grid converters for photovoltaic and wind power systems · • the dead‐beat controller belongs...
TRANSCRIPT
Grid Converters for Photovoltaic and Wind Power Systems
by R. Teodorescu, M. Liserre and P. RodriguezISBN: 978‐0‐470‐05751‐3Copyright Wiley 2011
Chapter 12p
Grid Current Control
Outline
• Introduction
• Harmonic requirementsHarmonic requirements
• Current control overview
• Linear current control with separated modulation Use of averaging
PI‐based control
Dead‐beat controlDead beat control
Resonant control
Harmonic compensation
• Modulation techniques Bipolar and unipolar modulation
Three‐phase modulation (continuous and discontinuous)Three phase modulation (continuous and discontinuous)
Multilevel modulation
Interleaved converters
• Operating limits of the grid converter
2
Introduction1Li 2L gLgigv
b)
20
-10
0
v fC Cv edcvC
mag
nitu
de (D
b
-60
-50
-40
-30
-20
L1+L2+Lg
LCL
v
frequency (Hz)10
110
210
310
410 5 -70
• The influence of the capacitor of the filter will be neglected since it is only dealing withthe switching ripple frequencies. In fact at frequencies lower than half of the resonancefrequency the LCL‐filter inverter model and the L‐filter inverter models have the samef h t i tifrequency characteristic
• PI‐based current control implemented in a synchronous frame is commonly used inthree‐phase converters
• In single‐phase converters the PI controller capability to track a sinusoidal reference islimited and Proportional Resonant (PR) can offer better performances
• Modulation has an influence on the design of the converter (dc voltage value), losses andEMC problems including leakage current
3
Harmonic requirements: PV‐systems
• In Europe there is the standard IEC 61727
• In US there is the recommendation IEEE 929
• The recommendation IEEE 1547 is valid for all distributed resourcestechnologies with aggregate capacity of 10 MVA or less at the point of commong gg g p y pcoupling interconnected with electrical power systems at typical primaryand/or secondary distribution voltages
• All of them impose the following conditions regarding grid current harmonic• All of them impose the following conditions regarding grid current harmoniccontent
• The total THD of the grid current should not be higher than 5%g g
4
Harmonic requirements: WT‐systems• In Europe the standard 61400‐21 recommends to apply the standard 61000‐3‐6
valid for polluting loads requiring the current THD smaller than 6‐8% depending on the type of network
harmonic limit 5th 5 6 %5 5-6 %7th 3-4 %
11th 1.5-3 % 13th 1 2 5 %
• In case of several WT systems
13th 1-2.5 %
1
Nhi
hII
• In WT systems asynchronous and synchronous generators directly connected to h d h l h
1i i
the grid have no limitations respect to current harmonics
5
Current Control overview
PWM current control methods
ON/OFF controllers with pulse width modulator
linear Non - linearlinear
fuzzypassivity
PI predictiveD d b t
resonanttiti
hysteresis predictiveoptimized
Dead - beat repetitive
p
6
Linear current control with separated
• Continuous switching vector which components are the duty cycle of each
modulation: use of averaging
22( ) ( ) ( ) ( )3 a b cd t d t d t d t
converter leg
• Average model
1dq d d d
di ti t Ri t e t v t
dt L
• Average model
1qd q q q
dt Ldi t
i t Ri t e t v tdt L
d d dc
q q dc
v t d t v tv t d t v t
• Linearized model v (t)=V
10 0dc
d d d d
VRi t i t d t e td L L L
• Linearized model vdc(t)=Vdc
100q q q qdci t i t d t e tR VdtL LL
7
Linear current control with separated
• Typically PI controllers are used for the current loop in grid inverters
modulation: PI current controlyp y p g
• Technical optimum design (damping 0.707 overshoot 5%)
e ( ) IPI P
kG s k
s
v
v i( )dG s ( )fG s( )PIG si
1( )1 1.5d
s
G sT s
( ) 1i sgv ( ) 1( )( )f
i sG sv s R Ls
1 0
b)0.2
0.4
0.6
0.8
10-1 100 101 102 103 104-20
-15
-10
-5
Mag
nitu
de (D
b
-0.6
-0.4
-0.2
0 10 10 10 10 10 10
-200
-100
0
e (D
egre
e)
-1 -0.5 0 0.5 1
-1
-0.8
100 101 102 103 104-400
-300
Frequency (Hz)
Pha
s
8
Shortcomings of PI controller
1
0.1
0.15
0.2
0.023 0.0235 0.024 0.0245 0.025 0.0255 0.026 0.0265 0.027 0.02750.8
