240q
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Mutual inductance between stator and rotor windings
58
af fa mL L L cosq
0bf fb mL L L cos 120q
0cf fc mL L L cos 240q
1m s r
min
L CN Ng
• mutual inductances between a stator and the rotor winding varies as a cosine function of θ.
• The mutual inductance between phase a winding and the rotor becomes maximum when the rotor aligns with the axis of this winding
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0 0d a b ci K i cos i cos 120 i cos 240q q q
0 0q a b ci K i sin i sin 120 i sin 240q q q
fd f f af a bf b cf c
0 0f f m a b c
L i L i L i L i
L i L i cos i cos 120 i cos 240
q q q
Total rotor flux linkage along the d-axis (rotor)
59
Machine rotor flux linkages
fd f f m d f m d
3 3L i L i L i
2 2
Let
Expressed with one current rather than 3 currents
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2 2
amax bmax cmax d qI I I i i
0 a b c
1i i i i
3
0 0
d a
0 0q b
c0
cos cos 120 cos 240i i
2i sin sin 120 sin 240 i
3ii 1 1 1
2 2 2
q q q
q q q
60
We choose K = 2/3, so that,
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61
0 0
0 0
cos cos 120 cos 2401 0.5 0.5cos sin 02 2
A sin cos 0 0 3 2 3 2 sin sin 120 sin 2403 3
0 0 1 1 / 2 1 / 2 1 / 2 1 1 1
2 2 2
q q qq q
q q q q q
Stay Awake Question I
d
q
0 0
i cos sin 0 i
i sin cos 0 i
i 0 0 1 i
q q
q q
a
b
c0
1 11
2 2i i
2 3 3i 0 i
3 2 2ii 1 1 1
2 2 2
Find the matrix A, which can convert 3-ph (abc) currents to 2-ph currents in the rotor ref. frame (dq)
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62
0 0
0 0
cos cos 120 cos 240
2A sin sin 120 sin 240
31 1 1
2 2 2
q q q
q q q
Stay Awake Question II
Find the reverse transformation, which can convert dq currents to 3-ph (abc) currents
1 0 0
0 0
cos sin 1
A cos 120 sin 120 1
cos 240 sin 240 1
q q
q q
q q
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63
Stay Awake Question II
1AA E
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a d
1
b q
c 0
i i
i A i
i i
1 0 0
0 0
cos sin 1
A cos 120 sin 120 1
cos 240 sin 240 1
q q
q q
q q
0 0
0 0
cos cos 120 cos 240
2A sin sin 120 sin 240
31 1 1
2 2 2
q q q
q q q
64
Inverse transformation
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Stator flux linkages a aa a ab b ac c af fL i L i L i L i
65
0
a A B a A B b
0
A B c af f
1L L cos 2 i L L cos 2 30 i
2
1L L cos 2 150 i L i
2
q q
q
0 0
b A B a A B b
0
A B c b f f
1L L cos 2 30 i L L cos 2 120 i
2
1L L cos 2 90 i L i
2
q q
q
0 0
c A B a A B b
0
A B c c f f
1 1L L cos 2 150 i L L cos 2 90 i
2 2
L L cos 2 240 i L i
q q
q
b ba a bb b bc c bf fL i L i L i L i
c ca a cb b cc c cf fL i L i L i L i
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Step II:
66
Rotor and stator flux linkages of SM on abc ref. frame;
Transform the stator flux linkages to the rotor (d-q) ref. frame;
Machine voltage equations derived from flux linkage
equations;
Derive the equation of output power from instantaneous input
power;
Derivation of torque equation from output power and
mechanical speed.
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Stator flux linkages
67
1
0 0
1 0.5 0.5
0.5 1 0.5
0.5 0.5 1
cos(2 ) cos(2 120) cos(2 240)
cos(2 120) cos(2 240) cos(2 )
cos(2 240) cos(2 ) cos(2 120)
d a d
q b A q
c
B
i
A L A A i
i
L A
q q q
q q q
q q q
1
0
cos( )
cos( 120)
cos( 240)
d
q m f
i
A i L i A
i
q
q
q
0 0
0 0
cos cos 120 cos 240
2A sin sin 120 sin 240
31 1 1
2 2 2
q q q
q q q
1 0 0
0 0
cos sin 1
A cos 120 sin 120 1
cos 240 sin 240 1
q q
q q
q q
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Stator flux linkages
68
cos 0.5cos 120 0.5cos 1202
1 term sin 0.5sin 120 0.5sin 1203
0
0.5cos cos 120 0.5cos 120
0.5sin sin 120 0.5sin 120
0
0.5cos 0.5
Ast L
q q q
q q q
q q q
q q q
q
1
cos 120 cos 120
0.5sin 0.5sin 120 sin 120
0
A
q q
q q q
cos cos 120 cos 120q q q
sin sin 120 sin 120q q q
Using the following identity
0.5cosq
0.5sinq
0.5cos 120q
0.5sin 120q
0.5cos 120q
0.5sin 120q
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Stator flux linkages
69
1
1 1
1.5cos 1.5cos 120 1.5cos 1202
1 term 1.5sin 1.5sin 120 1.5sin 1203
0 0 0
0 0 0 1 0 03 3
= 0 0 0 0 1 02 2
0.5 0.5 0.5 0 0 0
A
A A A
st L A
L AA L A L
q q q
q q q
1 0 03
2 term 0 1 02
0 0 0
Bnd L
0 0
0 0
cos cos 120 cos 240
2A sin sin 120 sin 240
31 1 1
2 2 2
q q q
q q q
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Stator flux linkages
70
2 2 2cos cos 120 cos 1202
3rd term sin cos sin 120 cos 120 sin 120 cos 1203
0.5 cos cos 120 cos 120
1
= 0
0
m f
m f
L i
L i
q q q
q q q q q q
q q q
2cos 1 cos 2 2q q
2cos 120 1 cos 2 240 2q q
2cos 120 1 cos 2 240 2q q
cos 2 cos 2 240 cos 2 240 0q q q
sin 2 sin 2 240 sin 2 240 0q q q
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71
d A A B d a f f
d d m f d d f
1 3L L L i L i
2 2
L i L i L i
q A A B q
q q
1 3( L L L )i
2 2
L i
d A B
3L L L
2
q A B
3L L L
2
Stator flux linkages on Rotor Reference Frame
Ld and Lq are independent of position now
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Step III:
72
Rotor and stator flux linkages of SM on abc ref. frame;
Transform the stator flux linkages to the rotor (d-q) ref. frame;
Machine voltage equations derived from flux linkage
equations;
Derive the equation of output power from instantaneous input
power;
Derivation of torque equation from output power and
mechanical speed.
