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SamundraGurung, P.Somasundram/ International Journal of Engineering Research and
Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 3, May-Jun 2013, pp.315-326
315 | P a g e
An Improved Electronic Load Controller for Isolated Small
Hydro Wind Hybrid system
SamundraGurung, P.Somasundram
(Power Systems Engineering, College of Engineering, Anna University, Guindy-25)
(Associate Professor, Power Systems Engineering, College of Engineering, Anna University,Guindy-25)
ABSTRACT
A standalone hydro wind hybrid grid feeding a
common three phase four wire load is considered.
There are three generators Synchronous and
Induction Generator fed by a hydro-turbine and a
variable Wind speed turbine driven Permanent
Magnet Synchronous Generator (PMSG). An
Electronic Load Controller (ELC) based on
Statcom principle is connected in shunt with the
system. Vector control scheme for reference
current generation technique of Statcom is
developed. The major objectives in a standalone
system are regulation of frequency and voltage. A
battery bank is used on the dc side of Statcom
thus enabling it for active power control and thus
regulating the frequency. The ELC also performs
other functions such as voltage regulation,
reactive power compensation, neutral current
compensation and harmonic elimination. The
output from PMSG is connected to dc link via
three phase voltage source converter (VSC) which
is used for maximum power point tracking
(MPPT). All models are developed using Matlab,
Simulink.
Keywords-Battery Energy Storage, Voltage and
Frequency regulator, MPPT, Standalone Hydro
Wind system
I. INTRODUCTION
Standalone generation with small hydro turbines is
widely used in developing countries. On average it
can feed as many as 600 houses which can be widely
dispersed. However, only a single source makes these
schemes far from reliable. Normally Synchronous
Generators are preferred in small hydro plants due to
their better voltage regulation capability. For a
standalone Wind system, Permanent Magnet
Synchronous Generators are preferred due to
reduction in gear box and non-requirement for
excitation capacitors. Thus a more reliable isolated
grid can be developed if we can integrate these two
sources.
The major challenge in an isolated grid is voltage and
frequency regulation. The voltages are allowed +-5%
variation and frequency +-2% variation from its
nominal value.
An isolated grid can have an increase in load demand
in future. Thus an additional generator is needed to
meet the extra demand. Induction Generator will be
more suitable for this purpose due to ruggedness and
economic reasons.
Unlike SG they do not have Automatic Voltage
Regulators(AVR) which results in poor voltage
regulation capability. They also need capacitor banks
for voltage buildup during no load condition. When
the IG is loaded, extrareactive power is needed for its
continuous operation.
Variable speed wind generators are very popular and
are an ideal choice for standalone systems. PMSG
based schemes allow much lower cost and thus can
be considered for hybrid with the hydro schemes.
However variable wind schemes suffer from
intermittency and thus a battery based schemes will
give more reliable operation.
Parallel operation of Synchronous and Induction
Generator has been reported in literature[1]. A
Power-Quality Improvement of a Stand-Alone
Induction Generator Using a Statcom with Battery
Energy Storage System is also suggested [2].A
variable speed drive Permanent magnet Synchronous
Generator in hybrid with a hydro driven squirrel cage
Induction Generator along with a battery is also
discussed [3].Analysis of voltage control for a self-
excited induction generator using a current-controlled
voltage source inverter (CC-VSl) which also
performs functions of load balancing and harmonic
elimination is also discussed [4]. A Permanent
Magnet Synchronous Generator-Based Standalone
Wind Energy Supply System has also been suggested
[5].
In this work an attempt is made to use Statcom as
both voltage and frequency controller which acts as
an improved electronic load controller (IELC) for a
standalone system feeding 3-phase 4-wire loads
driven by uncontrolled micro hydroturbine and a
variable wind speed turbine.
The proposed controller is a 4 Leg IGBTs based
VSCs which are connected to the each phaseof the
generator through interfacing inductors.The neutral
point of the load is connected to neutral point of the
fourth leg of the controller. A dc link capacitor and a
battery are connected on the dc bus of the VSCs. The
output from variable wind speed driven PMSG is
connected to a three phase VSC which is then again
connected to the common dc bus. Maximum power
point tracking(MPPT) based on constant torque
control is used.The proposed IELC is also found
SamundraGurung, P.Somasundram/ International Journal of Engineering Research and
Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 3, May-Jun 2013, pp.315-326
316 | P a g e
capable of reactive power compensation, harmonic
elimination and neutral current compensation.
The schematic diagram of the proposed ELC is
shown in Fig. 1. There are two generators namely
Synchronous and Squirrel Cage Induction Generator
fed by uncontrolled hydro turbines. These turbines
always produce a rated power which is given to the
generator. The exciter voltage is limited to 2pu which
is just sufficient for it to produce rated voltage during
full load condition.The Induction Generator is
connected to an external capacitor bank which helps
in voltage buildup at no load condition. When there is
an increase in load demand, additional reactive power
is needed for IG to supply real power. As the AVR
output is limited, Statcom has to supply this
additional reactive power to keep the voltage to its
rated value. The Statcom is implemented using three
phase VSC with an additional leg for neutral current
compensation. On the dc side of the Statcom a
capacitor to filter voltage ripple and a dc battery is
connected. Thus, it can also provide or absorb real
power whenever needed. The amount of real power it
can provide depends on the capacity of the battery. It
can also absorb excess power in case of lightly load
condition and thus the Statcom acts both as a voltage
and frequency controller.
The control structure for a Statcom is based on
Vector Control principle where synchronously
rotating reference frame is considered.This reference
frame is chosen as it gives the transformed quantities
in dc variables which are ideal for compensation and
also filtering purpose.Besides functioning as voltage
and frequency controller, it also performs other
functions like harmonics eliminator and neutral
current compensator. The third generator used is
Permanent Magnet Synchronous Generator which is
driven by a variable speed small wind turbine. As the
scheme is a variable speed wind system, a maximum
power point tracker (MPPT) must be employed for
efficient power production. This is implemented
using Vector Control technique based on constant
torque angle control as shown in Fig. 4. Again a three
phase VSC is used to track the reference speed based
on optimum tip speed ratio at certain wind velocity.