0.82
0.84
0.86
0.88
0.9
0.92
0.94
0.96
0.98
1
steady‐state magnitude and phase
0.019 0.0192 0.0194 0.0196 0.0198 0.02 0.0202 0.0204 0.0206 0.0208 0.021
-0.25
-0.2
-0.15
-0.1
-0.05
0
0.05magnitude and phase
error
limited disturbance rejection capability
• When the current controlled inverter is connected to the grid, the phase errorresults in a power factor decrement and the limited disturbance rejection
bili l d h d f id f d f d icapability leads to the need of grid feed‐forward compensation
• However the imperfect compensation action of the feed‐forward control due tothe background distortion results in high harmonic distortion of the current andconsequently non‐compliance with international power quality standards
9
Use of a PI controller in a rotating frame
didi
gdv
k
In order to overcome the limit of the PI in dealing with
ii
i
di
di
L
qiL
je je
abcv
v
v
IP
kks
limit of the PI in dealing with sinusoidal reference and
harmonic disturbances, the PI control is implemented in
a rotating frameL
qi
gqvgv gv
f gV
abc
IP
kks
a rotating frame
abc
gvgv
je
gdv
gqv
dcv
dcV
P
IP
kks
di
P
Q qi
P
igv 1
3
ga a gb b gc c
gab a gbc b gca c
P v i v i v i
Q v i v i v i
IP
kks
Ikk
0( )
0
IP
PI dqI
P
kk
sG sk
k
Q
IPk
s P s
10
Use of a PI controllers in a rotating frame in
di
gdv
single‐phase systems
• An independent Q control ishi d
IP
kks
i di
d
digd
v
Lv
achieved
• A phase delay block createthe virtual quadrature f
gV
ije i qi
i
je v
L2je
IP
kks
the virtual quadraturecomponent that allows toemulate a two‐phase system
h f h
gv
gv
gv
g
gdv
qi
gqv
2je
• The v component of thecommand voltage is ignoredfor the calculation of the
dc controllerV
je gqv
MPPT dcV di
dci
dcv
Ikk
duty‐cycle
MPPT
P
Q
IPk
s
qi
gdvQ
gqv
Q
11
Use of a PI controllers in two rotating frames
• Under unbalanced conditions inorder to compensate the
di
PIi v
order to compensate theharmonics generated by theinverse sequence present in theid lt b th th iti d i
PIi v
je je
grid voltage both the positive‐ andnegative‐sequence referenceframes are required
qi
di
PIi v
• Obviously using this approach,double computational effort mustbe devoted
PI
PI
i
v
je je
be devoted qi
PI
12
Linear current control with separated modulation: Dead‐beat controller
• The dead‐beat controller belongs to the family of the predictivecontrollers
• They are based on a common principle: to foresee the evolution of thecontrolled quantity (the current) and on the basis of this prediction: To choose the state of the converter (ON OFF predictive) or To choose the state of the converter (ON‐OFF predictive) or
The average voltage produced by the converter (predictive with pulse widthmodulator)
• The starting point is to calculate its derivative to predict the effect of thecontrol action
Th t ll i d l d th b i f th d l f th filt d f• The controller is developed on the basis of the model of the filter and ofthe grid, which is used to predict the system dynamic behavior: thecontroller is inherently sensitive to model and parameter mismatches
13
Dead‐beat controller
• The information on the model is used to decide the switching state of theconverter with the aim to minimize the possible commutations (ON‐OFFconverter with the aim to minimize the possible commutations (ON‐OFFpredictive) or the average voltage that the converter has to produce in order tonull it
e
• In case it is imposed that the error at the
v i( )fG z( )DBG zi
• In case it is imposed that the error at theend of the next sampling period is zerothe controller is defined as “dead‐beat”.It b d t t d th t it i th
gv
It can be demonstrated that it is thefastest current controller allowingnulling the error after two sampling
i d*iperiods i
i
ONt ONt
sTk 1k 2k sT
14
Dead‐beat controller
)1()1()1()(1)1()1( kekekiakikvkv )1()1()1()()1()1( kekekib
kib
kvkv
)()1()(1)1( kekekikvkv Neglecting R! )()1()()1( kekekib
kvkv
0.8
1
0.8
1
0.2
0.4
0.6
0.2
0.4
0.6
450 460 470 480 490 500 510 520 530 540 550-0.2
0
450 460 470 480 490 500 510 520 530 540 550-0.2
0
15
Dead‐beat controller: limits
0
10
20
0
10
20
-30
-20
-10
0
curre
nt [A
]
-30
-20
-10
0
curre
nt [A
]
Due to PWM!