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0 0
d a
0 0
q b
c0
cos cos 120 cos 240
2sin sin 120 sin 240
31 1 1
2 2 2
q q q
q q q
73
0 0
d a a
0 0
q b b
c c0
sin sin 120 sin 240
d 2 d dcos cos 120 cos 240 A
dt 3 dt dt0 0 0
q q q q
q q q
qa d
b q d
c 00
d dA
dt dt
' ' 'uv u v uv
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Stator voltage equations
74
aa a
dv Ri
dt
bb b
dv Ri
dt
cc c
dv Ri
dt
1
0 0
1 0 0
0 1 0
0 0 1
d a d a
q b q b
c c
v v id
v A v R A A i Adt
v v i
qdd d
q q q d
0 0 00
v id
v R idt
v i
1 0 0
0 1 0
0 0 1
a a a
b b b
c c c
v id
v R idt
v i
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d d d d m f e q q
dv Ri L i L i L i
dt
fd dd d m e q q d d e q q
didi diRi L L L i Ri L L i
dt dt dt
q
q q q e d d f
div Ri L L i
dt
00 0
dv Ri 0
dt
75
e r
dp
dt
q
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Review of Dynamics of SM
76
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77
0 0
0 0
cos cos 120 cos 240
2A sin sin 120 sin 240
31 1 1
2 2 2
q q q
q q q
Forward(abcdq) and reverse (dqabc) transforms
1 0 0
0 0
cos sin 1
A cos 120 sin 120 1
cos 240 sin 240 1
q q
q q
q q
a
a’
b
b’
c
c’θ
ia
ib
ic
ea
eb
ec
Axis of
phase ‘a’
mmf
d-axis;
axis of
rotor mmf
q-axis;
orthogonal
to d-axis
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78
fd f f m d f m d
3 3L i L i L i
2 2
Machine rotor and stator flux linkages
d d d fL i
q q qL i
d A B
3L L L
2
q A B
3L L L
2
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79
Recall dynamic model of DC machine
dt
diLiRv
fffff
dd d d e q q
div Ri L L i
dt
q
q q q e d d f
div Ri L L i
dt
Voltage equ. of SM machine
mffa
aaaa iKdt
diLiRV
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Step IV:
80
Rotor and stator flux linkages of SM on abc ref. frame;
Transform the stator flux linkages to the rotor (d-q) ref. frame;
Machine voltage equations derived from flux linkage
equations;
Derive the equation of output power from instantaneous input
power;
Derivation of torque equation from output power and
mechanical speed.
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The developed power
81
a a b b c c
d d q q
P v i v i v i
3v i v i
2
Power input to the machine and the developed torque
The factor 3/2 in the power is because of the factor 2/3 in the abc-dq transformation for both voltage and current.
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The developed power
82
a a b b c c
2 2 2d d
d q
q d
2 2 2q q
P v i v i v i
=v i cos cos 120 cos 240
-v i cos sin cos 120 sin 120 cos 240 sin 240
-v i cos sin cos 120 sin 120 cos 240 sin 240
+v i sin sin 120 sin 240
q q q
q q q q q q
q q q q q q
q q q
d d
d q q d
q q
cos 2 240 1 cos 2 480 1cos2 1 =v i
2 2 2
- v i v i 0.5sin2 0.5sin 2 240 0.5sin 2 480
1-cos 2 240 1-cos 2 4801-cos2 +v i
2 2 2
q qq
q q q
q qq
0
3/2
3/2
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The developed power
qdd q q d d q
2 2d q
d3 d 3 dP i i i i
2 dt dt 2 dt
3 i i R
2
q
We expect to see only current in the torque equation.
q 2 2dd d q q d d q q
didi d 1 d 11st term L i L i L i L i
dt dt dt 2 dt 2
Represent rate of change of stored energy in the inductors
Copper loss
q
q q e d
dv Ri
dt
dd d e q
dv Ri
dt
d d d fL i
q q qL i
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The developed power
qdd q q d d q
2 2d q
d3 d 3 dP i i i i
2 dt dt 2 dt
3 i i R
2
q
q d d q
32nd term i i
2
This term being the product of the back emf and currents of the d- and q-windings, is the developed power of the machine.
back emf
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Step V:
85
Rotor and stator flux linkages of SM on abc ref. frame;
Transform the stator flux linkages to the rotor (d-q) ref. frame;
Machine voltage equations derived from flux linkage
equations;
Derive the equation of output power from instantaneous input
power;
Derivation of torque equation from output power and
mechanical speed.
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dev dev q d d q
f q d q q d
3 pT P / i i
2
3 pi L L i i Nm
2
For a non-salient pole synchronous machine, Ld = Lq
dev f q
3T p i
2
86
For a machine with p pole pairs.