Fig.1. Schematic diagram of Hydro-Wind Hybrid system
II. MODELING OF THE SYSTEM
2.1 StatcomReference Current Generation
The control structure for Statcom is based on
synchronously rotating reference frame theory as
shown in Fig. 3.When the three phase voltages are
transformed in dq quantities, based on given direction
of q axis leading d,peak voltage isobserved on the d
axis only.A three phase PLL is used to synchronize
and thus calculate the position of transformation
angle ϴs.
Real power and reactive power in dq co-ordinates can
be written as
𝑃 =
3
2
∗ 𝑉𝑑 𝐼 𝑑 + 𝑉𝑞 𝐼𝑞 (1)
𝑄 =
3
2
∗ 𝑉𝑞 𝐼𝑞 − 𝑉𝑑 𝐼 𝑑 (2)
As Vq=0 thus
𝑃 = 𝑉𝑑 𝐼 𝑑(3)
𝑄 = −𝑉𝑑 𝐼𝑞(4)
where, Vd, Id, Vq, Iq are d-axis and q-axis voltage and
current respectively.
Equation (3) and (4) shows the decoupling of active
and reactive power. Thus by controlling Id we can
control the real power and by controlling Iq we can
control the reactive power.
Since the battery cannot produce reactive power and
the dc link voltage is held constant by the battery
unlike in other schemes where it is held constant by
capacitor, Id directly relates to the current that should
be produced or absorbed by the battery to keep the
frequency constant. This current is kept within a safe
value given by the battery rating using a limiter.
d-axis reference current generation
SamundraGurung, P.Somasundram/ International Journal of Engineering Research and
Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 3, May-Jun 2013, pp.315-326
317 | P a g e
When the speed of the machine is at rated value and
thus frequency is at its nominal value, there is no
absorption or production. The load current is
decomposed into its direct and quadrature
component. When harmonic loads are present, there
will also be an oscillating component in which is
added to frequency regulating component.
.
Fig. 2. Block diagram of Statcom reference generation
𝜔𝑒𝑟𝑟 = 𝜔 𝑟𝑒𝑓 𝑛 − 𝜔𝑟 (5)
𝐼 𝑑𝑓 = 𝐼 𝑑𝑓 𝑛 − 1 + 𝐾𝑝𝑓 𝜔𝑒𝑟𝑟 − 𝜔𝑒𝑟𝑟 𝑛 − 1 +
𝐾𝑖𝑓 𝜔𝑒𝑟𝑟 (n)(6)
𝐼 𝑑𝑜 = 𝐼 𝑑𝑙 − 𝐼 𝑑𝑙𝑓 (7)
𝐼 𝑑 = 𝐼 𝑑𝑜 + 𝐼 𝑑𝑓 (8)
𝜔ref is the reference speed,𝜔is the actual rotor
speed, Kpf&Kifare PI controller gains respectively,
Ido is the oscillating component of load current, Idl
is the total d axis load current, Idlf is the filtered d
axis load current.
q-axis reference generation
For voltage regulation, peak voltage of three phase
system (325 in this case) is compared with the
direct axiscomponent of the voltage which is
obtained after passing through a low pass filter of
10Hz. The error is passed through a PI controller
and subtracted from total load quadrature
component
𝑉𝑒𝑟𝑟 = 𝑉𝑑𝑟𝑒𝑓 𝑛 − 𝑉𝑑 (9)
𝐼𝑞𝑣 = 𝐼𝑞𝑣 𝑛 − 1 + 𝐾𝑝𝑣 𝑉𝑑 𝑛 − 𝑉𝑑 𝑛 − 1 +
𝐾𝑖𝑣 𝑉𝑒𝑟𝑟 𝑛 (10)
𝐼𝑞 = 𝐼𝑞𝑙 − 𝐼𝑞𝑣(11)
WhereVdref is the rated d axis voltage, Kpv and Kiv
are PI controller values respectively. Iql is the q-
axis load current.
After obtaining reference currents from dq to abc
conversion, these are compared with the actual
Statcom currents and given to a PWM generator.A
similar method of reference current generation
technique can also be seen in [6].
Fig.3. Vector control of Statcom
SamundraGurung, P.Somasundram/ International Journal of Engineering Research and
Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 3, May-Jun 2013, pp.315-326
318 | P a g e
2.2Vector control of PMSG
The stator flux linkage equations can be written as
[7]
𝑉𝑞𝑠
𝑟
= 𝑅 𝑞 𝑖 𝑞𝑠
𝑟
+ 𝑝𝜆 𝑞𝑠
𝑟
+ 𝜔𝑟 𝜆 𝑑𝑠
𝑟
(12)
𝑉𝑑𝑠
𝑟
= 𝑅 𝑑 𝑖 𝑑𝑠
𝑟
+ 𝑝𝜆 𝑑𝑠
𝑟
− 𝜔𝑟 𝜆 𝑞𝑠
𝑟
(13)
𝜆 𝑞𝑠
𝑟
= 𝐿 𝑠 𝑖 𝑞𝑠
𝑐
+ 𝐿 𝑚 𝑖 𝑞𝑟
𝑐
(14)
𝜆 𝑑𝑠
𝑟
= 𝐿 𝑠 𝑖 𝑑𝑠
𝑐
+ 𝐿 𝑚 𝑖 𝑑𝑟
𝑐
(15)
𝜆 𝑞𝑠
𝑟
= 𝐿 𝑞 𝑖 𝑞𝑠
𝑟
(16)
𝑇𝑒 =
3
2
𝑃
2
𝑖 𝑞𝑠
𝑟
𝜆 𝑑𝑠
𝑟
− 𝑖 𝑑𝑠
𝑟
𝜆 𝑞𝑠
𝑟
(17)
𝑇𝑒 =
3
2
𝑃
2
𝑖 𝑞𝑠
𝑟
𝜆 𝑎𝑓
𝑟
+ (𝐿 𝑑 − 𝐿 𝑞 )𝑖 𝑑𝑠
𝑟
𝑖 𝑞𝑠
𝑟
(18)
𝑇𝑒 =
3
2
𝑃
2
𝑖 𝑞𝑠
𝑟
𝜆 𝑎𝑓
𝑟
(19)
where Vqs
r
, Iqs
r
are rotor q axis voltage and current
𝜆qs
r
and𝜆ds
r
are stator q and d axis flux linkages, Ld,
Lq, Lm are d, q axis inductance and mutual
inductance respectively, P is number of poles, Te is
electromagnetic torque .
