Inter
national
J
our
nal
of
Electrical
and
Computer
Engineering
(IJECE)
V
ol.
8,
No.
5,
October
2018,
pp.
3711
–
3721
ISSN:
2088-8708
3711
I
ns
t
it
u
t
e
o
f
A
d
v
a
nce
d
Eng
ine
e
r
i
ng
a
nd
S
cie
nce
w
w
w
.
i
a
e
s
j
o
u
r
n
a
l
.
c
o
m
PI
and
LQR
contr
ollers
f
or
Fr
equency
Regulation
including
W
ind
Generation
Semaria
Ruiz
1
,
J
ulian
P
ati
˜
no
2,3
,
and
J
air
o
Espinosa
1
1
Departmento
de
Ingenier
´
ıa
El
´
ectrica
y
Autom
´
atica,
F
acultad
de
Minas,
Uni
v
ersidad
Nacional
de
Colombia,
Medell
´
ın,
Colombia
2
Departmento
de
Ingenier
´
ıa
El
´
ectrica,
F
acultad
de
Ingenier
´
ıa
y
Arquitectura,
Uni
v
ersidad
Nacional
de
Colombia,
Manizales,
Colombia
3
Instituci
´
on
Uni
v
ersitaria
P
ascual
Bra
v
o,
Medell
´
ın,
Colombia
Article
Inf
o
Article
history:
Recei
v
ed
February
21,
2018
Re
vised
May
26,
2018
Accepted
June
21,
2018
K
eyw
ord:
W
ind
T
urbines
Load
Frequenc
y
Control
Linear
Quadratic
Re
gulator
Proportional
Inte
gral
control
Po
wer
Systems
ABSTRA
CT
The
increasing
use
of
rene
w
able
technologies
such
as
wind
turbines
in
po
wer
systems
may
require
the
contrib
ution
of
these
ne
w
sources
into
grid
ancilla
ry
services,
such
as
Load
Frequenc
y
Control.
Hence,
this
w
ork
dealt
with
the
performance
compar
-
ison
of
tw
o
traditional
control
structures,
PI
and
LQR,
for
secondary
re
gulation
of
Load
Frequenc
y
Control
with
the
participation
of
v
ariable-speed
wind
turbines.
F
or
this
purpose,
the
doubly-fed
induction
generator
wind
turbine
w
as
modeled
with
addi-
tional
control
loops
for
emulation
of
the
inertial
response
of
con
v
entional
machines
for
frequenc
y
re
gulation
tasks.
Performance
of
proposed
strate
gies
w
as
v
erified
through
simulation
in
a
benchmark
adapted
from
the
WSCC
3
machines
9-b
us
test
system.
Results
s
ho
wed
o
v
erall
superior
performance
for
LQR
controller
,
although
requiring
more
strenuous
control
ef
fort
from
con
v
entional
units
than
PI
control.
Copyright
c
2018
Institute
of
Advanced
Engineering
and
Science
.
All
rights
r
eserved.
Corresponding
A
uthor:
Semaria
Ruiz
Departmento
de
Ingenier
´
ıa
El
´
ectrica
y
Autom
´
atica,
F
acultad
de
Minas,
Uni
v
ersidad
Nacional
de
Colombia,
Medell
´
ın,
Colombia
Carrera
80
No
65-223
Medell
´
ın,
Colombia
+57
4
4255092
seruizal@unal.edu.co
1.
INTR
ODUCTION
Electricity
production
from
rene
w
able
ener
gy
sources
(RES)
has
been
continually
gro
wing.
This
de
v
elopment
is
taking
place
in
a
po
wer
system
s
tructure
designed
for
con
v
entional
po
wer
sources,
with
char
-
acteristics
such
as
a
v
ailability
,
controllability
,
and
reliability
utterly
dif
ferent
to
those
of
RES
systems
[1][2].
Also,
the
ener
getic
production
of
RES
may
fluctuate
significantly
o
v
er
time
due
to
some
characteristics
of
natural
resources,
such
as
unpredictability
,
v
ariability
,
and
dependenc
y
on
the
geographic
location
[3]
[4].
In
particular
,
some
issues
attracting
a
lot
of
interest
in
the
technical
community
are
the
acti
v
e
po
wer
v
ariations
and
frequenc
y
performance
in
presence
of
RES
[1][3]
[5],
for
systems
including
solar
photo
v
oltaic
(PV)
panels
[6]
and
mostly
for
wind
turbines
(WT)
[7].
In
po
wer
systems,
frequenc
y
constitutes
a
parameter
indicating
the
equilibrium
between
po
wer
de-
manded
by
load
and
the
ener
gy
produced
by
generation
systems
[8].
When
this
relationship
is
unbalanced,
control
structures
are
in
place
to
return
system
frequenc
y
to
the
right
operat
ional
v
alues.