0.04 0.045 0.05 0.055 0.06-60
-50
-40
time [s]0.04 0.045 0.05 0.055 0.06
-60
-50
-40
time [s]time [s] time [s]
Pole-Zero Map
10.6/T
0.5/T0.4/T
10
20
y Ax
is
0
0.2
0.4
0.6
0.8
0.90.80.70.60.50.40.30.20.1
/T
0.9/T
0.8/T
0.7/T 0.3/T
0.2/T
0.1/T
-20
-10
0
10
ent [
A]
Imag
inar
y
0 8
-0.6
-0.4
-0.2
0/T
0.9/T
0.8/T
0.7/T 0.3/T
0.2/T
0.1/T
-50
-40
-30curre
Due to parameter error!
Real Axis
-1 -0.8 -0.6 -0.4 -0.2 0 0.2 0.4 0.6 0.8 1
-1
-0.80.6/T
0.5/T0.4/T
0.04 0.045 0.05 0.055 0.06-60
time [s]
16
Linear current control with separated
R t t l i b d th f G li d I t t (GI)
modulation: Resonant controller• Resonant control is based on the use of Generalized Integrator (GI)
• A double integrator achieves infinite gain at a certain frequency, called resonancefrequency, and almost no attenuation outside this frequency
• The GI will lead to zero stationary error and improved and selective disturbance rejection
2 2
ss
GI
The GI will lead to zero stationary error and improved and selective disturbance rejectionas compared with PI controller
B o d e D ia g r a m2 0 0 2
in
- 2 0 0
- 1 0 0
0
1 0 0
Mag
nitu
de (d
B)
0
0.5
1
1.5
out
2 2
ss
- 9 0
0
9 0
1 8 0
Phas
e (d
eg)
2 0 0
1.5
-1
0.5
0
1 01
1 02
1 03
- 1 8 0
F r e q u e n c y ( H z )0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 2
-2
Resonant control
)()()( jsGjsGsG DCDCAC • The resonant controller can be obtained via afrequency shift
2k s
2 2
2( ) IAC
k sG ss
( ) IDC
kG ss
k
600
800
) 60
80
)
2 2
2( )2
I cAC
c
k sG ss s
( )1 ( )
IDC
c
kG ss
0
200
400
600
Mag
nitu
de (
dB)
0
20
40
60
Mag
nitu
de (
dB)
101
102
103
0
Frequency (Hz)
50
100
deg)
101
102
103
0
Frequency (Hz)
50
100
deg)
101
102
103
-100
-50
0
Pha
se (
d
Freq enc (H )10
110
210
3-100
-50
0
Pha
se (
d
Frequency (Hz) Frequency (Hz)
Bode plots of ideal and non‐ideal PR with kP = 1, kI = 20, = 314 rad/s, c = 10 rad/s18
Resonant control• The stability of the system should be taken into consideration
e
v i( )dG s ( )fG s( )P RESG s
i
• The phase margin (PM) decreases as the resonant frequency approach to thecrossover frequency
2 2P Isk k
s
B o d e D ia g r a m Bode Diag ram
q y
2 21
P Isk k
s R Ls
- 1 0 0
0
1 0 0
2 0 0
3 0 0
4 0 0
Mag
nitu
de (d
B)
0
100
200
300
400
Mag
nitu
de (d
B)
g
- 2 0 0
1 0 0
9 0
0
9 0
1 8 0
Phas
e (d
eg)
- 100
0
0
90
180
Phas
e (d
eg)
1 01
1 02
1 03
- 1 8 0
- 9 0
Fr e q u e n c y ( H z ) Frequenc y (Hz )10
110
210
3-180
-90
P
PM
19
Tuning of resonant control• The gain kP is founded by ensuring the desired bandwidth using either rlocus Matlab
function or SISOTOOL
Th i t l t t k t t li i t th t d t t h• The integral constant kI acts to eliminate the steady‐state phase error