This vector control scheme is based on constant
torque angle control, where torque angle 𝛿 is
maintained at 90 degrees as shown in Fig. 4
hence, the field or direct axis current is made to
be zero, leaving only the torque or quadrature
axis current in place.
Reference speed can be found by
𝜔𝑜𝑝𝑡 =
𝜆∗𝑉
𝑟
(20)
𝜔𝑒𝑟𝑟 = 𝜔 𝑟𝑒𝑓 𝑛 − 𝜔𝑟 (21)
𝐼𝑞 = 𝐼𝑞 𝑛 − 1 + 𝐾𝑝𝑔 𝜔𝑒𝑟𝑟 − 𝜔𝑒𝑟𝑟 𝑛 − 1 +
𝐾𝑖𝑔 𝜔𝑒𝑟𝑟 (n) (22)
This speed is compared with the actual speed and
passed through a PI controller with limiter to
produce the reference torque.
Fig. 4.Vector control of PMSG
As, Id=0
𝐼𝑞 =
4∗𝑇𝑒
3∗𝑃∗𝜆𝑎𝑓
(23)
Ѳ 𝑚 =
𝑃
2
∗ Ѳ 𝑒 (24)
𝑖 𝑝𝑎𝑒 = 𝑖 𝑝𝑎
∗
− 𝑖 𝑝𝑎 (25)
𝑖 𝑝𝑏𝑒 = 𝑖 𝑝𝑏
∗
− 𝑖 𝑝𝑏 (26)
𝑖 𝑝𝑐𝑒 = 𝑖 𝑝𝑐
∗
− 𝑖 𝑝𝑐 (27)
Where, 𝜔opt is the optimal speed, 𝜆 is the tip speed
ratio, V is the free wind velocity, r is the radius of
the turbine, 𝜔ref is the reference speed,𝜔r is the
actual rotor speed, Iq is quadrature current
component, Kpg&Kigare PI controller gains
respectively, i*
pa, i*
pb, i*
pc are reference PMSG a, b
and c currents respectively, ipa, ipb and ipc are actual
PMSG a ,b, c currents respectively, Ѳm and Ѳe are
mechanical and electrical angles respectively.
These currents are transformed into abc domain
and compared with the actual currents and given to
the PWM generator and to the three phase VSC.
Fig. 5. Control scheme of PMSG
converter
III. DESIGN OF COMPONENTS
3.1DC link design
For proper PWM operation,
𝑉𝑑𝑐 > 2
2
3
∗ 𝑉𝑙 ∗ 𝑚 𝑎 (28)
Taking line voltageVl as 400V and modulation
index, ma as 1, Vdc is chosen as 700V which is also
the battery dc voltage.
C >=
𝑚 𝑎 ∗𝐼𝑠
4∗2𝜋𝑓∗∆𝑉
(29)
C is the dc link capacitance, ∆V is the allowed
voltage ripple (5% in this case), Isis the Statcom
current, f is the supply frequency.
The battery is chosen of 700V, 150Ah and C as
8000μF.
3.2 Synchronous link reactor design
The synchronous link reactor is chosen as [8]
SamundraGurung, P.Somasundram/ International Journal of Engineering Research and
Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 3, May-Jun 2013, pp.315-326
319 | P a g e
𝐿 =
𝑉𝑎𝑛 +0.5∗𝑉𝑑𝑐
4∗𝑓𝑡∗𝜉
(30)
Where, Van is the phase voltage, ft is the frequency
of the carrier wave, 𝜉 is the amplitude of carrier
wave.
Taking, Van=230V, ft=20 KHz,
L=7.25mH
3.3. Selection of wind turbine
The wind turbine used for simulation purpose is
taken from Simpower systems, Matlab Simulink
which has maximum power coefficient cp=0.48
and tip speed ratio 𝜆=8.1. Turbine rating is taken as
5kW and radius can be found using
𝑃 =
1
2
∗ 𝐶𝑝 ∗ 𝜋 ∗ 𝑅2
∗ 𝜌 ∗ 𝑉3
(31)
Where R= radius of the turbine, 𝜌=air density, v is
wind velocity.
R=2.3m
Fig. 6. Turbine output characteristics
3.4 Tuning of PMSG converter
The overall PMSG side with its controller can be
can be modeled as [9]
Fig. 7. Closed loop speed control of PMSG
𝐾𝑠 =
4
9∗𝐾𝑔∗𝑇𝑤𝑖
(32)
𝑇𝑠 = 6 ∗ 𝑇𝑤𝑖
(33)
Root locus method is used to tune the PI controller
where the design requirement taken are damping
ratio, 𝜉=0.707, maximum overshoot, Mp = 2%, rise
time, tr= 0.005s and settling time, ts= 0.01s.
Fig. 8. Root locus plot of closed loop
system
Fig. 9.Step input response for given
system
SamundraGurung, P.Somasundram/ International Journal of Engineering Research and
Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 3, May-Jun 2013, pp.315-326
320 | P a g e
IV. RESULTS
4.1 Statcom as voltage regulator
At 0.5s an IG is connectedthrough a circuit breakerin
parallel with the Synchronous Generator as shown in
Fig. 11.There is an injection of reactive power by the
Statcom which quickly restores thedipping terminal
voltage back to its rated value.