The developed torque
dev q d d q
3 dP i i
2 dt
q
aT K iCompare to DC machine torque
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Steps to Model Dynamics of SM
89
Clarke and Park Transformation, A
2. Obtain the dq currents from the state equations.
dd d e q d
e fq q qe dq
dL
i v R L i 0dt
i v id L RL
dt
3. Obtain the developed torque from
dev f q
3T p i
2
4. Obtain speed by integrating dev L
d 1T D T sign
dt J
5. dq flux linkages d d d fL i
q q qL i
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Steps to Model Dynamics of SM
90
6. Find θ by integrating ω
7. Use the θ to recalculate dq voltage for the next integration step.
8. Repeat Step 2-7
9. Continue until the end of the duration of modeling.
10. Obtain actual voltages, currents and flux linkages in the abc
reference frame with the inverse of A.
1 0 0
0 0
cos sin 1
A cos 120 sin 120 1
cos 240 sin 240 1
q q
q q
q q
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91
Review of steady state analysis of DC machine Review of dynamics of Separately Excited (SE) DC machine
Dynamics of Synchronous Machine (SM)
Rotor flux oriented control (RFOC) of SM
Dynamics of Induction Machine (IM)
Rotor Flux Oriented (FOC) Vector Control of IM
Outlines
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Torque control using id and iq controls
d
** * *d
d d e q q
div Ri L L i
dt
*
q* * *
q q q e d d f
div Ri L L i
dt
These equations are coupled and non-linear.
Back emf
dev f q d q q d
3pT i L L i i Nm
2
dev f q
3T p i Nm
2
d d d fL i q q qL i 2 2
s d q 92
for a SP SM
for a NSP SM
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Rotor flux oriented MTPA control of IPM
93
2
f s q d s
dT 3 3I sin p( L L )I cos 2 0
d 2 2
2
f s q d s
3 3T I cos p( L L )I sin 2
2 4
2 2 2
f f q d q
d
q d
2
f f 2
q2
q d q d
4( L L ) ii
2( L L )
i2( L L ) 4( L L )
2 2
s d qI i i
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Vector or rotor flux oriented control of the SM
dq-1
*qi
*di
*av
*bv
*cv
d/dt
PWM
Inverter
q
q
*ai
*bi
*ci
* T *
s
Current
Reference
Generator
ia - ic
SMSpeed
Controller
Current
Controllers
94
• In servo drive, id is maintained at a constant value corresponding to the rated flux.
• In PM and large air gap motor, id is maintained at 0 (λf>>idLd). • In field weakening, id is maintained at negative values.
AC dev f q
3T p i Nm
2
d d d fL i q q qL i 2 2
s d q
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Vector or rotor flux oriented control of the SM
95
** * dd d d e q q
div Ri L L i
dt
*
q* *
q q q e d d f
div Ri L L i
dt
De-coupling compensation results in faster dynamics of current (and hence torque) control.
dq
*qi
*di
*av
*bv
*cv
w
q
w*
T *
Current
Ref
Gen
ia
SMSpeed
Controller
dq current
Controllers
w
ic
ib
d/dt
+
-
+
-
iq
id
PWM
Inverter
*qv
*dv
*
s
dq-1
e q qL i
-
e d d fL i
+
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Vector or rotor flux oriented control of the SM
96
With de-coupling compensation
Without de-coupling compensation
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Example of RFOC SM
97
A 10-pole, 50Hz, Surface mounted PMSM, Ef= 115 Vrmsl-l/krpm, Irated=4.17 Arms, Imax=6 A (peak) within the rated speed. The developed torque and stator flux linkage of such a motor under rotor flux oriented control (without field weakening)
1.5 f qsT p i
ds d ds fL i
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Example of RFOC SM
98
(a) Calculate the rotor flux linkage, λf.
115 2 30.18 V/rad/s
5 1000 30f
(b) Calculate the stator current reference ids in the rotor reference frame, so that the stator flux linkage d along the rotor d-axis remains constant at all times.
* 0 so that 0.18ds ds fi
(c) Calculate the stator current reference for iqs if the motor is to develop 8 Nm of torque. And the maximum developed torque?
1.5 5 5 Nmf qsT i 5 1.5 5 0.18 3.7 Aqsi
max ,max1.5 5 1.5 5 0.18 6 8.1 Nmf qsT i
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Example of RFOC SM
99
(d) Sketch the torque and flux-linkage control schemes in which the stator flux-linkage must be maintained at f.
Voltage
Source
Inverter
PI
*
qi
ˆqi
* 0di *
dsv
*
qsv
PIˆdi ˆ
req
-+
*
anv
*
bnv
-+
abc
dq
d−q
abc
EPMSM
ˆreq
*
cnv
asi
bsi
csi
Pp
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Simulation of Vector or RFOC of PMSM
100
Vector control: Stator currents are identified as two orthogonal components (dq), representing a vector. RFOC: The d component defines the magnetic flux and q the torque. d axis is aligned with the electrical position of the rotor flux.
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Simulation of Vector or RFOC of PMSM
101
vd
Current controller step response
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Simulation of Vector or RFOC of PMSM
102
Speed controller step response And load disturbance response
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Review of Dynamics of SM
103
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104
0 0
0 0
cos cos 120 cos 240
2A sin sin 120 sin 240
31 1 1
2 2 2
q q q
q q q
Forward(abcdq) and reverse (dqabc) transforms
1 0 0
0 0
cos sin 1
A cos 120 sin 120 1
cos 240 sin 240 1
q q
q q
q q
a
a’
b
b’
c
c’θ
ia
ib
ic
ea
eb
ec
Axis of
phase ‘a’
mmf
d-axis;
axis of
rotor mmf
q-axis;
orthogonal
to d-axis
fi
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Torque control using id and iq controls
** * *dd d d e q q
div Ri L L i
dt
*
q* * *
q q q e d d f
div Ri L L i
dt
These equations are coupled and non-linear.