Ho
we
v
er
,
these
frequenc
y
control
strate
gies
ha
v
e
been
de
v
eloped
for
a
po
wer
system
with
almost
complete
reliance
on
con
v
en-
tional
ener
gy
sources,
and
the
penetration
of
RES
may
require
the
participation
of
these
ne
w
units
in
the
control
tasks
[3].
W
ind
t
urbines,
particularly
those
of
v
ariable-speed
with
doubly-fed
induction
(DFIG),
constit
ute
one
of
the
most
used
RES
around
the
w
orld
[9]
[10].
Hence,
se
v
eral
studies
ha
v
e
been
proposed
about
control
strate
gies
for
the
acti
v
e
inclusion
of
DFIG
WT
in
Load
Frequenc
y
Control
loops,
and
complete
re
vie
ws
can
be
found
in
references
[7]
[11]
[12].
J
ournal
Homepage:
http://iaescor
e
.com/journals/inde
x.php/IJECE
I
ns
t
it
u
t
e
o
f
A
d
v
a
nce
d
Eng
ine
e
r
i
ng
a
nd
S
cie
nce
w
w
w
.
i
a
e
s
j
o
u
r
n
a
l
.
c
o
m
,
DOI:
10.11591/ijece.v8i5.pp3711-3721
Evaluation Warning : The document was created with Spire.PDF for Python.
3712
ISSN:
2088-8708
+
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+
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Wind Turb
ine
Model
Figure
1.
LF
C
scheme
for
a
multi-area
(
N
areas)
po
wer
system,
including
primary
and
secondary
control
loops
[1].
The
block
”W
ind
T
urbine
Model”
inte
grates
WT
to
LFC.
One
of
the
most
used
strate
gies
for
DFIG
contrib
ution
in
frequenc
y
re
gulation,
is
the
so-called
syn-
thetic
inertia
method,
as
e
xplained
in
the
studies
[13]
and
[14].
In
this
technique,
additional
control
loops
are
de
v
eloped
for
the
WT
with
the
goal
of
emulating
frequenc
y
response
of
con
v
entional
generators.
This
alter
-
nati
v
e
w
as
e
xplored
in
other
w
orks
where
controllers
based
on
the
dynamic
representat
ions
of
the
DFIG
WT
were
proposed.
In
[15]
a
Linear
Quadratic
Re
gulator
type
of
controller
is
designed
for
the
WT
,
taking
as
model
inputs
the
reference
torque
and
the
reference
pitch
angle
of
the
turbine.
The
w
ork
of
Mohamed
et
al.
[16]
proposes
a
Model
Predicti
v
e
Controller
for
WT
inte
gration
to
frequenc
y
re
gulation,
using
a
simplified
model
of
the
DFIG
with
the
quadrature-axis
rotor
v
oltage
as
the
model
input.
Ho
we
v
er
,
these
studies
are
not
e
xploring
WT
penetration
in
a
multi-area
scenario
for
po
wer
systems,
an
increasingly
common
operational
possibility
as
grid
gro
ws
in
size
and
RES
inte
gration
le
v
el
arises.
Also,
a
performance
comparison
of
some
of
the
proposed
strate
gies
o
v
er
the
same
scenario
w
ould
be
useful
to
establish
the
most
suitable
control
structure
for
WT
con-
trib
ution
in
frequenc
y
re
gulation
tasks.
This
paper
addresses
both
of
the
formerly
mentioned
issues,
comparing
the
performance
of
PI-based
and
LQR-based
controllers
for
DFIG
WT
inte
gration
into
Load
Frequenc
y
Re
gu-
lation
(LFC)
structure
for
a
multi-area
po
wer
system.
The
simulation
is
performed
in
a
modified
v
ersion
of
the
9-b
us
WSCC
po
wer
system
[8].
This
w
ork
is
the
continuation
of
the
research
with
preliminary
results
reported
in
[17].
The
former
paper
focused
on
the
utilization
of
the
synthetic
inertia
model
for
WT
inte
gration
into
LFC
of
po
wer
systems
with
PI
controllers.
Our
current
article
presents
a
more
elaborated
description
of
the
non-linear
state-space
realization
emplo
yed
for
the
modeling
of
v
ariable
speed
wind
turbines.
Moreo
v
er
,
DFIG
wind
turbine
operation
includes
a
pitch-angle
control
loop.
Also,
additional
control
structures
are
e
xplored
with
the
consideration
of
LQR
controllers
for
secondary
re
gulation,
and
a
performance
comparison
discussion
v
ersus
PI
strate
gies.
Current
paper
is
di
vided
as
foll
o
ws:
Section
2.
describes
the
LFC
structure
for
po
wer
systems.
Section
3.
deals
with
the
WT
modeling
and
the
formulation
of
PI
and
LQR
controllers.