4.2 Statcom as frequency regulator
As in Fig. 10.Initally as the total connected load is
12kW and Synchronous Generator produces around
15.4kW, remaining 3.4kW is consumed by the
Battery leading to its charging.
At 0.5s, Induction generator of 3.8kW is connected
thus changing total generating power (SG and IG) to
19.2kW, thus causing a mismatch of 7.2kW. This
power is again consumed by the battery.
At 1s, an extra load of 12kW and 8kVAR is
connected. This causes deficiency in the generating
power of around 4kW which is supplied by the
Statcom. Thus we can see asStatcom keeps the total
generated and consumed power equal and thus the
system frequency is kept at nominal value (50Hz).
4.3 Statcom as reactive power compensator
In Fig. 11.at 1s, an extra load of 12kW and 9kVAR,
considering power factor of 0.8 lagging is connected.
Since the Statcom is designed to keep the supply side
power factor as unity, its reactive power injection
increases from 0 to 8kVAR.
4.4 Statcom as neutral current compensator
At 1.5s, an unbalanced load of 6kW with two phase
switched off is connected. Thus the load currents are
highly unbalanced as shown in Fig. 11. However, the
source currents are balanced as the Statcom provides
a path for neutral current through its fourth leg.
4.5 Statcom as harmonic eliminator
Fig. 12 shows connection of only nonlinear load. The
nonlinear here considered is a three phase diode
bridge rectifier with 50 ohms resistor. As we can
notice, the currents are highly distorted but the source
currents are linear.
Fig. 13 and 14 shows the Total harmonic distortion
(THD) values of load and source current.Load
current have THD equal to 25% which is very high
whereas source currents have their THD well within
allowed level of 3%.
4.6 PMSG output
Initially, wind velocity is at 8m/s as shown in Fig. 17
which gives reference speed of 34.11 rad/s for
maximum power extraction. The electromagnetic
torque developed is 45Nm and the generator output is
2kW. At 0.5s, wind velocity increases to 12m/s
which correspond to reference speed of 51 rad/s. The
electromagnetic torque developed is around 102Nm
and the Power output is 4.7kW.
SamundraGurung, P.Somasundram/ International Journal of Engineering Research and
Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 3, May-Jun 2013, pp.315-326
321 | P a g e
Fig. 10. Statcom as frequency regulator
SamundraGurung, P.Somasundram/ International Journal of Engineering Research and
Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 3, May-Jun 2013, pp.315-326
322 | P a g e
Fig. 11. Statcom as voltage regulator
Fig. 11. Statcom
as voltage regulator
SamundraGurung, P.Somasundram/ International Journal of Engineering Research and
Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 3, May-Jun 2013, pp.315-326
323 | P a g e
Fig. 12.Statcom as harmonic eliminator
SamundraGurung, P.Somasundram/ International Journal of Engineering Research and
Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 3, May-Jun 2013, pp.315-326
324 | P a g e
Fig. 13. THD of source current
Fig. 14. THD of source current
Fig. 15. Speed of Induction Generator (pu)
Fig. 16. Speed of Synchronous Generator (pu)
SamundraGurung, P.Somasundram/ International Journal of Engineering Research and
Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 3, May-Jun 2013, pp.315-326
325 | P a g e
Fig. 17. Performance of PMSG converter
SamundraGurung, P.Somasundram/ International Journal of Engineering Research and
Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 3, May-Jun 2013, pp.315-326
326 | P a g e
V. CONCLUSION
The paper has divided its focus on mainly two
renewable sources, uncontrolled Hydro turbine and
variable Wind turbine. An Electronic load controller
or a Statcom is used interchangeably because it
functions both as voltage and frequency control. It is
based on vector control scheme based on
synchronously rotating dq referenceframe.
A battery is connected on the dc side which is
charged and discharged by the bidirectional activity
of Statcom. This action helps to keep the frequency
constant. Similarly, the battery is also charged from
the output of PMSG converter. The Statcom also
performs other functions like voltage regulation,
harmonic elimination and neutral current
compensation.
The PMSG machine converter is employed for MPPT
tracking. Thus an overall hydro and wind hybrid has
been developed which can perform satisfactorily
even in an isolated case. All these models are
developed using Matlab,Simulink.This paper can be
extended to more detailedBattery Energy
Management system. It can also be extended by using
Multi level Inverter for higher power ratings and
lesser harmonic output.
APPENDIX
Synchronous Generator
16kVA, 400V, 1500rpm, Xd=1.734pu,
Xd’=0.177puXd’’ = 0.111pu, Xq = 0.861pu ,
Xq’’=0.199pu,Xl=0.07pu,Td=0.018s,Td’’=0.0045s,T
q’’=0.0045,Rs=0.02pu,H=0.5s,P=2
InductionGenerator
4kVA,400V,50Hz,Rs=0.03513pu,Lls=0.04586pu,Rr’
=0.03488pu,Llr’=0.04586pu,Lm=2.8pu,H=0.2s,
Excitation capacitor=1.5kVAR
Permanent Magnet Synchronous Generator
Rs=0.085Ω,Ld=0.95mH,Lq=0.95mH, Flux
linkage=0.192Vs, J=0.008kgm2
,F=0.11Nms,P=8
Synchronous link reactor
Rf=0.44Ω,Lf=7.25mH
Statcom 40kVA
Vdc=700V,Cdc=8000μF,Battery=700V,150AH
PI controller
Frequency controller, Kpf=9000,Kif=30000
Ac voltage controller, Kpv=0.02,Kiv=0.02
PMSG converter, Kpg=5, Kig=80
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[5] PrabhaKundur, Power System Stability and
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Education, 2006)
[6] Muhammad H. Rashid, Power electronics
handbook (Burlington: Butterworth-
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[7] K. R. Padiyar, Facts controllers in power
transmission and distribution (Daryaganj,
New Delhi: New Age International (P) Ltd,
2007)
[8] R. Krishnan,Electric Motor Drives: Modeling,
Analysis and Control(New Delhi:PHI
Learning, 2009).