6
2 2( )c P Io
sG s k ks
6
2 2( )c P Io
sG s k ks
0
2
4o
0
2
4 o
-4
-2
-4
-2
0 0.005 0.01 0.015 0.02 0.025 0.03 0.035 0.04 0.045 0.05-6
0 0.005 0.01 0.015 0.02 0.025 0.03 0.035 0.04 0.045 0.05-6
kI = 100 kI = 500
• A higher kI will "catch" the reference faster but with higher overshoot
• Another aspect is that kI determines the bandwidth centered at the resonancefrequency in this case the grid frequency where the attenuation is positive Usually thefrequency, in this case the grid frequency, where the attenuation is positive. Usually, thegrid frequency is stiff and is only allowed to vary in a narrow range, typically ± 1%
20
Discretization of generalized integrators
GI integrator decomposed in two simple integrators Forward integrator for direct path and backward for
2 2
2
1
1
y s u s v sy s s su s s v s y s
ò y u
g
1 1 1
2
( )k k s k ky y T u v
Forward integrator for direct path and backward for feedback path
ys
ò 2
v21k k s kv v T y
The inverter voltage reference
*2 2( ) I
i Pk su s s k
s
Difference equations kp
Control diagram of PR implementation
1 1 1
*,
k k s I k s k
i k P k k
y y T k T v
u k y
Difference equations
ii*
ii
iiui*
ò
ò
yu
v
p
kI
2
aw
Gf(s)
,
21
1
1
i k P k k
k k s k
k k
k k
v v T y
y y
ò 2
max max,y y y yaw
y y y y
1k kv v
max max,y y y y
21
Use of P+resonant controller in stationary
frame
2 2I
Pk sk
s
ii
i
i
v
v
*v
Current controller
abc
i
i
v
2 2I
Pk sk
s
abc
Current controller
• PLL is still indispensable for reference generationPLLgv gv
gv
,f
gV
abcdv
IP
kks
dcv
dc controllerV
dcV
P
controllerP
sin
cos
i
gv
i
i
I
IP
kks
IP
kks
1
3
ga a gb b gc c
gab a gbc b gca c
P v i v i v i
Q v i v i v i
PQ
controllerP
calculationPQ scontrollerQ
calculationPQ
Q
22
From PI in a rotating‐frame to P+res for each phase
• In the hypothesis
• H11(s) = H22(s) = IP
kk H11(s)
+
+
Vd(s)Ed(s)
H11(s) H22(s)
• H12(s) = H21(s) = 0
Pks
H12(s)
H21(s)
H22(s)
+
+ Vq(s)Eq(s)
)()()()()()(
22
11
tethtvtethtv
dd
)()()( 22 qq
0 02 2 2 2 2 2
0 0 0
3 32 2 ( ) 2 2 ( )
I P I I P I IP
k s k k s k k k s kks s s
k 0 0 0
( , . ) 0 02 2 2 2 2 2
0 0 0
2 2 ( ) 2 2 ( )
2 3 3( )3 2 2 ( ) 2 2 ( )
3 3
a bc P I I I P I Ic P
s s s
k k s k k s k k s kG s ks s s
k k s k k k s k k s
( , )0
0
IP
d qc
I
kksG
kk
0 0
2 2 2 2 2 20 0 0
3 32 2 ( ) 2 2 ( )P I I P I I I
Pk k s k k k s k k sk
s s s
0 Pks
23
Linear controllers: from PI in a rotating‐frame to P+res for each phase
zva
( )( ) ( )0 2 1 11 1 ( )( ) ( )0 1 1 23
( )
aa a
bc c
c
v ti t i tRd v ti t i tRdt L
v t
( ) ( ) ( ) 0a b cv t v t v t
)(01)(01)( tvtiRtid aaa
zzvbvc
)(
)(10)(
)(0)(
)(tvtiRLtidt c
a
c
a
c
a
E h t i d t i d l b it lt !
