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Engineering, Technology & Applied Science Research Vol. 8, No. 2, 2018, 2847-2852 2847
www.etasr.com Abdelrehim et al.: Indirect 3D-Space Vector Modulation for a Matrix Converter
Indirect 3D-Space Vector Modulation for a Matrix
Converter
Ahmed Abdelrehim
Department of Electrical Engineering
Alexandria University
Alexandria, Egypt
ahmed.abdelrehim@siemens.com
Mohamed El-Habrouk
Department of Electrical Engineering
Alexandria University
Alexandria, Egypt
eepgmme1@yahoo.com
Samir Deghedie Erfan
Department of Electrical Engineering
Alexandria University
Alexandria, Egypt
deghedie@gmail.com
Karim Hassan Youssef
Department of Electrical Engineering
Alexandria University
Alexandria, Egypt
khmyoussef@yahoo.com
Abstract—This paper discusses the indirect space vector
modulation for a four-leg matrix converter. The four-leg matrix
converter has been proven to be a reliable, cost-effective, and
compact power electronic interface to supply unbalanced or
nonlinear loads. However, the added fourth leg has shifted the
inverter side modulation from simple two-dimension SVM into
complex three-dimension. This paper employs a new technique to
implement indirect 3D SVM in digital controllers with further
simplification in the modulation process. Moreover, Simulink
simulation using repetitive controller has been performed to
regulate the output voltage for 400 Hz Power supplies.
Keywords-repetitive controller; 3D SVM; four-leg matrix
converter
I. INTRODUCTION
The matrix converter is a static and direct AC to AC
converter with unique features of unity input power factor, high
power to volume ratio, high reliability and MTBF factor which
has gained interest in applications aiming to produce a
realization of a compact three-phase drive for military,
industrial and aerospace systems [1-3]. Moreover, researchers
utilized the matrix converter as an electronic interface layer
between all resources (wind, solar, storage, etc.) of the energy
matrix model and as an electronic transformer competing with
the traditional magnetic transformer. The added fourth leg is
placed to provide a return path for the zero-sequence current
during unbalancing and add the capability of supplying
different connected single-phase loads. Four-leg converters
have a superior ability to produce balanced output voltage
waveform even under severely unbalanced load or non-linear
load conditions [4]. A four-leg matrix converter topology is
shown in Figure 1. This paper investigates the indirect space
vector modulation which decouples the modulation into two
stages (rectifier + inverter) without intermediate energy
storage. This decoupling is efficient and allows separate control
to each stage, while as there is no intermediate energy storage,
a proper synchronization between the two stages is mandatory
to fulfill the power balance equation as instantaneous input
power shall be equal to the instantaneous output power for the
load [5]. At high-frequency applications with precise control
requirements as for naval and aerospace applications where the
115V-400Hz system is commonly used, traditional controllers
have failed to achieve a proper regulation, due to the limited
bandwidth so the repetitive controller is introduced as an
optimum solution for this control problem [6].
II. MATRIX CONVERTER MODEL
Matrix converter can be represented mathematically by
matrix M and switches are identified as , where X is the
output phase, Y is the input phase and S is the linking switch
between input and output. Rectifier switches are numbered
from to while inverter side switches are numbered from
to . The rectifier is represented in Figure 1. Governing
equations are:
Vout=M*Vin (1)
Iout=MT
*Iin (2)
Vout=Mi*VDC (3)
VDC=MR*Vin (4)
Vout=Mi*MR*Vin (5)
where , ,	 ,	 ,	 ,	 ,	 ,	 and	 are
output voltage, input voltage, output current, input current, DC
intermediate voltage, inverter side switching matrix, rectifier
side switching matrix, matrix converter switching matrix and
transposed matrix converter switching matrix respectively.
and Mi are described by (6) and (7) respectively:
=
1 3 5
2 4 6
							 (6)
spl
rec
ach
out
ass
A.
con
con
rec
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www.etasr
Fig. 1.
M =
S7 S8
S9 S1
S11 S1
S13 S1
M equals to M
M =
S7 S8
S9 S10
S11 S12
S13 S14
Equation (8)
=
S1 ∗ S7 S2
S1 ∗ S9 S2
S1 ∗ S11 S2
S1 ∗ S13 S2
=
SaA SaB
SbA SbB
ScA ScB
SnA SnB
In Figure 1 v
The mathema
Fig. 2.