Simulation
tests
and
performance
comparisons
appear
in
Section
4..
At
last,
some
conclusions
are
presented
in
Section
5..
2.
LO
AD
FREQ
UENCY
CONTR
OL
IN
MUL
TI-AREA
PO
WER
SYSTEMS
Frequenc
y
re
gulation
can
be
classified
in
three
main
stages
according
to
the
nature
and
timing
of
the
control
ef
forts:
primary
actions
proportional
to
the
frequenc
y
de
viations,
secondary
actions
allo
wing
correction
of
steady-state
errors,
and
tertiary
actions
related
with
predefined
dispatches
and
some
emer
genc
y
conditions.
These
three
stages
constitute
the
Load
Frequenc
y
Control
(LFC)
system
[8,
1].
Grid
eleme
nts
must
be
modeled
for
the
design
of
LFC
controllers.
First
order
models
are
assumed
for
the
go
v
ernor
and
turbine
of
con
v
entional
units,
and
for
the
representation
of
the
frequenc
y
response
char
-
IJECE
V
ol.
8,
No.
5,
October
2018:
3711
–
3721
Evaluation Warning : The document was created with Spire.PDF for Python.
IJECE
ISSN:
2088-8708
3713
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P
i
t
c
h
a
ngl
e
c
o
nt
r
o
l
l
er
s
LF
C
LF
C
pr
i
ma
r
y
l
o
o
p
LF
C
s
ec
o
nda
r
y
l
o
o
p
R
o
t
o
r
s
peed
vs
t
o
r
que
c
ur
v
es
Figure
2.
W
ind
turbine
model
with
frequenc
y
response
and
v
ariable
wind
speed
(based
on
[19]).
acteristic
of
an
y
control
area
in
the
po
wer
system.
Figure
1
sho
ws
the
LFC
for
a
N
-area
po
wer
system,
where
parameters
for
the
i
-th
area
are:
P
mk
i
the
change
in
mechanical
po
wer
of
the
generator
k
,
P
g
k
i
the
change
in
the
acti
v
e
po
wer
output
of
generator
k
,
P
L
the
load
perturbation,
f
i
the
frequenc
y
change,
D
i
the
damp-
ing
coef
ficient.
H
i
the
equi
v
alent
inertia,
P
ck
i
the
control
action
of
the
LFC
for
the
k
-th
generator
,
T
ij
the
po
wer
e
xchange
coef
ficient
between
area
i
and
area
j
,
P
tiei
the
total
change
in
the
po
wer
e
xchanged
between
area
i
and
other
areas
and
f
j
the
change
in
the
frequenc
y
of
area
j
connected
to
area
i
.
Also,
B
i
denotes
the
bias
f
actor
for
modulation
of
the
error
signal
in
secondary
re
gulation,
K
i
(
s
)
is
the
transfer
function
of
the
secondary
controller
and
i
the
participation
f
actor
of
each
generator
in
secondary
control.
3.
INCLUSION
OF
V
ARIABLE
SPEED
WT
IN
LFC
This
w
ork
only
considered
v
ariable-speed
DFIG
WT
,
as
the
y
are
the
best-suit
ed
WT
f
or
acti
v
e
part
ici-
pation
in
grid
ancillary
services
[18].
Ho
we
v
er
,
WT
units
with
DFIG
do
not
present
a
natural
inertial
response
to
frequenc
y
changes
[1].
F
or
enabling
frequenc
y
response
capabilities
to
the
DFIG
WT
,
synthetic
inertia
control
strate
gy
[14]
w
as
emplo
yed.
This
technique
proposes
operation
of
the
DFIG
WT
belo
w
the
point
of
maximum
po
wer
e
xtraction
to
maintain
a
reserv
e
of
kinetic
ener
gy
to
be
used
for
frequenc
y
compensat
ion.
The
operating
point
P
o
depends
on
the
DFIG
angular
speed
w
r
and
the
so-called
operational
torque
T
o
[
N
m
]
,
calculated
as
indicated
in
equation
1
for
dif
ferent
v
alues
of
wind
speed
v
.
Gain
K
op
is
adjusted
for
the
operation
of
the
WT
under
the
curv
e
formed
by
the
points
of
maximum
withdra
w
able
po
wer
from
wind
at
each
speed.
T
op
=
K
op
v
2
:
(1)
F
or
the
electromagnetic
component
of
the
DFIG,
the
simplified
model
proposed
in
[13]
[19]
is
used
and
included
in
the
LFC
as
the
wind-turbine
model
block
in
Figure
1.
This
representation,
denominated
as
synthetic-inertia
model
,
is
a
reduced
induction-machine
model
of
fourth
order
and
only
uses
the
quantities
in
q
-axis,
as
the
d
-axis
is
selected
as
the
reference
frame.
Figure
2
presents
both
models.