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  • 1. SamundraGurung, P.Somasundram/ International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 3, May-Jun 2013, pp.315-326 315 | P a g e An Improved Electronic Load Controller for Isolated Small Hydro Wind Hybrid system SamundraGurung, P.Somasundram (Power Systems Engineering, College of Engineering, Anna University, Guindy-25) (Associate Professor, Power Systems Engineering, College of Engineering, Anna University,Guindy-25) ABSTRACT A standalone hydro wind hybrid grid feeding a common three phase four wire load is considered. There are three generators Synchronous and Induction Generator fed by a hydro-turbine and a variable Wind speed turbine driven Permanent Magnet Synchronous Generator (PMSG). An Electronic Load Controller (ELC) based on Statcom principle is connected in shunt with the system. Vector control scheme for reference current generation technique of Statcom is developed. The major objectives in a standalone system are regulation of frequency and voltage. A battery bank is used on the dc side of Statcom thus enabling it for active power control and thus regulating the frequency. The ELC also performs other functions such as voltage regulation, reactive power compensation, neutral current compensation and harmonic elimination. The output from PMSG is connected to dc link via three phase voltage source converter (VSC) which is used for maximum power point tracking (MPPT). All models are developed using Matlab, Simulink. Keywords-Battery Energy Storage, Voltage and Frequency regulator, MPPT, Standalone Hydro Wind system I. INTRODUCTION Standalone generation with small hydro turbines is widely used in developing countries. On average it can feed as many as 600 houses which can be widely dispersed. However, only a single source makes these schemes far from reliable. Normally Synchronous Generators are preferred in small hydro plants due to their better voltage regulation capability. For a standalone Wind system, Permanent Magnet Synchronous Generators are preferred due to reduction in gear box and non-requirement for excitation capacitors. Thus a more reliable isolated grid can be developed if we can integrate these two sources. The major challenge in an isolated grid is voltage and frequency regulation. The voltages are allowed +-5% variation and frequency +-2% variation from its nominal value. An isolated grid can have an increase in load demand in future. Thus an additional generator is needed to meet the extra demand. Induction Generator will be more suitable for this purpose due to ruggedness and economic reasons. Unlike SG they do not have Automatic Voltage Regulators(AVR) which results in poor voltage regulation capability. They also need capacitor banks for voltage buildup during no load condition. When the IG is loaded, extrareactive power is needed for its continuous operation. Variable speed wind generators are very popular and are an ideal choice for standalone systems. PMSG based schemes allow much lower cost and thus can be considered for hybrid with the hydro schemes. However variable wind schemes suffer from intermittency and thus a battery based schemes will give more reliable operation. Parallel operation of Synchronous and Induction Generator has been reported in literature[1]. A Power-Quality Improvement of a Stand-Alone Induction Generator Using a Statcom with Battery Energy Storage System is also suggested [2].A variable speed drive Permanent magnet Synchronous Generator in hybrid with a hydro driven squirrel cage Induction Generator along with a battery is also discussed [3].Analysis of voltage control for a self- excited induction generator using a current-controlled voltage source inverter (CC-VSl) which also performs functions of load balancing and harmonic elimination is also discussed [4]. A Permanent Magnet Synchronous Generator-Based Standalone Wind Energy Supply System has also been suggested [5]. In this work an attempt is made to use Statcom as both voltage and frequency controller which acts as an improved electronic load controller (IELC) for a standalone system feeding 3-phase 4-wire loads driven by uncontrolled micro hydroturbine and a variable wind speed turbine. The proposed controller is a 4 Leg IGBTs based VSCs which are connected to the each phaseof the generator through interfacing inductors.The neutral point of the load is connected to neutral point of the fourth leg of the controller. A dc link capacitor and a battery are connected on the dc bus of the VSCs. The output from variable wind speed driven PMSG is connected to a three phase VSC which is then again connected to the common dc bus. Maximum power point tracking(MPPT) based on constant torque control is used.The proposed IELC is also found