III. INDIREC
Indirect spac
litting the mo
ctifying stage
hieve decoupl
tput voltage
sumption of vi
Rectifying St
The main fu
ntrol on the d
ntrol the amp
ctifying stage,
ng, Technology
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Schematic of a f
8
10
12
14
	
Mi*MR:
8
0
2
4
*
S1 S3 S5
S2 S4 S6
can be further
∗ S8 S3 ∗ S7
∗ S10 S3 ∗ S9
∗ S12 S3 ∗ S11
∗ S14 S3 ∗ S13
SaC
SbC
ScC
SnC
voltages are: V
atical modelin
Mathematical
CT SPACE VECT
ce vector mod
odulation into
and the seco
ling between t
control.as per
irtual DC link
tage
unction of the
displacement a
plitude of the
, only two sw
y & Applied Sci
four-leg direct ma
5
6
r synthesized i
7 S4 ∗ S8 S
S4 ∗ S10 S
1 S4 ∗ S12 S5
3 S3 ∗ S14 S5
=
V
V
V
V
and V
ng is summariz
modeling of matr
TOR MODULAT
dulation can b
o two stages,
ond is called
the input curr
r (5) and (9)
as shown in F
e rectifying sta
angle of the in
virtual DC l
witches must b
ience Research
A
atrix converter
(7)
(8)
into
S5 ∗ S7 S6 ∗ S8
5 ∗ S9 S6 ∗ S10
5 ∗ S11 S6 ∗ S1
5 ∗ S13 S6 ∗ S1
(9)
V =
V
V
V
.
zed in Figure 2
rix converter
TION
be implement
the first is
inversion sta
rent control an
and based o
Figure 1.
age is to achi
nput current a
link voltage. I
be closed at a
h V
Abdelrehim et a
8
0
12
14
2.
ted by
called
ge, to
nd the
on the
ieve a
and to
In the
time,
just
sim
num
com
wil
B.
abc
ang
con
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ther
com
mo
the
ind
is n
wil
Fig
vec
sele
the
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rect
mat
The
be
Vol. 8, No. 2, 20
al.: Indirect 3D
t one upper s
multaneously to
mbered from o
mbinations are
l occur as show
Fig. 3. Ni
Rectifier Spac
SVM for the
c to αβ coord
gle by which w
nverter modul
mulation that sw
re is no nee
mmonly hap
dulations as sh
Fig
In Figure 4, θ
actual hexa
dex=Iref/IDC	 ,	 0
no need to syn
l be switched
gure 5. Modula
ctor during t
ections have b
number of th
range of on
tifying stage
trix converter
e displacemen
zero. To impl
018, 2847-2852
D-Space Vector M
switch and on
o avoid short c
one to six as sh
e only allowed
wn in Figure 3
ine switching com
ce Vector Mod
rectifying sta
dination and c
we can define
lation requirem
witching one v
ed to synthes
ppens with
hown in Figur
g. 4. Synthesi
θc is the angle
agon sector,
0<mc<1.	 For
nthesize the re
d during ever
ation process
the time inte
been translated
he current sec
ne to six. To
and one of t
is to have uni
nt angle betwee
lement this, th
2
Modulation for
ne lower swi
circuit. The re
hown in Figure
to guarantee t
3.
mbinations for the
dulation
age works by
calculating th
e the working
ment, it has
vector per sect
size two vect
conventional
re 4.
is of reference cu
e of the refere
mc	 the	 cu
matrix conver
ference vector
ry sector dura
happens by as
erval of eve
d into a train
ctor, numbers
o achieve the
the most inter
ity power facto
en input curren
he reference s
2848
r a Matrix Con
itch can be c
ectifier switche
e 1. Nine switc
that no short c
e rectifying stage
transforming
he reference v
sector. For m
been approve
tor is sufficien
tors per secto
l rectifier
urrent
ence current w
urrent	 modul
rter, mc=1 and
r as just one v
ation as show
ssigning one a
ry sector. V
of pulses car
are represent
e second targ
resting featur
or at the input
nt and voltage
signal given t
verter
closed
es are
ching
circuit
input
vector
matrix
ed by
nt and
or as
SVM
within
lation	
there
vector
wn in
active
Vector
rrying
ted in
get of
res of
t side.
shall
to the
mo
ins
mo
con
app
fun
out
add
the
thr
app
unb
app
neu
rol
leg
coo
inv
the
inv
com
by
tur
(ne
coo
con
be
ana
Pri
vec
A.
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www.etasr
odulation proc
stead of the inp
Fig. 5.
Inversion st
odulation, and
nverter, we w
proach for th
nction of inve
tput voltage
ded fourth leg
e zero-sequenc
ree-phase syste
		+ 		+
And the tra
plied as it ha
balanced syst
plied. Due to
utral current p
le of 3D SVM
gs.