0 02 2 2 2 2 2
3 32 2 ( ) 2 2 ( )
I P I I P I IP
k s k k s k k k s kks s s
22
00sKK ip
Each current is determined only by its voltage!
0 0 0
( , . ) 0 02 2 2 2 2 2
0 0 0
0 0
2 2 ( ) 2 2 ( )
2 3 3( )3 2 2 ( ) 2 2 ( )
3 3
a bc P I I I P I Ic P
P I I P I I I
s s s
k k s k k s k k s kG s ks s s
k k s k k k s k k sk
22
20
2
02
).,(1
00
00)(
sKK
ssKK
s
sG
ip
ip
p
cbac
2 2 2 2 2 20 0 02 2 ( ) 2 2 ( ) Pk
s s s
2
02 sp
24
Linear controllers: results (ideal grid conditions)
current errorharmonic spectrum
PI controller in a rotating frame
current error
P+resonant controller for each phase
current errorharmonic spectrum
P+resonant controller for each phase
25
Linear controllers: results (equivalence of PI in dq and P+res in )
PI controller in a rotating frame triggering LCL‐filter resonance
P+resonant in stationary frame triggering LCL filter resonancey triggering LCL‐filter resonance
26
Comparison under fault
Single‐phase fault:
With dead beat controllerWith dead‐beat controller the current overshoot is
limited
27
Harmonic compensation
• The decomposition of signals into harmonics with the aim ofmonitor and control them is a matter of interest for various electricand electronic systemsand electronic systems
• There have been many efforts to scientifically approach typicalproblems (e.g. faults, unbalance, low frequency EMI) in powerp ( g , , q y ) psystems (power generation, conversion and transmission) throughthe harmonic analysis
• The use of Multiple Synchronous Reference Frames (MSRFs), earlyproposed for the study of induction machines, allowscompensating selected harmonic components in case of two phasecompensating selected harmonic components in case of two‐phasemotors, unbalance machines or in grid connected systems
28
Harmonic compensation
• The harmonic components of power signals can be represented in stationaryor synchronous frames using phasors
• In case of synchronous reference frames each harmonic component istransformed into a dc component (frequency shifting)p ( q y g)
i5 Signal
Signal
7q
i5je
7
Time Time
5q5d
5
7
i
i7je
7
Time Time
SignalSignal
7d
• If other harmonics are contained in the input signal, the dc output will bedi t b d b i l th t b il filt d t
disturbed by a ripple that can be easily filtered out
29
Harmonic compensation by means of synchronous dq‐frames
• Two controllers should beimplemented in two frames
5 0di
1 si v
5
implemented in two framesrotating at -5 and 7
• Or nested frames can be used i.e.i l ti i th i
i v
5je 5je
1 s
implementing in the mainsynchronous frame twocontrollers in two frames rotatingt 6 d 6
5 0qi
7 0di 7
at 6 and -6• Both solutions are equivalent also
in terms of implementation
7di
i
v
7je 7je
1 s
burden because in both the casestwo controllers are needed
7 0qi
i v
1 s
7q
30
Harmonic compensation by means of synchronous dq‐frames
gdv
IP
kks
i
je
i
i
di
qi
g
je
v
v
L
i
L
i i
i i
gv
gv
je
di
qi
gqv
IP
kks
v
i
je
gdv
gqv 5Iks
je
i
ije
5v
5v
55Ik
s
k
5
5
7Iks
je
i
ije
7v
7v
7Ik7 7s
731
Harmonic compensation by means of synchronous dq‐frames
vi
IP
kks
i
di
qi
gdv
L
i
L
di
di
je
v
v
PLLgv
gv
je
di
qi
gqv
IP
kks
v
ii
qi
qi
je
gdv
gqv 5Iks
je
di
qije
5dv
5qv
65Ik
s
k
6
6
7Iks
je
di
qi
6
je
7dv
7qv
7Ik6 6s
632
Harmonic compensation by means of stationary ‐frame
Besides single frequency compensation (obtained with the generalizedintegrator tuned at the grid frequency), selective harmonic compensation canalso be achieved by cascading several resonant blocks tuned to resonate at thedesired low‐order harmonic frequencies to be compensated.