Back emf
dev f q d q q d
3pT i L L i i Nm
2
dev f q
3T p i Nm
2
d d d fL i q q qL i 2 2
s d q 105
for a SP SM
for a NSP SM
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Vector or rotor flux oriented control of the SM
106
** * dd d d e q q
div Ri L L i
dt
*
q* *
q q q e d d f
div Ri L L i
dt
De-coupling compensation results in faster dynamics of current (and hence torque) control.
dq
*qi
*di
*av
*bv
*cv
w
q
w*
T *
Current
Ref
Gen
ia
SMSpeed
Controller
dq current
Controllers
w
ic
ib
d/dt
+
-
+
-
iq
id
PWM
Inverter
*qv
*dv
*
s
dq-1
e q qL i
-
e d d fL i
+
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107
Review of steady state analysis of DC machine Review of dynamics of Separately Excited (SE) DC machine
Dynamics of Synchronous Machine (SM)
Rotor flux oriented control (RFOC) of SM
Dynamics of Induction Machine (IM)
Rotor Flux Oriented (FOC) Vector Control of IM
Outlines
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Dynamics of Induction Machines
108
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Review of SM Working Principle
109
The rotating magnetic field rotates at synchronous speed, like a N-S poles rotating at the same speed.
Rotor&stator poles repel each other get aligned with the opposite poles
Rotor&stator poles interlocked Rotating at synchronous speed
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Working Principle of IM
110
• Rotating magnetic field at the synchronous speed • Closed rotor windings (wound, squirrel cage), emf I F • Rotor cutting rotating magnetic field relative speed, slip s
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Why Do we Need the Dynamic Model of an IM
111
• Scalar control methods such as VVVF and slip power recovery
schemes are not instantaneous control of torque .
• VSD/VFD drives require high dynamic performance (fast acceleration
and deceleration), like in a servo system
• The vector control of an IM is based on the decoupling between the
current components used for generating magnetizing flux and torque.
• The decoupling allows the induction motor to be controlled as a simple
DC motor and high dynamic performance, comparable to that of a DC
motor.
• Vector control uses machine dynamic model rather than steady-state
model (scalar control) .
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Reference Frame Transformation in an IM
112
• Transform 3-ph sinusoidal quantities of stator windings and rotor windings to an orthogonal reference frame separately (abcsdqs, abcrdqr).
• Pick a rotating reference frame synchronously rotating reference frame (ωs, ωs≠ωr);
• For IM, the steps of the transformation are the same as SM except for inductance expression (much simpler).
• The stator voltage (dq) equations of IM should be the same as SM, but the rotor voltage equations are a little different.
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Dynamic model of an IM in the synchronously rotating reference frame
0
t
s odtq q
q is the angle of the
synchronously
rotating d-axis with
respect to the ‘a’
stator winding axis.
113
iar
idr
iqr
ibr
icr
ids
ibs
ics
iqs
ias
r
s
s
qr
ids /idr
q
iqs /iqr
![Page 103: Section 6. Dynamics of Electric Drive Systems Section 6 - Dynamics... · DCM has two windings (field and armature in a SE DC motor) SM has three-phase stator windings. ... Review](https://reader034.vdocuments.us/reader034/viewer/2022051509/5aef71447f8b9ac62b8d720a/html5/thumbnails/103.jpg)
Axes transformation
120 240
120 240
ds as
qs bs
cso
cos cos cosf f2
f sin sin sin f3
f1 1 1f
2 2 2
q q q
q q q
s as
s bs
csos
1 11
2 2f f
2 3 3f = 0 f
3 2 2ff 1 1 1
2 2 2
114
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Assumptions & machine inductances
Balanced windings, uniform air-gap and linear magnetic field.
Stator winding self-inductances, Laas= Lbbs=Lccs=L1 (LB=0), independent of
the angular position of the rotor.
Rotor winding self inductances, Laar = Lbbr = Lccr = L2
Mutual inductances between stator windings, Labs = Lbcs = Lcas = M1
Mutual inductances between rotor windings, Labr = Lbcr = Lcar = M2
The mutual inductances between stator and rotor windings (M) have
cosine variation with qr.
Thus, Lasar = Mcosqr, ; Lbsar = Mcos(qr −120°) and so on.
115
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Compare Self Winding Inductances
aa A BL L L cos 2q
bb A BL L L cos 2 120q
cc A BL L L cos 2 240q
116
1aas bbs ccsL L L L
2aar bbr ccrL L L L
Salient Pole SM IM
Dependent on rotor position Independent of rotor position Constant
fL
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Compare Mutual Inductances between Stator
117
Salient Pole SM IM
Dependent on rotor position Independent of rotor position Constant
ab ba A B
1L L L L cos 2 30
2q
bc cb A B
1L L L L cos 2 90
2q
ca ac A B
1L L L L cos 2 150
2q
1abs bcs casL L L M
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Compare Mutual Inductances between Rotor
118
Salient Pole SM IM
No mutual inductance between the rotor windings
Independent of rotor position Constant
2abr bcr carL L L M
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Compare Mutual Inductances Stator- Rotor
119
Salient Pole SM IM
Dependent on rotor position Dependent of rotor position
;
120
240
( )
( );
( )
asar bsbr cscr r
bsar csbr ascr r
csar asbr bscr r
L L L Mcos
L L L Mcos
L L L Mcos
q
q
q
0cf fc mL L L cos 240q
0bf fb mL L L cos 120q
af fa mL L L cosq
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Compare Mutual Inductances between Rotor-Stator
120
Salient Pole SM IM
Dependent on rotor position Dependent of rotor position
;
240
120
( )
( );
( )
aras brbs crcs r
bras crbs arcs r
cras arbs brcs r
L L L Mcos
L L L Mcos
L L L Mcos
q
q
q
0cf fc mL L L cos 240q
0bf fb mL L L cos 120q
af fa mL L L cosq
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Dynamic model of an IM in the synchronously rotating reference frame
121
iar
idr
iqr
ibr
icr
ids
ibs
ics
iqs
ias
r
s
s
qr
ids /idr
q
iqs /iqr
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Flux linkages
For stator:
1 1
cos cos 240 cos 120
as as bs cs
ar r br r cr r
L i M i i
M i i i
q q q
1 1
cos 120 cos cos 240
bs bs as cs
ar r br r cr r
L i M i i
M i i i
q q q
1 1
cos 240 cos 120 cos
cs cs as bs
ar r br r cr r
L i M i i
M i i i
q q q
qr is the angular displacement of the rotor a-axis with respect to stator a-
axis.