		+ 		+
Transformati
ordination du
version stage,
e same time in
verter with
mbinations ar
p or n for ea
rned on (posi
egative). If th
ordination, th
nventional SV
divided into
alog to secto
ism number m
ctor angle on α
Prism Identif
If
0<θ<60
60<θ<12
120<θ<1
180<θ<24
ng, Technology
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cess has been
put phase curr
. Rectifying s
III. INV
tage is conce
d as this pa
will address
he four-leg
ersion stage i
under balanc
g is responsibl
ce component
em follows (10
		=0
ansformation f
as happened
tem (10) is n
the unbalanc
passing throug
M to provide
		≠ 0
ion to statio
ue to the zer
switches on th
n order to avo
eight switc
re sixteen. Sw
ach leg, where
tive) and n in
he sixteen-ve
he result is
VM are turned
six prisms (F
ors representat
may be ident
αβγ coordinati
fication
the
0 the
80 the
40 the
y & Applied Sci
taken from i
rent.
stage SVM vector
VERSION STAGE
erned with in
aper discusse
the 3D SVM
matrix conve
is to provide
ced and unba
e for providin
t during unbal
0).
from abc to
with the rect
no longer vali
cing of the sy
gh the system
accurate swit
onary frame
ro-sequence c
he same leg ca
oid short circu
ches, the p
itching combi
e p indicates
ndicates the l
ectors are rep
a 3D hexago
into prisms. T
Figures 6-7).
tion on conv
tified by defi
ion.
en P=1
en P=2
en P=3
en P=4
ience Research
A
input phase v
rs selection
E
nverter side
es four-leg m
M as a modu
erter. The pr
a control ove
alanced loads
ng a current pa
lance. The bal
(10
αβ coordinati
tifier stage. F
id and (11) is
ystem, there w
m and it is the
tching pulses
(11
happens into
component. I
an’t be turned
uit. For the fo
possible swit
inations repres
the upper swi
lower switch
presented into
on and secto
The 3D hexago
The prisms a
entional 2D
ining the refe
h V
Abdelrehim et a
oltage
SVM
matrix
ulation
rimary
er the
. The
ath for
lanced
0)
ion is
For an
s now
will be
basic
to all
)
o αβγ
In the
d on at
our-leg
tching
sented
itch is
is on
o αβα
ors of
on can
are an
SVM.
erence
8. E
B.
and
imp
bes
thre
swi
Vol. 8, No. 2, 20
al.: Indirect 3D
240<θ<30
300<θ<36
Vectors are d
Each prism con
Fig. 6. 3D re
Fig.
Fig.
Switching Vec
As the referen
d tetrahedron
plemented by
side each tetr
ee switching v
itching vector
018, 2847-2852
D-Space Vector M
00 then
60 then
distributed into
ntains four act
epresentation of sw
7. Prisms ide
8. Vector dist
ctor Selection
nce vector loca
number, sel
choosing the n
rahedron[8, 9]
vectors, to ca
the reference
2
Modulation for
n P=5
n P=6, where θ
o each prism a
tive vectors.
witching vectors i
entification for 3D
tribution into each
ation is define
ection of sw
nearest referen
]. Each tetrah
alculate the du
e required volt
2849
r a Matrix Con
θ=	tan
as shown in F
in αβγ coordinatio
D SVM
h prism
ed by prism nu
witching vecto
nce vectors lo
hedron consis
uty cycle for
tage is transfo
verter
Figure
on
umber
ors is
ocated
sts of
each
ormed
firs
sw
wh
the
and
ma
var
tetr
po
SV
the
nu
act
(re
cha
rep
rep
tw
ma
val
var
suc
var
Th
op
sho
10
Engineerin
www.etasr
st to αβγ coor
witching vector
V 	
V
V
= d
The duty cyc
d
d
d
= 	 ∗ S
= 1
here S is the d
e reference vec
d d represents
atrix is depend
rying values
rahedron. S m
ssible coincid
VM code check
e current value
The rectifyin
mbers from 1
tive rectifier
ectifier matrix
arge of genera
presenting the
presented on
o matrices as i
atrix converter
Fig. 9. M
A Simulink
lidate the effe
rying types o
ccessfully va
rious scenario
he input and
eration. The s
own in Table
-26.
ng, Technology
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rdination and
rs [9] as per (1
d d
V
V
V
cles can be furt
∗
V 	
V
V
duty cycle mat
ctor, (V1 V2 V3
s the duty cy
dent on the sel
depending
matrix calcula
ence between
ks the prism a
es of S.