In
the
scheme
of
Figure
2,
P
base
is
the
nominal
po
wer
of
t
he
area,
w
r
is
the
angular
speed
of
rotor
,
n
is
the
quantity
of
WTs,
v
q
r
is
the
rotor
quadrature
v
oltage,
i
q
r
is
the
rotor
quadrature
current,
iq
r
;r
is
the
reference
quadrature
current
for
rotor
,
P
I
v
q
r
is
the
PI
controller
for
v
q
r
,
T
e
is
the
electromagnetic
torque,
T
m
is
the
mechanical
torque,
is
the
bla
d
e
pitch
angle,
r
is
the
blade
pitch
angle
reference,
denotes
the
time
delay
of
pitch
angle
actuator
,
w
r
;r
is
the
rotor
angular
speed
reference,
P
I
v
q
r
is
the
PI
controller
for
w
r
,
v
r
is
the
rated
wind
speed
of
WT
,
K
1
is
the
proportional
action
of
primary
control,
K
2
is
the
proportional
action
of
secondary
control,
K
w
and
T
w
are
the
g
ain
and
time
delay
of
secondary
control
loop,
J
is
the
inertia
moment
of
WT
,
and
X
1
X
2
,
X
3
,
and
T
1
are
approximately
constant
v
alues
representing
some
combinations
among
DFIG
internal
generator
parameters
(see
[13]
and
[20]
for
detailed
e
xplanation).
As
seen
from
Figure
2,
se
v
eral
control
loops
are
added
to
the
simplified
turbine
model
to
emulate
the
beha
vior
of
the
dif
ferent
control
stages
of
the
LFC
struct
ure
and
to
k
eep
the
stable
operation
of
the
DFIG
WT
after
contrib
ution
to
frequenc
y
re
gulation.
These
loops
are
described
as
follo
ws:
1.
A
primary
response
loop
for
the
DFIG
labeled
as
LFC
primary
loop
in
Figure
2.
Proportional
g
ain
K
1
is
PI
and
LQR
contr
oller
s
for
F
r
equency
Re
gulation
including
W
ind
Gener
ation
(Semaria
Ruiz)
Evaluation Warning : The document was created with Spire.PDF for Python.
3714
ISSN:
2088-8708
modulating
the
frequenc
y
change
rate
d!
dt
.
2.
A
secondary
response
loop
mark
ed
as
LFC
secondary
loop
in
Figure
2
operating
in
the
same
w
ay
as
t
he
secondary
control
of
LFC.
The
po
wer
deli
v
ered
by
WT
is
restored
to
the
nominal
operating
point
after
a
control
of
frequenc
y
disturbances.
3.
The
pitc
h-angle
contr
oller
loop
in
Figure
2,
task
ed
with
maintaini
ng
the
angular
speed
of
the
WT
at
nominal
operating
v
alue
for
wind
speeds
equal
or
o
v
er
the
rated
ones.
Under
the
action
of
pitch
control,
in
case
of
a
frequenc
y
disturbance
occurring,
an
additional
control
loop
is
required
for
modulating
pitch
angle
with
a
g
ain
R
proportional
to
frequenc
y
de
viation.
The
area
de
viation
frequenc
y
signal
is
filtered
(through
a
filter
with
g
ain
K
a
and
time
delay
T
a
,
see
Figure
2)
before
being
applied
to
primary
and
secondary
control
loops.
This
w
ork
performs
a
comparison
of
the
mentioned
loops
for
tw
o
dif
ferent
secondary
controllers
in
frequenc
y
re
gulation.
The
follo
wing
subsections
describe
the
PI
and
LQR
secondary
controllers
(see
K
i
(
s
)
block
i
n
Figure
1)
and
their
interaction
with
the
WT
control
scheme.
3.1.
Considerations
f
or
system
with
secondary
PI
contr
oller
Proportional
Inte
gral
(PI)
control
constitutes
the
most
used
v
ariation
of
the
Proportional
Inte
gral
Deri
v
ati
v
e
(PID)
structure
[21].
Starting
from
a
simple
Single-Input
Single-Output
(SISO)
loop
[21],
the
trans-
fer
function
C
P
I
(
s
)
of
the
PI
controller
is
C
P
I
(
s
)
=
K
p
(1
+
(
T
r
s
)
(
1)
.
The
term
K
p
is
the
Proportional
g
ain,
T
r
is
kno
wn
as
the
reset
time
[21],
and
the
relationship
K
p
(
T
r
)
(
1)
is
called
the
inte
gral
g
ain.
PI
controllers
constitute
the
traditional
strate
gy
for
secondary
re
gulation
in
LFC
system.
In
this
w
ork,
additional
PI
controllers
re
gulate
quadrature
rotor
current
(
P
I
i
q
r
)
and
the
pitch
angle
(
P
I
w
r
),
as
sho
wn
in
Figure
2.