r r edt 1 s dtq 122
0as bs csi i i
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2 2
cos cos 120 cos 240
ar ar br cr
as r bs r cs r
L i M i i
M i i i
q q q
2 2
cos 240 cos cos 120
br br ar cr
as r bs r cs r
L i M i i
M i i i
q q q
2 2
cos 120 cos 240 cos
cr cr ar br
as r bs r cs r
L i M i i
M i i i
q q q
For rotor:
1 1sL L M
2 2rL L M
123
Flux linkage contd.
0ar br cri i i
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cos cos 240 cos 120as s as ar r br r cr rL i M i i i q q q
cos 120 cos cos 240bs s bs ar r br r cr rL i M i i i q q q
cos 240 cos 120 coscs s cs ar r br r cr rL i M i i i q q q
cos cos 120 cos 240ar r ar as r bs r cs rL i M i i i q q q
cos 240 cos cos 120br r br as r bs r cs rL i M i i i q q q
cos 120 cos 240 coscr r cr as r bs r cs rL i M i i i q q q
124
Rotor flux linkages
Stator flux linkages
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Stay-awake Questions
q
q
axis
d
axisq
cos cos 120 cos 240
2sin sin 120 sin 240
3
1/ 2 1 / 2 1 / 2
sA
q q q
q q q
125
Transform 3-ph stator currents to the synchronously rotating reference
frame (iabcs idqs )
1 0 0
s
0 0
cos sin 1
A cos 120 sin 120 1
cos 240 sin 240 1
q q
q q
q q
0
t
s odtq q
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Stay-awake Questions
126
Transform 3-ph rotor currents to the synchronously rotating reference frame
(iabcr idqr ) sl
e e r
ds
dt
q
=
sl e
e r slo
s dt
dt
q
q
0ar br cr ori i i i
cos cos 120 cos 240
2sin sin 120 sin 240
3
1/ 2 1 / 2 1 / 2
sl sl sl
r sl sl slA
q q q
q q q
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0ar br cr ori i i i
127
sle e r
ds
dt
q
=
sl e
e r slo
s dt
dt
q
q
Stay-awake Questions
Transform rotor currents from the synchronously rotating to the 3-ph
reference frame (iabcr idqr )
1
cos sin 1
cos 120 sin 120 1
cos 240 sin 240 1
sl sl
r sl sl
sl sl
A
q q
q q
q q
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128
Stator flux linkages
1
0
cos cos 240 cos 120
cos 120 cos cos 240
cos 240 cos 120 cos
r r r dr
ds ds
s s r r r r qr
qs qs
r r r r
ii
L MA A ii
i
q q q
q q q
q q q
cos( ) cos 120 cos 240 cos sin 1
sin( ) sin( 120 ) sin( 240 ) cos 120 sin 120 1
0 0 0 cos 240 sin 240 1
sl sl sl sl sl
sl sl sl sl sl
sl sl
q q q q q
q q q q q
q q
cos cos 240 cos 120
cos 120 cos cos 240
cos 240 cos 120 cos
as as r r r ar
bs s bs r r r br
cs cs r r r cr
i i
L i M i
i i
q q q
q q q
q q q
3 / 2 0 0
0 3 / 2 0
0 0 0
3
2
ds ds dr
s
qs qs qr
i iL M
i i
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Machine Stator voltages
as s as as
dv R i
dt
bs s bs bs
dv R i
dt
cs s cs cs
dv R i
dt
Non-linear differential equations because
of coefficients which have trigonometric
terms of qr.
Can these equations have constant
coefficients by transforming current and
voltage from abcdq0?
129
0 0
ds as ds as
qs s bs s qs s bs
s cs s cs
v v id
v A v R i Adt
v v i
1 1 1
0 0 0
as ds ds ds
s bs s s qs s s qs s s qs
cs s s s
d d d dA A A A A A A
dt dt dt dt
' ' 'AB A B AB
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Machine Stator voltages
130
0 0
sin cos 0 1 0 0
sin 120 cos 120 0 0 1 0
sin 240 cos 240 0 0 0 1
as ds ds
s bs e s qs qs
cs s s
d dA A
dt dt
q q
q q
q q
cos ' sind
dt
qq q
0 0
0 1 0 1 0 0
1 0 0 0 1 0
0 0 0 0 0 1
as ds ds
s bs e qs qs
cs s s
d dA
dt dt
0 0 0 0
1 0 0 0 1 0
0 1 0 1 0 0
0 0 1 0 0 0
ds ds ds ds
qs s qs qs e qs
s s s s
v id
v R idt
v i
ds s ds ds e qs
dv R i
dt
qs s qs qs e ds
dv R i
dt
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131
Rotor flux linkages
1
0
cos cos 120 cos 240
cos 240 cos cos 120
cos 120 cos 240 cos
r r r ds
dr dr
r r r r r s qs
qr qr
r r r s
ii
L MA A ii
i
q q q
q q q
q q q
cos( ) cos 120 cos 240 cos sin 1
sin( ) sin( 120 ) sin( 240 ) cos 120 sin 120 1
0 0 0 cos 240 sin 240 1
q q q q q
q q q q q
q q
cos cos 120 cos 240
cos 240 cos cos 120
cos 120 cos 240 cos
ar ar r r r as
br r br r r r bs
cr cr r r r cs
i i
L i M i
i i
q q q
q q q
q q q
3 / 2 0 0
0 3 / 2 0
0 0 0
3
2
dr dr ds
r
qr qr qs
i iL M
i i
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Machine Rotor voltages
ar r ar ar
dv R i
dt
br r br br
dv R i
dt
cr r cr cr
dv R i
dt
Non-linear differential equations because
of coefficients which have trigonometric
terms of qr.