IV. MATR
ng stage is de
1 to 6, these n
switches and
x). At the sam
ating another
current active
		 (inverter
in (5) allows u
r. The procedu
Matrix converter
V. SIMUL
k simulation
ectiveness of m
f loads. The
alidated as w
os such as bala
output wavef
simulation was
I. The simula
y & Applied Sci
then is divid
2).
ther calculated
trix [8-10], (V
3)T
is the curren
ycle for each s
lected switchin
on each se
ations have b
prisms and te
and tetrahedron
RIX CONVERTE
edicated to gen
numbers repre
d would be re
me time the in
series of num
e inverter swit
matrix) as we
us to find all p
ure is shown in
code generation f
LINK SIMULATI
was successf
matrix conver
proposed indi
well. Simulati
anced and unb
forms ensured
s carried out u
ation results ar
ience Research
A
ed by the ava
(12
d as shown in
(13
(14
Vα-ref Vβ-ref Vδ-r
nt switching v
switching vec
ng vectors, so
elected prism
been done for
etrahedrons. Th
n number to e
ER
nerating a ser
esenting the c
epresented on
nversion stage
mbers from 1
tches that wou
ell. Multiplyin
possible switch
n Figure 9.
from Mi and MR
ION
fully develop
rter operation
irect 3D SVM
ion worked
balanced linear
d proper con
using the param
re shown in F
h V
Abdelrehim et a
ailable
2)
(13).
3)
4)
ref)T
	 is
vector,
ctor. S
it has
m and
r each
he 3D
extract
ries of
current
n 		
e is in
to 16,
uld be
ng the
hes for
ed to
under
M was
under
r load.
nverter
meters
igures
R
A.
Vol. 8, No. 2, 20
al.: Indirect 3D
Source sys
Load syst
Switching freq
Input filter
Output filter
Repetitive Contr
Tracking con
Unbalanced
Balanced l
Nonlinear l
Non-Linear L
Fig. 12. FF
018, 2847-2852
D-Space Vector M
TABLE I.
tem
em
quency
(LC)
r (LC)
roller Q(z)
ntroller
d load 5Ω
load
load
Load
Fig. 10. O
(a) P
(b) P
(c) P
(d) N
Fig. 11. O
FT analysis for ou
2
Modulation for
SYSTEM PARAM
440V
115V-
1280
56Ω/0.8m
180uH+70
1.72377
1.663
1.868
Ω+5.5mH, 10Ω+6
5Ω +5
3phase diode
Output voltage
Phase A
Phase B
Phase C
Neutral
Output current
utput phase voltag
2850
r a Matrix Con
METERS
V-60Hz
-400Hz
00Hz
mH/10uF
0uH/100uF
2 1
76 0.75754
3 0.9914
8 0.8735
6.2mH, 20Ω+7.5m
5.5 mH
e bridge +50Ω
ge (THD=3.3%)
verter
mH
B.
Engineerin
www.etasr
Fig. 13.
Unbalanced
Fig. 17. Inp
ng, Technology
r.com
FFT analysis fo
Fig. 14.
Load
Fig. 15.
(a) P
(b) P
(c) P
(d)
Fig. 16. O
put current multip
y & Applied Sci
or output current
Error signal
Output voltage
Phase A
Phase B
Phase C
Neutral
Output Currents
plied by factor 50
ience Research
A
(THD=1.8%)
and input voltage
h V
Abdelrehim et a
e
C.
Vol. 8, No. 2, 20
al.: Indirect 3D
Fig. 19.
Fig. 20. FF
Non Linear L
F
Fig. 22.
018, 2847-2852
D-Space Vector M
Fig. 18.
FFT analysis fo
FT analysis for ou
Load
Fig. 21. Output
FFT analysis fo
2
Modulation for
Error signal
or input current (T
utput phase voltag
t voltage 115V/40
or input current (T
2851
r a Matrix Con
THD=48%)
ge (THD=3.3%)
00H
THD=48%)
verter
mo
bee
con
lim
(11
con
eff
rep
vo
[1]
[2]
[3]
[4]
[5]
[6]
[7]
Engineerin
www.etasr
Fig
Fig. 25. Inp
This paper
odulation for
en implement
ntroller was s
mited bandw
15V/400Hz).
nditions (bal
fectiveness o
petitive contro
ltage in an exc
P. Zanchetta,
Empringham, “
AC power s
Electronics Sp
16, 2005
C. Klumpner,
process of th
Electronics Sp
1083–1088, Ju
D. Casadei, G
torque control
Electronics, Vo
F. Yue, P. W. W
space vector m
Electronics Co
R. Zhang, Hig
unbalanced loa
State Universit
R. Cárdenasa,
control system
Electric Power
T. Friedli, J.
evaluation of t
back-to-back
Electronics, Vo
ng, Technology
r.com
Fig. 23.