3.2.
Considerations
f
or
LFC
system
with
secondary
LQR
contr
oller
Criterion-based
synthesis
of
controllers
is
a
design
technique
dri
v
en
by
the
comple
xity
of
multi-
v
ariable
systems.
A
commonly
emplo
yed
set
of
criteria
is
formed
by
cost
functions
related
to
quadratic
forms
of
control
ef
fort
and
error
signals
[21].
F
or
linear
case,
the
so-called
Linear
Quadratic
Re
gulator
e
xpresses
the
problem
as
the
feasible
solving
of
the
dynamic
Riccati
equation
in
continuous
time,
leading
to
a
time-v
ariable
state
feedback
[21].
F
or
this
configuration,
secondary
controller
K
i
(
s
)
requires
a
state-space
representation
of
the
whole
LFC.
Equations
(2)
to
(11)
describe
the
complete
non-linear
state-space
model
for
a
multi-area
po
wer
system
with
inte
gration
of
WT
to
the
LFC
scheme,
adapted
from
[16].
This
representation
includes
the
transferred
po
wer
between
areas
P
tie
as
a
state,
with
an
additional
state
equation
for
WT
pitch-angle
(see
eq.
(8))
as
a
parameter
with
high
influence
in
the
contrib
ution
of
WT
to
LFC
[15].
_
f
=
P
m
D
f
P
L
2
H
P
tie
2
+
X
3
w
r
iq
r
n
P
r
ef
P
base
f
2
H
(2)
_
P
tie
=
2
N
X
j
=1
T
i;j
f
+
P
c
T
g
2
v
i
(3)
_
P
m
=
P
m
T
P
g
T
g
(4)
_
P
g
=
f
R
T
g
P
g
T
g
+
P
c
T
g
(5)
_
i
q
r
=
i
q
r
T
1
+
v
q
r
T
1
(6)
_
w
r
=
X
3
i
q
r
J
+
T
m
J
(7)
IJECE
V
ol.
8,
No.
5,
October
2018:
3711
–
3721
Evaluation Warning : The document was created with Spire.PDF for Python.
IJECE
ISSN:
2088-8708
3715
Gen2
Gen3
Gen1
1
2
3
4
5
6
7
8
9
Lo
a
d5
Lo
a
d6
Lo
a
d8
Ar
ea
I
Ar
ea
I
I
Ar
ea
I
I
I
Figure
3.
WSCC
9-b
us
system
multi-area
partitioning.
System
parameters
can
be
found
in
[8].
_
=
+
r
ef
+
R
f
(8)
Mechanical
torque
T
m
is
calculated
from
parameters
such
as
air
density
,
length
of
turbine
blades
and
WT
po
wer
coef
ficient
C
p
(fraction
of
a
v
ailable
wind
po
wer
being
e
xtracted).
Dif
ferences
with
[16]
in
v
olv
e
the
consideration
of
pitch
angle
reference
r
ef
as
an
input,
and
wind
speed
v
and
frequenc
y
de
viation
of
neighboring
areas
f
j
as
outputs.
Complete
v
ectors
of
system
inputs
U
and
disturbances
W
are
sho
wn
belo
w
,
with
P
L
the
de
viations
in
demanded-load:
Mechanical
torque
is
calculated
di
viding
equation
(9)
by
the
angular
rotor
speed:
P
m
=
1
2
R
2
v
3
C
p
:
(9)
where
represents
air
density
,
R
is
the
length
of
the
turbine
blades
and
the
po
wer
coef
ficient
C
p
denotes
the
fraction
of
a
v
ailable
po
wer
in
the
wind
that
is
being
harv
ested.
This
parameter
is
a
function
of
the
T
ip-Speed
Ratio
(TSR)
denoted
by
=
R
w
r
v
,
and
the
collecti
v
e
blade
pitch
.
U
T
=
v
q
r
P
c
r
ef
,
W
T
=
P
L
f
j
v
(10)
Finally
,
v
ector
Y
presents
system
outputs
in
equation
(11).
The
first
output
is
the
rotor
quadrature
current
i
q
r
,
whose
reference
is
gi
v
en
by
i
q
r
;r
.
The
second
output
is
the
system
Area
Control
Error
(A
CE),
reference
signal
for
the
LFC
secondary
controller
(
AC
E
=
f
+
P
tie
).
The
last
output
is
the
rotor
angular
speed,
whose
reference
is
defined
for
a
gi
v
en
mechanical
torque.
y
T
=
iq
r
f
+
P
tie
w
r
:
(11)
4.
RESUL
TS
4.1.
Description
of
case
of
study
A
slightly
modified
v
ersion
of
the
WSCC
9-b
us
po
wer
system
[8]
w
as
emplo
yed
for
simulation
of
the
DFIG
participation
in
the
LFC
for
a
multi-area
po
wer
.