As an example the transfer kAs an example, the transferfunctions of a non‐idealharmonic compensator (HC)designed to compensate for
Pk
u
i
i
designed to compensate forthe 3rd, 5th and 7th harmonicsis reported. 2 2
Ik ss
22
2( )
2Ih c
hk s
G sh
2 2
3,5,7... ( )I h
h
k ss h
23,5,7 2h cs s h , , ( )
33
Harmonic compensation by means of
Open‐loop PR current control system with and Closed loop PR current control system with and
stationary ‐frameOpen loop PR current control system with and
without harmonic compensator Closed loop PR current control system with and
without harmonic compensator
• Having added the harmonic compensator, the open‐loop and closed‐loop bodegraphs changes as it can be observed with dashed line. The change consists inthe appearance of gain peaks at the harmonic frequencies, but what isinteresting to notice is that the dynamics of the controller, in terms ofbandwidth and stability margin remains unaltered
34
Disturbance rejection comparison
Disturbance rejection (current error ratio disturbance) of the PR+HC, PR and P
• Around the 5th and 7th harmonics the PR attenuation being around 125 dB and the PI attenuationonly 8 dB. The PI rejection capability at 5th and 7th harmonic is comparable with that one of asimple proportional controller the integral action being irrelevantsimple proportional controller, the integral action being irrelevant
• PR +HC exhibits high performance harmonic rejections leading to very low current THD!
35
Results: grid voltage background distortion
Effect of the grid voltage background distortion on the
currents
Use of harmonic compensators
36
Results: grid voltage background distortion
Effect of the grid voltage background distortion on the
currents
Use of harmonic compensators
37
Modulation techniques
• Characteristic parameters of these strategies are:Characteristic parameters of these strategies are: The ratio between amplitudes of modulating and carrier waves (called
modulation index M)
The ratio between frequencies of the same signals (called carrier index m)
• These techniques differ for the modulating wave chosen with the goal toobtainobtain A lower harmonic distortion
To shape the harmonic spectrum
To guarantee a linear relation between fundamental output voltage andmodulation index in a wider range
• The space ector mod lations are de eloped on the basis of the space• The space vector modulations are developed on the basis of the spacevector representation of the converter ac side voltage
38
Modulation techniques
• Analogic or digital
• Natural sampled or regular sampled
1
2
Ao
d
VV
• Natural sampled or regular sampled
• Symmetric or asymmetric 4
.1 278
.1 0
Linear
Over-modulation
Square-wave
Optimization both for the linearity and harmonic
t t0
0 .1 0 M for 15fm
.3 24
content
39
Bipolar and unipolar modulations
2dcV
2C
V v t
P
V v t
PP
2dcV
1C
dcV v t
P
dcV v t
PP
00 1
0cos2
sin2
14)(
mm
nn
cndc tntmnmMqJ
qVtv • Bipolar
10120 122cos1cos
218cos2)(
m ncn
dcdc tntmnmMmJ
mVtMVtv
• Unipolar 1m n
40
Bipolar and unipolar modulations
-0 50
0.51
1.5
v ref, v
tri
00.5
11.5
ef, v
tri
0 10 20 30 40-1.5
-10.5
t [ms]
vref vtri
50
0
50
100
v Ao [V
]
0 10 20 30 40-1.5
-1-0.5
t [ms]
v re
vref vtri
0
50
100
v Ao [V
]
0 10 20 30 40-100
-50
t [ms]
-50
0
50
100
v Bo [V
]
0 10 20 30 40-100
-50
v
t [ms]
0
50
100
v Bo [V
]
0 10 20 30 40-100
t [ms]
-100-50
050
100150
v AB [V
]
0 10 20 30 40-100
-50
t [ms]
-500
50100150
v AB [V
]
0 20.40.60.8
1
v AB/V
d
0 20.40.60.8
1
v Ao/V
d
0 10 20 30 40-150100
t [ms] 0 10 20 30 40-150-100
t [ms]
0 5 10 15 20 25 30 35 40 45 50 55 600
0.2
h0 5 10 15 20 25 30 35 40 45 50 55 60
00.2
h
Due to the unipolar PWM the odd carrier and associated sideband harmonics arel t l ll d l i l dd id b d h i (2 1) t dcompletely cancelled leaving only odd sideband harmonics (2n‐1) terms and
even (2m) carrier groups.41
Three‐phase modulation techniques
-0.50
0.51
1.5
v ref, v
tri
50
0
50
100
v An [V
]
0 10 20 30 40-1.5
-1
t [ms]
vref vtri
0
50
100
o [V]
0 10 20 30 40-100
-50
t [ms]
050
100150
[V]
0 10 20 30 40-100
-50
v Ao
t [ms]
50
100
V]
0 10 20 30 40-150-100-50
E
t [ms]
10
20
0 10 20 30 40-100
-50
0
v on [V
t [ms]100150
0 10 20 30 40-20
-10
0
i o [A]
t [ms]
10
20
0 10 20 30 40-150-100-50
050
v AB [V
]
t [ms]0 10 20 30 40
-20
-10
0
10
i d [A]
t [ms][ ] [ ]
The basic three‐phase modulation is obtained applying a bipolar modulation to each of thethree legs of the converter. The modulating signals have to be 120 deg displaced. The phase‐to‐phase voltages are three levels PWM signals that do not contain triple harmonics If theto phase voltages are three levels PWM signals that do not contain triple harmonics. If thecarrier frequency is chosen as multiple of three, the harmonics at the carrier frequency andat its multiples are absent.