. 24. Repetitive
put current multip
VI. C
introduced th
four-leg matri
ted and simu
selected to reg
width for
The simulat
anced, unbal
f the propos
oller showed t
cellent way.
REFE
J. C. Clare, P.
“Control Design
upply using ge
pecialists Confere
F. Blaabjerg, P
he matrix conve
ecialist Conferenc
une 17-21, 2001
G. Serra, A. Tani,
of induction mac
ol. 48, No. 6, pp.
Wheeler, N. Mas
modulation for a
onference, PESC 2
gh performance p
ad/source, PhD T
ty, 1998
R. Penab, J. Clar
m for four-leg mat
r Systems Researc
W. Kolar, J. Ro
three-phase AC–A
converter system
ol. 59, No. 12, pp
y & Applied Sci
Output current
e controller outpu
plied by factor 50
CONCLUSION
he design of
ix converter, c
ulated in Sim
gulate the out
high-freque
tion results
lanced, nonlin
sed modulati
the ability to
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D-Space Vector M
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Indirect 3D-Space Vector Modulation for a Matrix Converter

  • 1. Engineering, Technology & Applied Science Research Vol. 8, No. 2, 2018, 2847-2852 2847 www.etasr.com Abdelrehim et al.: Indirect 3D-Space Vector Modulation for a Matrix Converter Indirect 3D-Space Vector Modulation for a Matrix Converter Ahmed Abdelrehim Department of Electrical Engineering Alexandria University Alexandria, Egypt ahmed.abdelrehim@siemens.com Mohamed El-Habrouk Department of Electrical Engineering Alexandria University Alexandria, Egypt eepgmme1@yahoo.com Samir Deghedie Erfan Department of Electrical Engineering Alexandria University Alexandria, Egypt deghedie@gmail.com Karim Hassan Youssef Department of Electrical Engineering Alexandria University Alexandria, Egypt khmyoussef@yahoo.com Abstract—This paper discusses the indirect space vector modulation for a four-leg matrix converter. The four-leg matrix converter has been proven to be a reliable, cost-effective, and compact power electronic interface to supply unbalanced or nonlinear loads. However, the added fourth leg has shifted the inverter side modulation from simple two-dimension SVM into complex three-dimension. This paper employs a new technique to implement indirect 3D SVM in digital controllers with further simplification in the modulation process. Moreover, Simulink simulation using repetitive controller has been performed to regulate the output voltage for 400 Hz Power supplies. Keywords-repetitive controller; 3D SVM; four-leg matrix converter I. INTRODUCTION The matrix converter is a static and direct AC to AC converter with unique features of unity input power factor, high power to volume ratio, high reliability and MTBF factor which has gained interest in applications aiming to produce a realization of a compact three-phase drive for military, industrial and aerospace systems [1-3]. Moreover, researchers utilized the matrix converter as an electronic interface layer between all resources (wind, solar, storage, etc.) of the energy matrix model and as an electronic transformer competing with the traditional magnetic transformer. The added fourth leg is placed to provide a return path for the zero-sequence current during unbalancing and add the capability of supplying different connected single-phase loads. Four-leg converters have a superior ability to produce balanced output voltage waveform even under severely unbalanced load or non-linear load conditions [4]. A four-leg matrix converter topology is shown in Figure 1. This paper investigates the indirect space vector modulation which decouples the modulation into two stages (rectifier + inverter) without intermediate energy storage. This decoupling is efficient and allows separate control to each stage, while as there is no intermediate energy storage, a proper synchronization between the two stages is mandatory to fulfill the power balance equation as instantaneous input power shall be equal to the instantaneous output power for the load [5]. At high-frequency applications with precise control requirements as for naval and aerospace applications where the 115V-400Hz system is commonly used, traditional controllers have failed to achieve a proper regulation, due to the limited bandwidth so the repetitive controller is introduced as an optimum solution for this control problem [6]. II. MATRIX CONVERTER MODEL Matrix converter can be represented mathematically by matrix M and switches are identified as , where