The
modified
sys
tem
parameters
are
summarized
in
T
able
1.
This
system
w
as
partitioned
into
three
areas,
as
illustrated
in
Figure
3.
Consider
Generator
1
as
h
ydraulic
and
Generators
2
and
3
as
g
as
units.
F
or
the
sak
e
of
this
w
ork,
50%
of
con
v
entional
generation
in
Area
III
w
as
replaced
by
a
wind
f
arm.
The
wind
f
arm
w
as
formed
by
32
DFIG
WT
of
2
M
W
each,
whose
model
parameters
are
sho
wn
in
T
able
2.
W
ind
speed
w
as
simulated
from
a
normally
distrib
uted
random
signal
with
a
period
of
50
seconds,
mean
v
alue
of
12
:
5
m=s
and
v
ariance
of
2
:
8
m=s
.
Finally
,
load
disturbances
were
applied
as
follo
ws:
an
increment
of
0.06
[
p:u
]
at
30
seconds
of
operation
in
area
III;
a
v
ariation
of
magnitude
0.08
[
p:u
]
at
60
seconds
in
area
II;
and
another
disturbance
of
0.01
[
p:u
]
at
90
seconds
for
area
I.
The
Po
wer
Base
is
set
at
100
M
V
A
.
PI
and
LQR
contr
oller
s
for
F
r
equency
Re
gulation
including
W
ind
Gener
ation
(Semaria
Ruiz)
Evaluation Warning : The document was created with Spire.PDF for Python.
3716
ISSN:
2088-8708
T
able
1.
WSCC
9
b
us
system
parameters
[8].
P
arameter
V
alue
P
arameter
V
alue
P
arameter
V
alue
H
1
23.64
s
T
12
2.064
p.u.
R
1
2
p.u.
H
2
6.4
s
T
13
6.1191
p.u.
R
2
10
p.u.
H
3
1.505
s
T
23
14.4353
p.u.
R
3
7.5019
p.u.
M
V
A
nom
1
247.5
D
1
;
D
2
;
D
3
0.8
B
1
2.8
s
M
V
A
nom
2
192
T
g
1
;
T
g
2
;
T
g
3
0.2
B
2
10.8
s
M
V
A
nom
3
128
T
1
;
T
2
;
T
3
0.3
B
3
8.3
s
T
able
2.
W
ind-turbine
model
simulation
parameters
[14].
P
arameter
V
alue
P
arameter
V
alue
P
nom
2
M
W
R
s
0.00491
p.u.
V
nom
966
V
X
l
s
0.09273
p.u.
K
1
5000
N
m
X
m
3.96545
p.u.
K
2
2000
N
m
R
r
0.00552
p.u
T
w
1
X
l
r
0.1
p.u.
K
a
500
H
4.5
s
T
a
20
J
506.6059
K
g
m
2
.
4.2.
T
uning
of
PI
contr
ollers
PI
controllers
for
secondary
frequenc
y
re
gulation
in
each
area
were
tuned
using
the
Gradient
Descent
method,
along
with
P
I
controllers
of
rotor
angular
speed
w
r
and
rotor
quadrature
v
oltage
v
q
r
.
T
able
3
presents
the
parameters
for
all
of
them.
T
able
3.
P
arameter
v
alues
for
the
dif
ferent
PI
controllers
in
simulation
for
the
case
of
study
.
Contr
oller
Pr
oportional
Gain
k
P
Integral
Gain
k
I
PI
Area
I
0
-0.05
PI
Area
II
0
-0.05
PI
Area
III
0
-0.28
PI
v
q
r
0
2.70
PI
w
r
7.19
0.53
4.3.
T
uning
of
LQR
contr
oller
T
o
calculate
the
g
ains
of
LQR
controller
with
reference
tracking,
a
linearization
must
be
performed
in
the
non-linear
state-space
model
described
by
equations
(2)
to
(8).
This
process
results
in
the
operating
point
v
ectors
U
T
op
=
[27
:
97
0
:
08
9]
for
the
inputs
and
W
T
op
=
[0
:
2
0
12]
for
disturbance
signals.
Design
of
LQR
controllers
for
secondary
LFC
implies
the
tuning
of
the
positi
v
e
definite
matrices
Q
ar
ea
and
R
ar
ea
for
each
area.
The
adjusted
matrix
elements
are
listed
in
T
able
4.
T
able
4.
P
arameter
v
alues
for
the
dif
ferent
PI
controllers
in
simulation
for
the
case
of
study
.
Matrix
dimensions
for
area
III
are
dif
ferent
due
to
the
presence
of
wind
generation.