Can these equations have constant
coefficients by transforming current and
voltage from abcdq0?
132
0 0
dr ar dr ar
qr r br r qr r br
r cr r cr
v v id
v A v R i Adt
v v i
1 1 1
0 0 0
ar dr dr dr
r br r r qr r r qr r r qr
cr r r r
d d d dA A A A A A A
dt dt dt dt
' ' 'AB A B AB
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Machine Rotor voltages
133
0 0
sin cos 0 1 0 0
sin 120 cos 120 0 0 1 0
sin 240 cos 240 0 0 0 1
ar sl sl dr dr
r br e r r sl sl qr qr
cr sl sl r r
d dA A
dt dt
q q
q q
q q
cos ' sin sinslsl sl sl e r
d
dt
qq q q
0 0
0 1 0 1 0 0
1 0 0 0 1 0
0 0 0 0 0 1
ar dr dr
r br e r qr qr
cr r r
d dA
dt dt
0 0 0 0
1 0 0 0 1 0
0 1 0 1 0 0
0 0 1 0 0 0
dr dr dr dr
qr r qr qr e r qr
r r r r
v id
v R idt
v i
dr r dr dr e r qr
dv R i
dt
qr r qr qr e r dr
dv R i
dt
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Flux linkages and voltages in synchronous dq frame
ds s ds m drL i L i
qs s qs m qrL i L i
2 2s ds qs
dr r dr m dsL i L i
qr r qr m qsL i L i
2 2r dr qr
ds s ds ds e qs
dv R i
dt
qs s qs qs e ds
dv R i
dt
dr r dr dr e r qr
dv R i
dt
qr r qr qr e r dr
dv R i
dt
After a lot of trigonometric manipulations, and using 3
2mL M
134
For stator For rotor
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Flux linkages and voltages in synchronous dq frame
ds s ds s ds m dr e s qs m qr
dv R i L i L i L i L i
dt
qs s qs s qs m qr e s ds m dr
dv R i L i L i L i L i
dt
dr r dr r dr m ds e r r qr m qs
dv R i L i L i L i L i
dt
qr r qr r qr m qs e r r dr m ds
dv R i L i L i L i L i
dt
135
For stator:
For rotor
Replacing fluxes in terms of current
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Dynamic equivalent circuits in dq-axes
s ls mL L L r lr mL L L
+ +
Rs Llr =Lr - Lm Lls =Ls - Lm
Lm
(e - r)dr eds Rr
iqs iqr
qs qr
vqr vqs
137
Part of the self flux linkage of each winding is leakage flux that does not cross the air gap. Thus,
qr r qr e r dr r m qr m qr qs
d dv R i L L i L i i
dt dt
qs s qs e ds s m qs m qs qr
d dv R i L L i L i i
dt dt
qsd
dt
qrd
dt
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Dynamic equivalent circuits in dq-axes
s ls mL L L r lr mL L L
+ +
Rs Llr Lls
Lm
(e - r)qr eqs Rr
ids idr
ds dr
vdr vds
138
Part of the self flux linkage of each winding is leakage flux that does not cross the air gap. Thus,
ds s ds e qs s m ds m ds dr
d dv R i L L i L i i
dt dt
dr r dr e r qr r m dr m dr ds
d dv R i L L i L i i
dt dt
dsd
dt
drd
dt
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The developed power and torque
Ws a a b b c cp v i v i v i
139
The power input to the 3-ph stator is given by
With abcdq0 transformation, it becomes
3
W2
s ds ds qs qsp v i v i
Substituting stator dq voltages yields
2 23
2
s s ds qs s ds ds qs qs
m ds dr qs qr e ds qs qs ds
d dp R i i L i i i i
dt dt
d dL i i i i i i
dt dt
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The developed power and torque
140
3
mr dr ds qr qs m ds ds qs qs
r
e r r qr ds m qs ds r dr qs m ds qs
L d drd term R i i i i L i i i i
L dt dt
L i i L i i L i i L i i
For a squirrel-cage rotor, 0dr qrv v
0 r dr r dr m ds e r r qr m qs
dR i L i L i L i L i
dt
0 r qr r qr m qs e r r dr m ds
dR i L i L i L i L i
dt
1
dr r dr m ds e r r qr m qs
r
d di R i L i L i L i
dt L dt
1
qr r qr m qs e r r dr m ds
r
d di R i L i L i L i
dt L dt
mp 4 term= e m dr qs qr dsth L i i i i
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The developed power and torque
3
2
3
2
mm e r r qr ds m qs ds r dr qs m ds qs
r
e m dr qs qr ds
Lp L i i L i i L i i L i i
L
L i i i i
141
The electromechanical power is given by
3
2m m r dr qs qr dsp L i i i i
3 3
2 2
m mdev m dr qs qr ds dr qs qr ds
r r
p LT pL i i i i p i i
p L
dr r dr m dsL i L i
qr r qr m qsL i L i
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The developed power and torque
142
A simple way to find the power associated with speed (motional)
voltages is from the equivalent dynamic circuit.