  • 2. SamundraGurung, P.Somasundram/ International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 3, May-Jun 2013, pp.315-326 316 | P a g e capable of reactive power compensation, harmonic elimination and neutral current compensation. The schematic diagram of the proposed ELC is shown in Fig. 1. There are two generators namely Synchronous and Squirrel Cage Induction Generator fed by uncontrolled hydro turbines. These turbines always produce a rated power which is given to the generator. The exciter voltage is limited to 2pu which is just sufficient for it to produce rated voltage during full load condition.The Induction Generator is connected to an external capacitor bank which helps in voltage buildup at no load condition. When there is an increase in load demand, additional reactive power is needed for IG to supply real power. As the AVR output is limited, Statcom has to supply this additional reactive power to keep the voltage to its rated value. The Statcom is implemented using three phase VSC with an additional leg for neutral current compensation. On the dc side of the Statcom a capacitor to filter voltage ripple and a dc battery is connected. Thus, it can also provide or absorb real power whenever needed. The amount of real power it can provide depends on the capacity of the battery. It can also absorb excess power in case of lightly load condition and thus the Statcom acts both as a voltage and frequency controller. The control structure for a Statcom is based on Vector Control principle where synchronously rotating reference frame is considered.This reference frame is chosen as it gives the transformed quantities in dc variables which are ideal for compensation and also filtering purpose.Besides functioning as voltage and frequency controller, it also performs other functions like harmonics eliminator and neutral current compensator. The third generator used is Permanent Magnet Synchronous Generator which is driven by a variable speed small wind turbine. As the scheme is a variable speed wind system, a maximum power point tracker (MPPT) must be employed for efficient power production. This is implemented using Vector Control technique based on constant torque angle control as shown in Fig. 4. Again a three phase VSC is used to track the reference speed based on optimum tip speed ratio at certain wind velocity. Fig.1. Schematic diagram of Hydro-Wind Hybrid system II. MODELING OF THE SYSTEM 2.1 StatcomReference Current Generation The control structure for Statcom is based on synchronously rotating reference frame theory as shown in Fig. 3.When the three phase voltages are transformed in dq quantities, based on given direction of q axis leading d,peak voltage isobserved on the d axis only.A three phase PLL is used to synchronize and thus calculate the position of transformation angle ϴs. Real power and reactive power in dq co-ordinates can be written as 𝑃 = 3 2 ∗ 𝑉𝑑 𝐼 𝑑 + 𝑉𝑞 𝐼𝑞 (1) 𝑄 = 3 2 ∗ 𝑉𝑞 𝐼𝑞 − 𝑉𝑑 𝐼 𝑑 (2) As Vq=0 thus 𝑃 = 𝑉𝑑 𝐼 𝑑(3) 𝑄 = −𝑉𝑑 𝐼𝑞(4) where, Vd, Id, Vq, Iq are d-axis and q-axis voltage and current respectively. Equation (3) and (4) shows the decoupling of active and reactive power. Thus by controlling Id we can control the real power and by controlling Iq we can control the reactive power. Since the battery cannot produce reactive power and the dc link voltage is held constant by the battery unlike in other schemes where it is held constant by capacitor, Id directly relates to the current that should be produced or absorbed by the battery to keep the frequency constant. This current is kept within a safe value given by the battery rating using a limiter. d-axis reference current generation
  • 3. SamundraGurung, P.Somasundram/ International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 3, May-Jun 2013, pp.315-326 317 | P a g e When the speed of the machine is at rated value and thus frequency is at its nominal value, there is no absorption or production. The load current is decomposed into its direct and quadrature component. When harmonic loads are present, there will also be an oscillating component in which is added to frequency regulating component. . Fig. 2. Block diagram of Statcom reference generation 𝜔𝑒𝑟𝑟 = 𝜔 𝑟𝑒𝑓 𝑛 − 𝜔𝑟 (5) 𝐼 𝑑𝑓 = 𝐼 𝑑𝑓 𝑛 − 1 + 𝐾𝑝𝑓 𝜔𝑒𝑟𝑟 − 𝜔𝑒𝑟𝑟 𝑛 − 1 + 𝐾𝑖𝑓 𝜔𝑒𝑟𝑟 (n)(6) 𝐼 𝑑𝑜 = 𝐼 𝑑𝑙 − 𝐼 𝑑𝑙𝑓 (7) 𝐼 𝑑 = 𝐼 𝑑𝑜 + 𝐼 𝑑𝑓 (8) 𝜔ref is the reference speed,𝜔is the actual rotor speed, Kpf&Kifare PI controller gains respectively, Ido is the oscillating component of load current, Idl is the total d axis load current, Idlf is the filtered d axis load current. q-axis reference generation For voltage regulation, peak voltage of three phase system (325 in this case) is compared with the direct axiscomponent of the voltage which is obtained after passing through a low pass filter of 10Hz. The error is passed through a PI controller and subtracted from total load quadrature component 𝑉𝑒𝑟𝑟 = 𝑉𝑑𝑟𝑒𝑓 𝑛 − 𝑉𝑑 (9) 𝐼𝑞𝑣 = 𝐼𝑞𝑣 𝑛 − 1 + 𝐾𝑝𝑣 𝑉𝑑 𝑛 − 𝑉𝑑 𝑛 − 1 + 𝐾𝑖𝑣 𝑉𝑒𝑟𝑟 𝑛 (10) 𝐼𝑞 = 𝐼𝑞𝑙 − 𝐼𝑞𝑣(11) WhereVdref is the rated d axis voltage, Kpv and Kiv are PI controller values respectively. Iql is the q- axis load current. After obtaining reference currents from dq to abc conversion, these are compared with the actual Statcom currents and given to a PWM generator.A similar method of reference current generation technique can also be seen in [6]. Fig.3. Vector control of Statcom
  • 4. SamundraGurung, P.Somasundram/ International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 3, May-Jun 2013, pp.315-326 318 | P a g e 2.2Vector control of PMSG The stator flux linkage equations can be written as [7] 𝑉𝑞𝑠 𝑟 = 𝑅 𝑞 𝑖 𝑞𝑠 𝑟 + 𝑝𝜆 𝑞𝑠 𝑟 + 𝜔𝑟 𝜆 𝑑𝑠 𝑟 (12) 𝑉𝑑𝑠 𝑟 = 𝑅 𝑑 𝑖 𝑑𝑠 𝑟 + 𝑝𝜆 𝑑𝑠 𝑟 − 𝜔𝑟 𝜆 𝑞𝑠 𝑟 (13) 𝜆 𝑞𝑠 𝑟 = 𝐿 𝑠 𝑖 𝑞𝑠 𝑐 + 𝐿 𝑚 𝑖 𝑞𝑟 𝑐 (14) 𝜆 𝑑𝑠 𝑟 = 𝐿 𝑠 𝑖 𝑑𝑠 𝑐 + 𝐿 𝑚 𝑖 𝑑𝑟 𝑐 (15) 𝜆 𝑞𝑠 𝑟 = 𝐿 𝑞 𝑖 𝑞𝑠 𝑟 (16) 𝑇𝑒 = 3 2 𝑃 2 𝑖 𝑞𝑠 𝑟 𝜆 𝑑𝑠 𝑟 − 𝑖 𝑑𝑠 𝑟 𝜆 𝑞𝑠 𝑟 (17) 𝑇𝑒 = 3 2 𝑃 2 𝑖 𝑞𝑠 𝑟 𝜆 𝑎𝑓 𝑟 + (𝐿 𝑑 − 𝐿 𝑞 )𝑖 𝑑𝑠 𝑟 𝑖 𝑞𝑠 𝑟 (18) 𝑇𝑒 = 3 2 𝑃 2 𝑖 𝑞𝑠 𝑟 𝜆 𝑎𝑓 𝑟 (19) where Vqs r , Iqs r are rotor q axis voltage and current 𝜆qs r and𝜆ds r are stator q and d axis flux linkages, Ld, Lq, Lm are d, q axis inductance and mutual inductance respectively, P is number of poles, Te is electromagnetic torque . This vector control scheme is based on constant torque angle control, where torque angle 