X is the output phase, Y is the input phase and S is the linking switch between input and output. Rectifier switches are numbered from to while inverter side switches are numbered from to . The rectifier is represented in Figure 1. Governing equations are: Vout=M*Vin (1) Iout=MT *Iin (2) Vout=Mi*VDC (3) VDC=MR*Vin (4) Vout=Mi*MR*Vin (5) where , , , , , , , and are output voltage, input voltage, output current, input current, DC intermediate voltage, inverter side switching matrix, rectifier side switching matrix, matrix converter switching matrix and transposed matrix converter switching matrix respectively. and Mi are described by (6) and (7) respectively: = 1 3 5 2 4 6 (6)
  • 2. spl rec ach out ass A. con con rec Engineerin www.etasr Fig. 1. M = S7 S8 S9 S1 S11 S1 S13 S1 M equals to M M = S7 S8 S9 S10 S11 S12 S13 S14 Equation (8) = S1 ∗ S7 S2 S1 ∗ S9 S2 S1 ∗ S11 S2 S1 ∗ S13 S2 = SaA SaB SbA SbB ScA ScB SnA SnB In Figure 1 v The mathema Fig. 2. III. INDIREC Indirect spac litting the mo ctifying stage hieve decoupl tput voltage sumption of vi Rectifying St The main fu ntrol on the d ntrol the amp ctifying stage, ng, Technology r.com Schematic of a f 8 10 12 14 Mi*MR: 8 0 2 4 * S1 S3 S5 S2 S4 S6 can be further ∗ S8 S3 ∗ S7 ∗ S10 S3 ∗ S9 ∗ S12 S3 ∗ S11 ∗ S14 S3 ∗ S13 SaC SbC ScC SnC voltages are: V atical modelin Mathematical CT SPACE VECT ce vector mod odulation into and the seco ling between t control.as per irtual DC link tage unction of the displacement a plitude of the , only two sw y & Applied Sci four-leg direct ma 5 6 r synthesized i 7 S4 ∗ S8 S S4 ∗ S10 S 1 S4 ∗ S12 S5 3 S3 ∗ S14 S5 = V V V V and V ng is summariz modeling of matr TOR MODULAT dulation can b o two stages, ond is called the input curr r (5) and (9) as shown in F e rectifying sta angle of the in virtual DC l witches must b ience Research A atrix converter (7) (8) into S5 ∗ S7 S6 ∗ S8 5 ∗ S9 S6 ∗ S10 5 ∗ S11 S6 ∗ S1 5 ∗ S13 S6 ∗ S1 (9) V = V V V . zed in Figure 2 rix converter TION be implement the first is inversion sta rent control an and based o Figure 1. age is to achi nput current a link voltage. I be closed at a h V Abdelrehim et a 8 0 12 14 2. ted by called ge, to nd the on the ieve a and to In the time, just sim num com wil B. abc ang con sim ther com mo the ind is n wil Fig vec sele the the rect mat The be Vol. 8, No. 2, 20 al.: Indirect 3D t one upper s multaneously to mbered from o mbinations are l occur as show Fig. 3. Ni Rectifier Spac SVM for the c to αβ coord gle by which w nverter modul mulation that sw re is no nee mmonly hap dulations as sh Fig In Figure 4, θ actual hexa dex=Iref/IDC , 0 no need to syn l be switched gure 5. Modula ctor during t ections have b number of th range of on tifying stage trix converter e displacemen zero. To impl 018, 2847-2852 D-Space Vector M switch and on o avoid short c one to six as sh e only allowed wn in Figure 3 ine switching com ce Vector Mod rectifying sta dination and c we can define lation requirem witching one v ed to synthes ppens with hown in Figur g. 4. Synthesi θc is the angle agon sector, 0<mc<1. For nthesize the re d during ever ation process the time inte been translated he current sec ne to six. To and one of t is to have uni nt angle betwee lement this, th 2 Modulation for ne lower swi circuit. The re hown in Figure to guarantee t 3. mbinations for the dulation age works by calculating th e the working ment, it has vector per sect size two vect conventional re 4. is of reference cu e of the refere mc the cu matrix conver ference vector ry sector dura happens by as erval of eve d into a train ctor, numbers o achieve the the most inter ity power facto en input curren he reference s 2848 r a Matrix Con itch can be c ectifier switche e 1. Nine switc that no short c e rectifying stage transforming he reference v sector. For m been approve tor is sufficien tors per secto l rectifier urrent ence current w urrent modul rter, mc=1 and r as just one v ation as show ssigning one a ry sector. V of pulses car are represent e second targ resting featur or at the input nt and voltage signal given t verter closed es are ching circuit input vector matrix ed by nt and or as SVM within lation there vector wn in active Vector rrying ted in get of res of t side. shall to the
