07_chybrid systemhapter2
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CHAPTER 2
POWER CONVERTERS IN PV SYSTEM
2.1 INTRODUCTION
Photovoltaic system is gaining increased importance as a renewable
source because of its advantages such as the absence of fuel cost, little
maintenance and no noise and wear due to the absence of moving parts. But
there are still two principal barriers to the use of photovoltaic systems: the
high installation cost and the low energy conversion efficiency.
A PV panel is a non-linear power source, i.e., its output current and
voltage (power) depend on the terminal operating point. The maximum power
generated by the PV panel changes with the intensity of the solar radiation
and the operating temperature. To increase the ratio of output power/cost of
the installation, the PV panel should operate in the maximum output power
point.
The main focus of this research is to identify the proper DC-DC
converter which uses the adaptive perturbs and observe MPPT algorithm to
maximize energy extraction from the solar PV module and to increase the
conversion efficiency of MPPT system
2.2 CHARACTERISTICS OF SOLAR PV MODULE
Solar cells consist of a p-n junction fabricated in a thin layer of
semiconductor. The semiconductor electron can be located in either the
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valence band or conduction band. Initially, all the electrons in the
semiconductor fill up the valence band but when sunlight hits the
semiconductor, some electrons acquire enough energy to move from the
valence band to the conduction band. The electrons in the conduction band,
then, begin to move freely creating electricity. The electron leaving the
valence band leaves a positively charged hole behind and now the valence
band is no longer full; it aids the current flow. Most solar cells are doped to
reduce the energy required for the electron to move from the valence band to
the conduction band.
The amount of energy from sunlight that is absorbed by a solar cell
determines its efficiency. This energy is called photon and it can be reflected,
absorbed or it can pass through a semiconductor. Since only the photons that
are absorbed contribute to the electrical energy, it is important to reduce the
percentage of photons that pass through and are reflected. An anti-reflective
coating is usually applied to the surface of the solar cell to decrease the
number of photons that are reflected. This reduces the percentage of photons
reflected but some photons are still able to pass right through the
semiconductor material.
There are several approaches to manufacturing solar cells,
including the kind of semiconductor used and the crystal structure employed,
with each different factor affecting the efficiency and cost of the cell. Other
external factors such as the ambient weather conditions like temperature,
illumination, shading, etc., also affect the solar panels output. The aim is to
design a system that will extract the most possible power regardless of
ambient weather conditions or solar cell efficiency.
Irradiance is a characteristic related to the amount of sun energy
reaching the ground, and under ideal conditions it is measured as 1000 W/m2
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at the equator. The sun energy around the earth is highest around the equator
when the sun is directly overhead. Some important magnitudes related to
irradiance include the spectral irradiance, irradiance, and radiation. Spectral
irradiance is the power received by a unit surface area at a particular
wavelength, while irradiance is the integral of the spectral irradiance extended
to all wavelengths of interest. Radiation is the time integral of the irradiance
extended over a given period of time.
In designing PV systems, the main concern is the radiation received
from the sun at a particular location at a given inclination angle and
orientation and for long periods of time. Since solar radiation is the energy
resource of the solar panel, the output of the panel is significantly affected by
changing irradiance. The I-V characteristic of a solar cell including the effects
of irradiance is shown in Figure 2.1.
Figure 2.1 I-V Characteristics of a solar PV module for change in
irradiation
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The irradiance at any location is strongly dependent on the
orientation and inclination angles of the solar panel. Orientation is usually
measured relative to the south in northern latitudes while it is measured
relative to the north in southern latitudes. On the other hand, the inclination
angle is measured relative to the horizontal. Using these two parameters, the
irradiation at any location can be determined.
The output power is directly proportional to the irradiance. As such,
a smaller irradiance will result in reduced power output from the solar panel.
However, it is also observed that only the output current is affected by the
irradiance.
Although irradiance is an important factor in determining the I-V
characteristic of a solar panel, it is not the only factor. Temperature also plays
an important role in predicting the I-V characteristic, and the effects of both
factors have to be considered when designing a PV system. Whereas the
irradiance mainly affects the output current, the temperature mainly affects
the terminal voltage. A plot of I-V characteristic with varying temperature is
shown in Figure 2.2.
Figure 2.2 Effects of temperature on I-V curve
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It is observed from Figure 2.2 that the terminal voltage increases
with decreasing temperature. This is somewhat surprising as one would
typically expect the solar panel to operate more efficiently as temperature
increases. However, one of the reasons the solar panel operates more
efficiently with decreasing temperature is due to the electron and hole
mobility of the semiconductor material. As temperature increases, the electron
and hole mobility in the semiconductor material decrease significantly. The
electron mobility for Silicon at 25 C is about 1700cm2/Volt-sec and will
decrease to about a fourth of this value as temperature increases to 225 C,
and likewise the hole mobility decreases from about 600cm2/Volt-sec at 25 C
to 200cm2/Volt-sec as temperature increases to 225 C. While the higher
reference temperatures are not realistic operating conditions for a solar panel,
it does show that electron and hole mobility decrease with increasing
temperature.