3
2m e ds qs e r dr qr e qs ds e r qr drp i i i i
+ +
Rs Llr =Lr - Lm Lls =Ls - Lm
Lm
(e - r)dr eds Rr
iqs iqr
qs qr
vqr vqs
+ +
Rs Llr Lls
Lm
(e - r)qr eqs Rr
ids idr
ds dr
vdr vds
dr r dr m dsL i L i
qr r qr m qsL i L i
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The developed power and torque
143
3
2m e ds qs e qs ds e r ds m qr e r qs m drp i i i L i i L i
3
2m e ds qs e qs ds e r ds qs s qs e r qs ds s dsp i i i L i i L i
m qr qs s qsL i L i
m dr ds s dsL i L i
3
2m r ds qs r qs dsp i i
3
2
mdev ds qs qs ds
r
p pT i i
p
The mechanical output power is given by
The developed electromagnetic torque is given by
In terms of stator variables
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The developed power and torque
144
3
2m e dr qr r qr e qr dr r dr e r dr qr e r qr drp i L i i L i i i
m qs qr r qrL i L i
m ds dr r drL i L i
3
2m r qr dr r dr qrp i i
3
2
mdev qr dr dr qr
r
p pT i i
p
3
2m e ds qs e r dr qr e qs ds e r qr drp i i i i
ds s ds m drL i L i
3
2m e qs s ds m dr e ds s qs m qr e r dr qr e r qr drp i L i L i i L i L i i i
In terms of rotor variables
qs s qs m qrL i L i
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145
Review of steady state analysis of DC machine Review of dynamics of Separately Excited (SE) DC machine
Dynamics of Synchronous Machine (SM)
Rotor flux oriented control (RFOC) of SM
Dynamics of Induction Machine (IM)
Rotor Flux Oriented (FOC) Vector Control of IM
Outlines
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Review of Dynamics of IM
146
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147
Self and Mutual Inductances of IM
1aas bbs ccsL L L L 2aar bbr ccrL L L L
1abs bcs casL L L M 2abr bcr carL L L M
;
120
240
( )
( );
( )
asar bsbr cscr r
bsar csbr ascr r
csar asbr bscr r
L L L Mcos
L L L Mcos
L L L Mcos
q
q
q
;
240
120
( )
( );
( )
aras brbs crcs r
bras crbs arcs r
cras arbs brcs r
L L L Mcos
L L L Mcos
L L L Mcos
q
q
q
Stator windings Rotor windings
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Dynamic model of an IM in the synchronously rotating reference frame
148
iar
idr
iqr
ibr
icr
ids
ibs
ics
iqs
ias
r
s
s
qr
ids /idr
q
iqs /iqr
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149
cos cos 120 cos 240
2sin sin 120 sin 240
3
1/ 2 1/ 2 1/ 2
sA
q q q
q q q
1 0 0
s
0 0
cos sin 1
A cos 120 sin 120 1
cos 240 sin 240 1
q q
q q
q q
Dynamic model of an IM in the synchronously rotating reference frame
cos cos 120 cos 240
2sin sin 120 sin 240
3
1/ 2 1/ 2 1/ 2
sl sl sl
r sl sl slA
q q q
q q q
1
cos sin 1
cos 120 sin 120 1
cos 240 sin 240 1
sl sl
r sl sl
sl sl
A
q q
q q
q q
abcsdq0s dq0sabcs
abcrdq0r dq0rabcr
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Flux Linkages and Voltages of IM
ds s ds m drL i L i
qs s qs m qrL i L i
2 2s ds qs
dr r dr m dsL i L i
qr r qr m qsL i L i
2 2r dr qr
ds s ds ds e qs
dv R i
dt
qs s qs qs e ds
dv R i
dt
dr r dr dr e r qr
dv R i
dt
qr r qr qr e r dr
dv R i
dt
After a lot of trigonometric manipulations,
150
For stator For rotor
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151
3 3
2 2
m mdev m dr qs qr ds dr qs qr ds
r r
p LT pL i i i i p i i
p L
Developed Torque of IM
+ +
Rs Llr =Lr - Lm Lls =Ls - Lm
Lm
(e - r)dr eds Rr
iqs iqr
qs qr
vqr vqs
+ +
Rs Llr Lls
Lm
(e - r)qr eqs Rr
ids idr
ds dr
vdr vds
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152
RFOC (Rotor Flux Oriented Control)
3
2
mdev dr qs qr ds
r
LT p i i
L
1.5dev f qsT p i
Recall developed torque of non-SP SM
0qr
r dr
Comparing to the developed torque of IM
3
2
mdev r qs
r
LT p i
L
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Conditions for rotor flux oriented control (RFOC)
For the squirrel-cage motor, vqr and vdr are both zero.
0qr
r qr e r dr
dR i ( )
dt
0drr dr e r qr
dR i ( )
dt
1 mqr qr qs
r r
Li i
L L
1 mdr dr ds
r r
Li i
L L
Eliminating iqr and idr (induced currents), which are not accessible
and hence cannot be controlled, using
153
(a)
(b)
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qr mrqr r qs e r dr
r r
d LLR i ( ) 0
dt R L
dr mrdr r ds e r qr
r r
d LRR i ( ) 0
dt L L
qr 0 r dr̂
We require all the rotor flux to be in the rotor d-axis.
so that
Also, the rotor flux should remain constant. Thus
qrdrdd
0dt dt
154
mr qs e r r
r
L ˆR i ( ) 0L
m re r sl qs
rr
L Ri
ˆ L
The first rotor voltage equation becomes
(1)
(b)(a)
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2
m mdev dr qs qr ds r qs
r r
L L3P 3 P ˆT i i i2 L L
r rr m ds
r
ˆL d ˆ L iR dt
155
mr rr r ds
r r
ˆ Ld R ˆ R i 0dt L L
The second rotor voltage equation becomes
Rotor flux λr is determined by ids, subject to a time delay Tr which is the rotor time constant (Lr/Rr).