  • 3. mo ins mo con app fun out add the thr app unb app neu rol leg coo inv the inv com by tur (ne coo con be ana Pri vec A. Engineerin www.etasr odulation proc stead of the inp Fig. 5. Inversion st odulation, and nverter, we w proach for th nction of inve tput voltage ded fourth leg e zero-sequenc ree-phase syste + + And the tra plied as it ha balanced syst plied. Due to utral current p le of 3D SVM gs. + + Transformati ordination du version stage, e same time in verter with mbinations ar p or n for ea rned on (posi egative). If th ordination, th nventional SV divided into alog to secto ism number m ctor angle on α Prism Identif If 0<θ<60 60<θ<12 120<θ<1 180<θ<24 ng, Technology r.com cess has been put phase curr . Rectifying s III. INV tage is conce d as this pa will address he four-leg ersion stage i under balanc g is responsibl ce component em follows (10 =0 ansformation f as happened tem (10) is n the unbalanc passing throug M to provide ≠ 0 ion to statio ue to the zer switches on th n order to avo eight switc re sixteen. Sw ach leg, where tive) and n in he sixteen-ve he result is VM are turned six prisms (F ors representat may be ident αβγ coordinati fication the 0 the 80 the 40 the y & Applied Sci taken from i rent. stage SVM vector VERSION STAGE erned with in aper discusse the 3D SVM matrix conve is to provide ced and unba e for providin t during unbal 0). from abc to with the rect no longer vali cing of the sy gh the system accurate swit onary frame ro-sequence c he same leg ca oid short circu ches, the p itching combi e p indicates ndicates the l ectors are rep a 3D hexago into prisms. T Figures 6-7). tion on conv tified by defi ion. en P=1 en P=2 en P=3 en P=4 ience Research A input phase v rs selection E nverter side es four-leg m M as a modu erter. The pr a control ove alanced loads ng a current pa lance. The bal (10 αβ coordinati tifier stage. F id and (11) is ystem, there w m and it is the tching pulses (11 happens into component. I an’t be turned uit. For the fo possible swit inations repres the upper swi lower switch presented into on and secto The 3D hexago The prisms a entional 2D ining the refe h V Abdelrehim et a oltage SVM matrix ulation rimary er the . The ath for lanced 0) ion is For an s now will be basic to all ) o αβγ In the d on at our-leg tching sented itch is is on o αβα ors of on can are an SVM. erence 8. E B. and imp bes thre swi Vol. 8, No. 2, 20 al.: Indirect 3D 240<θ<30 300<θ<36 Vectors are d Each prism con Fig. 6. 3D re Fig. Fig. Switching Vec As the referen d tetrahedron plemented by side each tetr ee switching v itching vector 018, 2847-2852 D-Space Vector M 00 then 60 then distributed into ntains four act epresentation of sw 7. Prisms ide 8. Vector dist ctor Selection nce vector loca number, sel choosing the n rahedron[8, 9] vectors, to ca the reference 2 Modulation for n P=5 n P=6, where θ o each prism a tive vectors. witching vectors i entification for 3D tribution into each ation is define ection of sw nearest referen ]. Each tetrah alculate the du e required volt 2849 r a Matrix Con θ= tan as shown in F in αβγ coordinatio D SVM h prism ed by prism nu witching vecto nce vectors lo hedron consis uty cycle for tage is transfo verter Figure on umber ors is ocated sts of each ormed
  • 4. firs sw wh the and ma var tetr po SV the nu act (re cha rep rep tw ma val var suc var Th op sho 10 Engineerin www.etasr st to αβγ coor witching vector V V V = d The duty cyc d d d = ∗ S = 1 here S is the d e reference vec d d represents atrix is depend rying values rahedron. S m ssible coincid VM code check e current value The rectifyin mbers from 1 tive rectifier ectifier matrix arge of genera presenting the presented on o matrices as i atrix converter Fig. 9. M A Simulink lidate the effe rying types o ccessfully va rious scenario he input and eration. The s own in Table -26. ng, Technology r.com rdination and rs [9] as per (1 d d V V V cles can be furt ∗ V V V duty cycle mat ctor, (V1 V2 V3 s the duty cy dent on the sel depending matrix calcula ence between ks the prism a es of S. IV. MATR ng stage is de 1 to 6, these n switches and x). At the sam ating another current active (inverter in (5) allows u r. The procedu Matrix converter V. SIMUL k simulation ectiveness of m f loads. The alidated as w os such as bala output wavef simulation was I. The simula y & Applied Sci then is divid 2). ther calculated trix [8-10], (V 3)T is the curren ycle for each s lected switchin on each se ations have b