P
arameter
V
alue
Q
ar
ea
1
diag
([1
;
1
;
10
1
;
10
1
;
10
3
])
Q
ar
ea
2
diag
([1
;
1
;
10
1
;
10
1
;
10
3
])
Q
ar
ea
3
diag
([10
2
;
10
2
;
5
;
5
;
10
2
;
10
2
;
10
2
;
1
;
10
6
;
10
2
])
R
ar
ea
1
10
7
R
ar
ea
2
10
2
R
ar
ea
3
diag
([10
2
;
10
6
;
10
9
])
IJECE
V
ol.
8,
No.
5,
October
2018:
3711
–
3721
Evaluation Warning : The document was created with Spire.PDF for Python.
IJECE
ISSN:
2088-8708
3717
0
25
50
75
100
125
150
175
200
Time [s]
49.2
49.6
50
50.4
50.7
Frequency [Hz]
PI
LQR
Figure
4.
Frequenc
y
de
viation
in
area
II.
LQR
achie
v
ed
a
reduction
of
0.32
H
z
o
v
er
PI
response
in
maximum
v
alue.
0
25
50
75
100
125
150
175
200
Time [s]
49
49.5
50
50.5
51
Frequency [Hz]
PI
LQR
Figure
5.
Frequenc
y
de
viation
in
area
III.
Peak
de
viation
v
alue
for
PI
w
as
0.17
H
z
bigger
than
LQR.
4.4.
Comparison
between
PI
and
LQR
contr
olled
LFC
with
WT
participation
Simulations
were
performed
on
the
selected
benchmark
with
models
and
conditions
pre
viously
de-
scribed.
Figures
4
and
5
depict
frequenc
y
de
viations
for
areas
II
and
III
respecti
v
ely
,
as
the
y
present
more
significant
v
ariations
than
area
I.
Load
disturbance
in
area
I
II
at
30
seconds
causes
the
most
notorious
ef
fects,
not
only
in
the
local
frequenc
y
de
viation
b
ut
also
in
the
other
areas
as
well.
This
beha
vior
could
be
attrib
uted
to
the
inertia
reduction
in
re
gion
3
and
some
latenc
y
in
the
operation
of
WT
control
loops:
po
wer
transferred
to
area
I
II
increases
as
WT
contrib
utions
in
frequenc
y
re
gulation
start.
On
the
other
hand,
the
o
v
erall
magnitude
of
the
frequenc
y
de
viations
o
v
er
the
total
simulation
time
is
smaller
for
the
LQR
controller
in
each
area.
Fe
wer
v
ariations
w
ould
mean
less
stress
in
the
re
gulation
systems,
a
k
e
y
f
actor
as
RES
penetration
increases.
Also,
longer
reco
v
ery
and
settling
times
can
be
seen
for
PI
controllers
at
each
area,
gi
ving
the
LQR
a
better
o
v
erall
performance
for
secondary
control
design
in
the
studied
case.
Figure
6
sho
ws
the
e
xchanged
po
wers
between
area
III
and
the
other
areas.
In
this
case,
LQR
reduces
the
po
wer
e
xchanged
with
other
areas
when
compared
with
PI
response.
Ho
we
v
er
,
a
continued
oscillation
in
po
wer
is
observ
ed,
due
to
wind
v
ariability
causing
fluctuations
in
WT
generation.
This
v
ariation
mak
es
area
III
more
sensiti
v
e
to
sudden
changes
in
load,
as
confirmed
when
the
most
significant
po
wer
de
viations
appear
at
the
same
time
as
the
load
disturbances
occur
.
W
ith
a
load
disturbance
in
area
III
at
30
seconds,
LFC
system
requires
an
increase
in
po
wer
transference
from
the
other
areas
to
mitig
ate
frequenc
y
fluctuations.
Ho
we
v
er
,
the
e
xchanged
po
wer
in
area
III
stabilizes
as
WT
start
contrib
uting
to
frequenc
y
re
gulation.
Figure
7
sho
ws
the
po
wer
generated
by
the
wind
f
arm
in
area
III.
F
ocusing
on
DFIG
WT
performance,
analysis
of
the
control
ef
forts
for
both
LQR
and
PI
strate
gies
in
area
III
is
required.
Control
actions
for
the
pitch-angle
r
ef
are
smaller
for
LQR
than
for
PI
controller
,
as
seen
in
figure
8.
This
beha
vior
seems
to
indicate
that
WT’
s
are
less
stressed
with
LQR
controller
.
Ho
we
v
er
,
the
total
control
ef
fort
of
the
secondary
control
P
c
is
higher
for
the
LQR
than
the
PI
scheme,
as
sho
wn
in
Figure
9.
LQR
is
imposing
an
aggressi
v
e
control
action
in
the
con
v
entional
unit
of
area
III,
diminishing
the
stress
in
WT
contrib
utions
to
frequenc
y
re
gulation.