𝛿 is maintained at 90 degrees as shown in Fig. 4 hence, the field or direct axis current is made to be zero, leaving only the torque or quadrature axis current in place. Reference speed can be found by 𝜔𝑜𝑝𝑡 = 𝜆∗𝑉 𝑟 (20) 𝜔𝑒𝑟𝑟 = 𝜔 𝑟𝑒𝑓 𝑛 − 𝜔𝑟 (21) 𝐼𝑞 = 𝐼𝑞 𝑛 − 1 + 𝐾𝑝𝑔 𝜔𝑒𝑟𝑟 − 𝜔𝑒𝑟𝑟 𝑛 − 1 + 𝐾𝑖𝑔 𝜔𝑒𝑟𝑟 (n) (22) This speed is compared with the actual speed and passed through a PI controller with limiter to produce the reference torque. Fig. 4.Vector control of PMSG As, Id=0 𝐼𝑞 = 4∗𝑇𝑒 3∗𝑃∗𝜆𝑎𝑓 (23) Ѳ 𝑚 = 𝑃 2 ∗ Ѳ 𝑒 (24) 𝑖 𝑝𝑎𝑒 = 𝑖 𝑝𝑎 ∗ − 𝑖 𝑝𝑎 (25) 𝑖 𝑝𝑏𝑒 = 𝑖 𝑝𝑏 ∗ − 𝑖 𝑝𝑏 (26) 𝑖 𝑝𝑐𝑒 = 𝑖 𝑝𝑐 ∗ − 𝑖 𝑝𝑐 (27) Where, 𝜔opt is the optimal speed, 𝜆 is the tip speed ratio, V is the free wind velocity, r is the radius of the turbine, 𝜔ref is the reference speed,𝜔r is the actual rotor speed, Iq is quadrature current component, Kpg&Kigare PI controller gains respectively, i* pa, i* pb, i* pc are reference PMSG a, b and c currents respectively, ipa, ipb and ipc are actual PMSG a ,b, c currents respectively, Ѳm and Ѳe are mechanical and electrical angles respectively. These currents are transformed into abc domain and compared with the actual currents and given to the PWM generator and to the three phase VSC. Fig. 5. Control scheme of PMSG converter III. DESIGN OF COMPONENTS 3.1DC link design For proper PWM operation, 𝑉𝑑𝑐 > 2 2 3 ∗ 𝑉𝑙 ∗ 𝑚 𝑎 (28) Taking line voltageVl as 400V and modulation index, ma as 1, Vdc is chosen as 700V which is also the battery dc voltage. C >= 𝑚 𝑎 ∗𝐼𝑠 4∗2𝜋𝑓∗∆𝑉 (29) C is the dc link capacitance, ∆V is the allowed voltage ripple (5% in this case), Isis the Statcom current, f is the supply frequency. The battery is chosen of 700V, 150Ah and C as 8000μF. 3.2 Synchronous link reactor design The synchronous link reactor is chosen as [8]
  • 5. SamundraGurung, P.Somasundram/ International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 3, May-Jun 2013, pp.315-326 319 | P a g e 𝐿 = 𝑉𝑎𝑛 +0.5∗𝑉𝑑𝑐 4∗𝑓𝑡∗𝜉 (30) Where, Van is the phase voltage, ft is the frequency of the carrier wave, 𝜉 is the amplitude of carrier wave. Taking, Van=230V, ft=20 KHz, L=7.25mH 3.3. Selection of wind turbine The wind turbine used for simulation purpose is taken from Simpower systems, Matlab Simulink which has maximum power coefficient cp=0.48 and tip speed ratio 𝜆=8.1. Turbine rating is taken as 5kW and radius can be found using 𝑃 = 1 2 ∗ 𝐶𝑝 ∗ 𝜋 ∗ 𝑅2 ∗ 𝜌 ∗ 𝑉3 (31) Where R= radius of the turbine, 𝜌=air density, v is wind velocity. R=2.3m Fig. 6. Turbine output characteristics 3.4 Tuning of PMSG converter The overall PMSG side with its controller can be can be modeled as [9] Fig. 7. Closed loop speed control of PMSG 𝐾𝑠 = 4 9∗𝐾𝑔∗𝑇𝑤𝑖 (32) 𝑇𝑠 = 6 ∗ 𝑇𝑤𝑖 (33) Root locus method is used to tune the PI controller where the design requirement taken are damping ratio, 𝜉=0.707, maximum overshoot, Mp = 2%, rise time, tr= 0.005s and settling time, ts= 0.01s. Fig. 8. Root locus plot of closed loop system Fig. 9.Step input response for given system
  • 6. SamundraGurung, P.Somasundram/ International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 3, May-Jun 2013, pp.315-326 320 | P a g e IV. RESULTS 4.1 Statcom as voltage regulator At 0.5s an IG is connectedthrough a circuit breakerin parallel with the Synchronous Generator as shown in Fig. 11.There is an injection of reactive power by the Statcom which quickly restores thedipping terminal voltage back to its rated value. 4.2 Statcom as frequency regulator As in Fig. 10.Initally as the total connected load is 12kW and Synchronous Generator produces around 15.4kW, remaining 3.4kW is consumed by the Battery leading to its charging. At 0.5s, Induction generator of 3.8kW is connected thus changing total generating power (SG and IG) to 19.2kW, thus causing a mismatch of 7.2kW. This power is again consumed by the battery. At 1s, an extra load of 12kW and 8kVAR is connected. This causes deficiency in the generating power of around 4kW which is supplied by the Statcom. Thus we can see asStatcom keeps the total generated and consumed power equal and thus the system frequency is kept at nominal value (50Hz). 4.3 Statcom as reactive power compensator In Fig. 11.at 1s, an extra load of 12kW and 9kVAR, considering power factor of 0.8 lagging is connected. Since the Statcom is designed to keep the supply side power factor as unity, its reactive power injection increases from 0 to 8kVAR. 4.4 Statcom as neutral current compensator At 1.5s, an unbalanced load of 6kW with two phase switched off is connected. Thus the load currents are highly unbalanced as shown in Fig. 11. However, the source currents are balanced as the Statcom provides a path for neutral current through its fourth leg. 4.5 Statcom as harmonic eliminator Fig. 12 shows connection of only nonlinear load. The nonlinear here considered is a three phase diode bridge rectifier with 50 ohms resistor. As we can notice, the currents are highly distorted but the source currents are linear. Fig. 13 and 14 shows the Total harmonic distortion (THD) values of load and source current.Load current have THD equal to 25% which is very high whereas source currents have their THD well within allowed level of 3%. 4.6 PMSG output Initially, wind velocity is at 8m/s as shown in Fig. 17 which gives reference speed of 34.11 rad/s for maximum power extraction. The electromagnetic torque developed is 45Nm and the generator output is 2kW. At 0.5s, wind velocity increases to 12m/s which correspond to reference speed of 51 rad/s. The electromagnetic torque developed is around 102Nm and the Power output is 4.7kW.