prisms and te and tetrahedron RIX CONVERTE edicated to gen numbers repre d would be re me time the in series of num e inverter swit matrix) as we us to find all p ure is shown in code generation f LINK SIMULATI was successf matrix conver proposed indi well. Simulati anced and unb forms ensured s carried out u ation results ar ience Research A ed by the ava (12 d as shown in (13 (14 Vα-ref Vβ-ref Vδ-r nt switching v switching vec ng vectors, so elected prism been done for etrahedrons. Th n number to e ER nerating a ser esenting the c epresented on nversion stage mbers from 1 tches that wou ell. Multiplyin possible switch n Figure 9. from Mi and MR ION fully develop rter operation irect 3D SVM ion worked balanced linear d proper con using the param re shown in F h V Abdelrehim et a ailable 2) (13). 3) 4) ref)T is vector, ctor. S it has m and r each he 3D extract ries of current n e is in to 16, uld be ng the hes for ed to under M was under r load. nverter meters igures R A. Vol. 8, No. 2, 20 al.: Indirect 3D Source sys Load syst Switching freq Input filter Output filter Repetitive Contr Tracking con Unbalanced Balanced l Nonlinear l Non-Linear L Fig. 12. FF 018, 2847-2852 D-Space Vector M TABLE I. tem em quency (LC) r (LC) roller Q(z) ntroller d load 5Ω load load Load Fig. 10. O (a) P (b) P (c) P (d) N Fig. 11. O FT analysis for ou 2 Modulation for SYSTEM PARAM 440V 115V- 1280 56Ω/0.8m 180uH+70 1.72377 1.663 1.868 Ω+5.5mH, 10Ω+6 5Ω +5 3phase diode Output voltage Phase A Phase B Phase C Neutral Output current utput phase voltag 2850 r a Matrix Con METERS V-60Hz -400Hz 00Hz mH/10uF 0uH/100uF 2 1 76 0.75754 3 0.9914 8 0.8735 6.2mH, 20Ω+7.5m 5.5 mH e bridge +50Ω ge (THD=3.3%) verter mH
  • 5. B. Engineerin www.etasr Fig. 13. Unbalanced Fig. 17. Inp ng, Technology r.com FFT analysis fo Fig. 14. Load Fig. 15. (a) P (b) P (c) P (d) Fig. 16. O put current multip y & Applied Sci or output current Error signal Output voltage Phase A Phase B Phase C Neutral Output Currents plied by factor 50 ience Research A (THD=1.8%) and input voltage h V Abdelrehim et a e C. Vol. 8, No. 2, 20 al.: Indirect 3D Fig. 19. Fig. 20. FF Non Linear L F Fig. 22. 018, 2847-2852 D-Space Vector M Fig. 18. FFT analysis fo FT analysis for ou Load Fig. 21. Output FFT analysis fo 2 Modulation for Error signal or input current (T utput phase voltag t voltage 115V/40 or input current (T 2851 r a Matrix Con THD=48%) ge (THD=3.3%) 00H THD=48%) verter
  • 6. mo bee con lim (11 con eff rep vo [1] [2] [3] [4] [5] [6] [7] Engineerin www.etasr Fig Fig. 25. Inp This paper odulation for en implement ntroller was s mited bandw 15V/400Hz). nditions (bal fectiveness o petitive contro ltage in an exc P. Zanchetta, Empringham, “ AC power s Electronics Sp 16, 2005 C. Klumpner, process of th Electronics Sp 1083–1088, Ju D. Casadei, G torque control Electronics, Vo F. Yue, P. W. W space vector m Electronics Co R. Zhang, Hig unbalanced loa State Universit R. Cárdenasa, control system Electric Power T. Friedli, J. evaluation of t back-to-back Electronics, Vo ng, Technology r.com Fig. 23. . 24. Repetitive put current multip VI. C introduced th four-leg matri ted and simu selected to reg width for The simulat anced, unbal f the propos oller showed t cellent way. REFE J. C. Clare, P. “Control Design upply using ge pecialists Confere F. Blaabjerg, P he matrix conve ecialist Conferenc une 17-21, 2001 G. Serra, A. Tani, of induction mac ol. 48, No. 6, pp. Wheeler, N. Mas modulation for a onference, PESC 2 gh performance p ad/source, PhD T ty, 1998 R. Penab, J. Clar m for four-leg mat r Systems Researc W. Kolar, J. Ro three-phase AC–A converter system ol. 59, No. 12, pp y & Applied Sci Output current e controller outpu plied by factor 50 CONCLUSION he design of ix converter, c ulated in Sim gulate the out high-freque tion results lanced, nonlin sed modulati the ability to ERENCES W. Wheeler, D of a three-phase enetic algorithms ence, Recife, Braz P. Nielsen, “Spee erter technology ce PESC, Vancou “The use of ma chines”, IEEE Tr 1057–1064, 2001 on, L. Empringha a 4-leg matrix c 2007, Orlando, U ower converter s Thesis, Virginia P e, P. Wheeler, P. trix converters fe ch, Vol. 104, pp. odriguez, P. W. AC matrix conver ms”, IEEE Tran p. 4487–4510, 201 ience Research A ut signal and input voltage 3D SVM in code validatio mulink. 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