Current iqs controls the developed torque T without delay.
2m m
qs s qs m qr s qs qrr r
L LL i L i L i
L L
2m m
ds s ds m dr s ds drr r
L LL i L i L i
L L
3
2dev ds qs qs ds
pT i i
qr 0 r dr̂ v
v v
(2)
(3)
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156
• ids and iqs are orthogonal to each other and called the flux and
torque-producing currents.
• RFOC is achieved by aligning the d-axis of the synchronous
reference frame with the rotor flux vector λr (λdr=|λr|, λqr=0
and dλdr/dt= dλqr/dt=0).
• Ids=CONST for operation up to the base speed. It is reduced in
order to weaken the rotor flux (constant-power-like
characteristic).
• Based on how the rotor flux is detected and regulated, indirect
rotor flux oriented control (IFOC) method and the direct vector
control method.
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Direct RFOC
157
In direct FOC, rotor flux angle θ is obtained by using flux-sensing
devices embedded inside the motor or using measured motor
terminal voltages and currents.
The requirement for accurate air-gap flux sensors with ability to
reject the effects of slot ripples are significant problems.
Also, the necessity for mounting additional search coils in the air-
gap which requires machine modifications have precluded the
adoption of the direct method.
Estimation Error in the rotor flux and angle comprises of a drift
produced by the integrator because of initial conditions and
terminal voltage and/or phase current sensor measurement offset
error.
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Indirect RFOC
160
In the indirect RFOC, the rotor flux angle θ is obtained from
detected rotor position angle θr and calculated slip angle θsl :
θ=θr+θsl
Terminal voltages sensors or flux sensors are not needed.
Please note the terminal voltages are PWM pulse trains (amplitude
is ±Vdc) and the flux calculation only needs the fundamental
component of the terminal voltage, which normally requires a low
pass filter or is estimated using DC bus voltage and duty cycle of
the switching signals.
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Indirect RFOC scheme 1
161
r rr m ds
r
ˆL d ˆ L iR dt
* *m rsl qs
rr
L Ri
ˆ L
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Voltage
Source
Inverter
PI
*
qi
ˆqi
*
di*
dsv
*
qsv
PIˆdi ˆ
eq
-+
*
anv
*
bnv
-+
abc
dq
d−q
abc
EIM
ˆeq
*
cnv
asi
bsi
csi
1/Lm
*
dr
*
2
3
r
m dr
L
PL
*
eT
*
r m
r dr
R L
L +
+
0
t
ed *
sl
ˆre
Ppˆ
rm
e
Indirect RFOC scheme 2
163
* m rsl qs*
rdr
L Ri
L
2
* * *mdev dr qs
r
L3 PT i
L * *
rd m dsL i
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Indirect RFOC scheme
164
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Indirect RFOC scheme
165
vds
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dq Rotor Flux in RFOC scheme
166
Psi_qr
ωs
ωr
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Dynamic Model
167
( )ABC dqo sv v v A
Solve diff equations (6.3.22) for ids and iqs
1.
2.
mdev m L m
d 1T D T si gn
dt J
3.
r = pm . 4.
r sl oq q 5.
6. Repeat steps 2-5, taking values of variables in the current step as initial values for the next step.
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Dynamic Model
168
s s e s m e mds ds
e s s s e m mqs qs
dr drm e r r r e r r
qr qre r m m e r r r r
d dR L L L Lv i
dt dt
d dL R L L Lv i
dt dt
d dv iL R L Ldt dt
d dv iL L L R L
dt dt
(6.3.22)
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Example of RFOC IM
170
50Hz parameters of a 415V/50Hz, 4-pole, squirrel-cage IM are: 𝑅𝑠 = 3.257 Ω; 𝑅𝑟 = 3.392 Ω; 𝐿𝑠 = 𝐿𝑟 = 589.9 mH; 𝐿𝑚 =569.5 mH; 𝑁𝑟 = 1450 rpm; 𝐼𝑟𝑎𝑡𝑒𝑑 = 5.8 Arms. The maximum current allowed in the machine is 2*𝐼𝑟𝑎𝑡𝑒𝑑. Equations of IM under Indirect RFOC (without field weakening), are given by
drrdr m ds
r
dLL i
R dt
m rsl e re qs
dr r
L Ri
L
2
mdev dr qs
r
L3 PT i
L
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Example of RFOC SM
171
(a) Calculate the approximated value of the rated rotor flux linkage and stator current reference of 𝑖𝑑𝑠.
ph,* * 415 2 31.08 Wb-t
50 2
peak
r dr
e
V
(b) Calculate the stator current reference for 𝑖𝑞𝑠 if the motor is to
develop 20 Nm of torque. And maximum developed torque under rated rotor flux linkage.
* *
*
2 2*589.9*20 6.39A
3*2*569.5*1.083P
rqs e
m dr
Li T
L
*max max
3P1.5*2*569.5 / 589.9*1.08*16.3 51Nm
2
me qsdr
r
LT i
L
** 1.08
1.9 A0.5695
drds
m
iL
2
* 2 2 2max s max ds 2*5.8* 2 1.9 16.3Aqsi i i
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Voltage
Source
Inverter
PI
*
qi
ˆqi
*
di*
dsv
*
qsv
PIˆdi ˆ
eq
-+
*
anv
*
bnv
-+
abc
dq
d−q
abc
EIM
ˆeq
*
cnv
asi
bsi
csi
1/Lm
*
dr
*
2
3
r
m dr
L
PL
*
eT
*
r m
r dr
R L
L +
+
0
t
ed *
sl
ˆre
2ˆ
rm
e
-+
ˆrm
*
rm
Block Diagram of IRFOC IM Drive
172
(c) Complete the following block diagram for RFOC IM drive.