  • 7. SamundraGurung, P.Somasundram/ International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 3, May-Jun 2013, pp.315-326 321 | P a g e Fig. 10. Statcom as frequency regulator
  • 8. SamundraGurung, P.Somasundram/ International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 3, May-Jun 2013, pp.315-326 322 | P a g e Fig. 11. Statcom as voltage regulator Fig. 11. Statcom as voltage regulator
  • 9. SamundraGurung, P.Somasundram/ International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 3, May-Jun 2013, pp.315-326 323 | P a g e Fig. 12.Statcom as harmonic eliminator
  • 10. SamundraGurung, P.Somasundram/ International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 3, May-Jun 2013, pp.315-326 324 | P a g e Fig. 13. THD of source current Fig. 14. THD of source current Fig. 15. Speed of Induction Generator (pu) Fig. 16. Speed of Synchronous Generator (pu)
  • 11. SamundraGurung, P.Somasundram/ International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 3, May-Jun 2013, pp.315-326 325 | P a g e Fig. 17. Performance of PMSG converter
  • 12. SamundraGurung, P.Somasundram/ International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 3, May-Jun 2013, pp.315-326 326 | P a g e V. CONCLUSION The paper has divided its focus on mainly two renewable sources, uncontrolled Hydro turbine and variable Wind turbine. An Electronic load controller or a Statcom is used interchangeably because it functions both as voltage and frequency control. It is based on vector control scheme based on synchronously rotating dq referenceframe. A battery is connected on the dc side which is charged and discharged by the bidirectional activity of Statcom. This action helps to keep the frequency constant. Similarly, the battery is also charged from the output of PMSG converter. The Statcom also performs other functions like voltage regulation, harmonic elimination and neutral current compensation. The PMSG machine converter is employed for MPPT tracking. Thus an overall hydro and wind hybrid has been developed which can perform satisfactorily even in an isolated case. All these models are developed using Matlab,Simulink.This paper can be extended to more detailedBattery Energy Management system. It can also be extended by using Multi level Inverter for higher power ratings and lesser harmonic output. APPENDIX Synchronous Generator 16kVA, 400V, 1500rpm, Xd=1.734pu, Xd’=0.177puXd’’ = 0.111pu, Xq = 0.861pu , Xq’’=0.199pu,Xl=0.07pu,Td=0.018s,Td’’=0.0045s,T q’’=0.0045,Rs=0.02pu,H=0.5s,P=2 InductionGenerator 4kVA,400V,50Hz,Rs=0.03513pu,Lls=0.04586pu,Rr’ =0.03488pu,Llr’=0.04586pu,Lm=2.8pu,H=0.2s, Excitation capacitor=1.5kVAR Permanent Magnet Synchronous Generator Rs=0.085Ω,Ld=0.95mH,Lq=0.95mH, Flux linkage=0.192Vs, J=0.008kgm2 ,F=0.11Nms,P=8 Synchronous link reactor Rf=0.44Ω,Lf=7.25mH Statcom 40kVA Vdc=700V,Cdc=8000μF,Battery=700V,150AH PI controller Frequency controller, Kpf=9000,Kif=30000 Ac voltage controller, Kpv=0.02,Kiv=0.02 PMSG converter, Kpg=5, Kig=80 REFERENCES [1] I. Tamrakar, L.B. Shilpakar, B.G. Fernandes and R. Nilsen, Voltage and frequency control of parallel operated synchronous generator and induction generator with STATCOM in micro hydro scheme, IET Gener. Transm. Distrib, 1, (5), 2007, pp. 743–750 [2] J. A. Barrado, R. Griñó, H. Valderrama-Blavi, Power-QualityImprovement of a Stand- AloneInduction Generator Using a STATCOM With Battery Energy Storage System, IEEE transactions on power delivery, vol. 25, no. 4, 2010 , 2734- 2741 [3] Puneet K. Goel, Bhim Singh, S.S. Murthy, and Navin Kishore, Autonomous Hybrid System Using SCIG for Hydro Power Generation and Variable Speed PMSG for Wind Power Generation,IEEE International Conference on Power Electronics Drive Systems, 2009, 55-60 [4] S.-C.KuoL.Wang, Analysis of voltage control for a self-excited inductiongenerator using a current-controlled voltage sourceinverter (CC- VSl),IEE Proc.-Genes. Transni. Distrrb., Vol. 148, No. 5, 2001, 431-438 [5] PrabhaKundur, Power System Stability and Control(New Delhi: Tata McGraw-Hill Education, 2006) [6] Muhammad H. Rashid, Power electronics handbook (Burlington: Butterworth- Heinemann, 2011) [7] K. R. Padiyar, Facts controllers in power transmission and distribution (Daryaganj, New Delhi: New Age International (P) Ltd, 2007) [8] R. Krishnan,Electric Motor Drives: Modeling, Analysis and Control(New Delhi:PHI Learning, 2009).