42
Extending the linear range (m=1,1)
SPWM
SVM
43
Three‐phase continuous modulation techniques
Continuous modulationsContinuous modulations• Sinusoidal PWM with Third Harmonic Injected – THIPWM. If the third harmonic
has amplitude 25% of the fundamental the minimum current harmonic contentis achieved; if the third harmonic is 17% of the fundamental the maximal linearrange is obtained
• Suboptimum modulation (subopt). A triangular signal is added to theSuboptimum modulation (subopt). A triangular signal is added to themodulating signal. In case the amplitude of the triangular signal is 25% of thefundamental the modulation corresponds to the Space Vector Modulation(SVPWM) with symmetrical placement of zero vectors in sampling time
vdc/2 vdc/2 vdc/2
ACRv ACRv ACRvTHIPWM1/6 THIPWM1/4 SVPWM
(SVPWM) with symmetrical placement of zero vectors in sampling time
0
-vdc/2
0
-vdc/2
0
-vdc/2
onv
DCRv
onv
DCRv
onv
DCRv
0 /2 2/3 2 0 /2 2/3 2 0 /2 2/3 2
Maximum linear range Minimum current harmonics Maximum linear range and almost optimal current harmonics
Triple harmonic injection 1/6 Triple harmonic injection 1/4 Space vector - Triangular 1/4
44
Three‐phase discontinuous modulation techniques
The discontinuous modulations formed by unmodulated 60 degsegments in order to decrease the switching lossessegments in order to decrease the switching losses• Symmetrical flat top modulation, also called DPWM1
• Asymmetrical shifted right flat top modulation, also called DPWM2
• Asymmetrical shifted left flat top modulation, also called DPWM0
vdc/2
0
vdc/2
0
ACRv DPWM0=-/6
DCRvACRv
DPWM1=0
DCRvvdc/2
0
ACRvDPWM2
=/6DCRv
0 /2 2/3 2
-vdc/2
0 /2 2/3 2
-vdc/2onv onv
0 /2 2/3 2
-vdc/2
onv
45
Multilevel converters and modulation techniques
• Wind turbine systems: high power ‐> 52dcV
y g pMW Alstom converter
• Photovoltaic systems: many dc‐links for atransformerless solution
0V 0V0V
V
transformerless solution2dcV
Different possibilities:• Alternative phase opposition (APOD) where carriers in adjacent bands are
A B C
phase shifted by 180 deg
• Phase opposition disposition (POD), where the carriers above the referencezero point are out of phase with those below zero by 180 degzero point are out of phase with those below zero by 180 deg
• Phase disposition (PD), where all the carriers are in phase across all bands46
Multilevel converters and modulation
Cascaded inverter
techniques
abdcV
i L
Cascaded inverter
dcV i L
Neutral point clamped
c
e
v
V
a
be
v
dcV
n
cd
dcV
012
0
2122cos1cos14
cos)(N
icndc
dc
mtntmnmMmJV
tMNVtv
1 1
012 2122cos1cos2m n i
icn mtntmnmMmJm
( 1)i
iN
, 1, 2,3...m kN k • Carrier shifting i Ng
47
Carrier shifting
-1
0
1
v ref, V
tri
0.02 0.025 0.03 0.035 0.04 0.045 0.05 0.055 0.06
100
0
100v ab
[V]
t [s]
0
1
0.02 0.025 0.03 0.035 0.04 0.045 0.05 0.055 0.06
-100vef
, Vtri
t [s]
0.02 0.025 0.03 0.035 0.04 0.045 0.05 0.055 0.06
-1
0
100
[V]
v re
t [s]
0.02 0.025 0.03 0.035 0.04 0.045 0.05 0.055 0.06
-100
0
200
v cd [
V]
t [s]
0.02 0.025 0.03 0.035 0.04 0.045 0.05 0.055 0.06
-200
0
1
pu]
v ad [V
t [s]
0 10 20 30 40 50 600