This,
i
n
turn,
reduces
frequenc
y
fluctuations
due
to
wind
v
ari
ability
for
PI
and
LQR
contr
oller
s
for
F
r
equency
Re
gulation
including
W
ind
Gener
ation
(Semaria
Ruiz)
Evaluation Warning : The document was created with Spire.PDF for Python.
3718
ISSN:
2088-8708
0
25
50
75
100
125
150
175
200
Time [s]
-0.2
-0.1
0
0.1
0.2
0.3
Power exchanged [p.u.]
PI
LQR
Figure
6.
Inter
-area
po
wer
e
xchange
de
viation
for
area
III.
0
25
50
75
100
125
150
175
200
Time [s]
0
0.03
0.06
0.09
0.12
0.15
Wind-turbine power change [p.u.]
PI
LQR
Figure
7.
V
ariations
in
po
wer
generated
by
the
wind
f
arm
in
area
III.
IJECE
V
ol.
8,
No.
5,
October
2018:
3711
–
3721
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IJECE
ISSN:
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3719
0
25
50
75
100
125
150
175
200
Time [s]
0
5
10
15
20
25
30
Pitch angle [Degree]
PI
LQR
Figure
8.
Magnitude
of
control
action
for
v
ariable
r
ef
in
area
III
0
25
50
75
100
125
150
175
200
Time [s]
0
0.02
0.04
0.06
0.08
0.1
ACE signal
PI
LQR
Figure
9.
Magnitude
of
control
action
for
v
ariable
P
c
in
area
III.
the
LQR
in
this
area.
5.
CONCLUSIONS
This
w
ork
studied
the
performance
of
v
ariable-speed
wind
turbines
in
LFC
structure
of
po
wer
syst
ems.
W
ith
inertial
response
emulation
methodology
,
DFIG
WT
were
included
in
the
primary
re
gulation
stage
of
the
LFC.
T
w
o
controllers
were
compared
for
secondary
re
gulation
in
the
test
system,
and
Linear
Quadratic
Re
gulator
presented
a
better
o
v
erall
performance
than
the
Proportional
Inte
gral
controller
.
F
or
e
v
ery
e
xplored
case,
frequenc
y
de
viations
under
LQR
strate
gy
were
smaller
and
the
settling
times
of
the
output
v
ariables
were
also
lo
wer
than
the
PI-controlled
results.
Furthermore,
LQR
operation
diminishe
d
control
ef
forts
of
WT
.
LQR
controller
based
on
the
system
model
and
it
achie
v
ed
acceptable
performances
despite
the
mandatory
requirement
for
linearization
of
the
state-space
representation.
An
unw
anted
o
v
ershoot
in
area
III
frequenc
y
appears
for
both
strate
gies
with
sudden
wind
v
ariations.
This
reaction
occurs
because
the
operating
point
of
the
system
is
changing
with
e
v
ery
v
alue
of
wind
speed.
This
ef
fect
w
as
more
notorious
for
LQR
configuration,
as
the
model
implemented
included
wind
speed
as
a
disturbance.
When
the
operating
point
changed,
linearization
might
ha
v
e
lead
to
the
inadequate
representation
of
the
nonlinear
system.
Neither
PI
nor
LQR
presented
a
total
disturbance
rejection,
and
wind
v
ariability
may
require
the
pairing
of
WT
with
”continuous”
generation
to
reduce
operational
uncertainty
.
Consideration
of
additional
control
s
chemes
for
the
participation
of
v
ariable-speed
WT
in
LFC
enabl
es
the
contrib
ution
of
WT
to
ancillary
tasks.
Ho
we
v
er
,
the
increment
of
WT
in
po
wer
systems
may
lead
to
inertia
reduction
with
the
decreasing
operation
of
con
v
entional
generation
systems.
More
adv
ancements
and
studies
are
needed
to
get
a
better
performance
of
the
wind
units
in
frequenc
y
re
gulation
tasks
or
e
xpanding
their
role
into
secondary
control.
Finally
,
the
implementation
of
a
transition-band
control
loop
between
torque
and
pitch
controllers
of
WT
is
suggested.
This
additional
loop
w
ould
help
to
a
v
oid
o
v
ershoots
in
WT
generated
po
wer
when
wind
v
aries
from
nominal
speed.
PI
and
LQR
contr
oller
s
for
F
r
equency
Re
gulation
including
W
ind
Gener
ation
(Semaria
Ruiz)
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3720
ISSN:
2088-8708
A
CKNO
WLEDGEMENT
Colciencias
supported
contrib
utions
of
S.
Ruiz
and
J.
P
atino
through
the
programs
”J
´
ov
enes
in
v
es-
tig
adores
-
Con
v
ocatoria
N.645
of
2014”
and
”Con
v
ocatoria
528
-
Con
v
ocatoria
Nacional
para
Estudios
de
Doctorados
en
Colombia
2011”,
respecti
v
ely
.
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ariable
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