0.5
h
A [p
48
PD Modulation for NPC
0
1
Vtri
0.02 0.025 0.03 0.035 0.04 0.045 0.05 0.055 0.06
-1
01
V]
Vre
f, V
0.02 0.025 0.03 0.035 0.04 0.045 0.05 0.055 0.06-1
t [s]
Van
[V
tri
1
01
Vre
f, [V
]
0.02 0.025 0.03 0.035 0.04 0.045 0.05 0.055 0.06
-1
0
0.02 0.025 0.03 0.035 0.04 0.045 0.05 0.055 0.06-10
t [s]
0200
Vbn
[V
]
0.02 0.025 0.03 0.035 0.04 0.045 0.05 0.055 0.06-200
0
t [s]1
pu]
Vab
[
Best WTHD !0 10 20 30 40 50 60
0
0.5
h
A [p
49
Inter‐leaved modulation
Shifting the carrier signals (interleaving modulation)reduces the harmonic content in the current withreduces the harmonic content in the current withthe same principle that leads cascaded convertersto have a reduced harmonic content.
H h it i th t t h d d
Parallel inverters
Inter-leaved connection
Without interleaved With interleaved
However here it is the current to have a reducedharmonic content.a
bdcV
i
'L
Inter-leaving
0.04 0.05 0.06 0.07 0.08-101
10.04 0.05 0.06 0.07 0.08-101
1
Without interleaved With interleaved
c d
e
v
dcV 'L
ginductances
0.04 0.05 0.06 0.07 0.08-10
0.04 0.05 0.06 0.07 0.08-100
0100
100
0.04 0.05 0.06 0.07 0.08-10
0.04 0.05 0.06 0.07 0.08-100
0100
100
0.04 0.05 0.06 0.07 0.08-100
0100
0.04 0.05 0.06 0.07 0.08-200
0200
20
0.04 0.05 0.06 0.07 0.08-100
0100
0.04 0.05 0.06 0.07 0.08-200
0200
20
0.04 0.05 0.06 0.07 0.08-20
020
0.04 0.05 0.06 0.07 0.08-20
020
50
Operating limits of the grid converter
Power processed by the converter
2 2 283
dcM V EP E
L
This means that the higher the dc voltage and the smaller the inductance, thehigher the power rating of the converter.
Current sharing ratio transistor/diodes2M
The transistors are conducting about 93% of the current while the load on the
cos3 boost
Mk
gdiodes is very low. In this situation the load on the transistors is slightly higher thanfor normal inverter operation on an induction motor. This is due to the smalldisplacement angle of the grid inverter compared to a typical phase angle of thep g g p yp p gstator current of an induction motor.
51
Conclusions
• The PR uses Generalized Integrators (GI) that are double integrators achievingvery high gain in a narrow frequency band centered on the resonant frequencyand almost null outside
• This makes the PR controller to act as a notch filter at the resonance frequencyand thus it can track a sinusoidal reference without having to increase theswitching frequency or adopting a high gain as it is the case for the classical PIswitching frequency or adopting a high gain, as it is the case for the classical PIcontroller
• PI adopted in a rotating frame achieves similar results, it is equivalent to the usef th PR’ f h hof three PR’s one for each phase
• Also single phase use of PI in a dq frame is feasible
• Dead‐beat controller can compensate current error in two samples but it isead beat co t o e ca co pe sate cu e t e o t o sa p es but t saffected by PWM limits and parameters mismatches
• Dead‐beat controller is faster in limiting overcurrent during faults
f d l h h b• A review of modulation techniques has been given
52