It should be noted here that irradiance and temperature represent
only two of the most significant external factors that affect the efficiency of a
solar cell; inclination, location, and time of the year are also factors that affect
the efficiency of solar cells. Additional parameters of a solar cell can be discussed
by an illustration of the maximum power point as shown in Figure.2.3
Figure 2.3 Illustration of maximum power point
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The cells short circuit current intersects the Y-axis at point B and
the open circuit voltage intersects the X-axis at point C. To achieve maximum
energy transfer, systems powered by solar cells should be designed to transfer
energy to the load at point A on the I-V curve. No energy should be delivered
at points B and C, and most of the energy should be delivered as the operating
point approaches point A. In a solar panel array, it is even more important that
load impedance and source impedance are well matched. Once the cells are
matched by their I-V characteristics, they can be grouped into individual
arrays and each array is then made to operate at its maximum energy transfer
point. Majority of solar cells have high capacitance associated with their
forward biased p-n junctions because the charged carriers are much closer
together. The unwanted capacitance increases as the size of the solar cell and
junction area increases. The I-V curve of the solar cell can be determined by
taking fast I-V measurements which is done by applying a constant voltage
and measuring the resulting current for the device being tested. However, the
high capacitance makes it difficult to get fast I-V measurements.
2.2.1 Modelling of Solar PV Module
A simplified equivalent circuit of a solar cell consists of a diode
and a current source which are switched in parallel. The photocurrent
generated when the sunlight hits the solar panels can be represented with a
current source and the p-n transition area of the solar cell can be represented
with a diode. The voltage and current relationship of the simplified solar cell
can be derived from Kirchhoffs current law. This simplified equivalent
circuit, however, does not give an accurate representation of the electrical
process at the solar cell. On real solar cells, voltage losses occur at the
boundary and external contacts and leakage currents occur throughout the
cell; these losses can be represented with a series resistance Rs
and a parallel
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resistance Rp, respectively. The equivalent circuit of the solar cell showing the
series and parallel resistance is shown in Figure 2.4.
Figure 2.4 Equivalent circuit of a solar PV module
For Figure.2.4, the current Equation is given by
Isc = ID +Ipv + (VD / R p) (2.1)
Vpv=VD - (Ipv*Rs) (2.2)
where diode current is, ID = Io + ( e (VD / VT) - 1), Isc is the short circuit current,
Vt = NsKT / q is the thermal voltage with Ns cells connected in a series (K is
the Boltzmann constant, q is the electron charge and T is the temperature of
the PV cells). The short circuit current is directly proportional to the
irradiation and slightly proportional to the level of the cell temperature.
Using Equations 2.1 and 2.2, the solar PV module is modeled in
MATLAB/Simulink as shown in Figure 2.6 and used to enhance the
understanding and predict the I-V and P-V characteristics and to analyze the
effect of temperature and irradiation variation. If irradiance increases, the
fluctuation of the open-circuit voltage is very small. But the short circuit
current has sharp fluctuations with respect to irradiance. However, for a rising
operating temperature, the open-circuit voltage is decreased in a non-linear
fashion.
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The P-V and I-V characteristics are validated in MATLAB
software for the L1235-37Wp (Watt peak) solar module. Table 2.1 shows the
technical specification of L1235-37Wp solar panel under test which is shown
in Figure 2.5. The I-V characteristic is obtained based on experimental results
under irradiation =1000 W/m2, temperature =25 C
Figure 2.5 L1235-37Wp solar module under test
The simulated I-V and P-V characteristics of solar module L1235-37Wp are
shown in Figure 2.7 and 2.8.
Table 2.1 Specification of a solar PV module under test
Parameter Values Open circuit voltage (Voc) 21V Short circuit current (Isc) 2.5A Voltage at MPP (Vmax) 16.4VCurrent at MPP (Imax) 2.25APower rating (Pmax) 37WMaximum system voltage 600V Module efficiency (%) 10.82%Size (mm) 645*530*16Weight (kg) 4
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Figure 2.6 MATLAB model for PV module
Figure 2.7 I-V Characteristics of solar PV module
Figure 2.8 P-V Characteristics of solar PV module
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2.3 MPPT METHODS
The efficiency of energy conversion depends mainly on the
efficiency of the PV panels that generate the power. Weather conditions also
influence the efficiency, which depends non-linearly on the irradiation level
and temperature. When a PV array is directly connected to a load, the
systems operating point will be at the intersection of the IV curves of the
PV panel and load. The non-linear variations in the output voltage and
current, which depend on solar-radiation levels, operating temperature and
load current, can cause a low electrical efficiency. To solve these problems
with the utilization of solar arrays for electrical power, the MPP of the PV
system (at given conditions) is tracked using offline or online algorithms,
where the system operating point is forced towards optimal conditions. The
PV array has an optimum operating point called the MPP, which is never
constant over time and varies depending on cell temperature and the present
irradiation level.
To obtain the maximum power from a PV array, an MPPT is
applied. The location of the MPP in the IV plane is not known in prior. It
can be calculated using a model of the PV array and measurements of
irradiance and array temperature, but making such measurements is usually
too expensive for this application, and often the required parameters for the
PV array model are not known adequately. Thus, the MPPT must
continuously search for the MPP of the solar PV module. Many techniques
for MPPT of solar PV have been proposed to track maximum power from
solar PV module. Some important useful techniques such as as hill climbing
/ Perturb And Observe (PAO), Incremental Conductance (IncCond), fractional
open-circuit voltage, fractional short-circuit current, fuzzy logic control,
neural network, and Ripple Correlation Control (RCC) are discussed briefly
in the following section.
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2.3.1 Hill Climping / PAO
Hill climbing involves a perturbation in the duty ratio of the power
converter, and PAO involves a perturbation in the operating voltage of the PV
array. In the case of a PV array connected to a power converter, perturbing the
duty ratio of power converter perturbs the PV array current and consequently
perturbs the PV array voltage. Hill climbing and PAO methods are different
ways to envision the same fundamental method.
Incrementing (or decrementing) the voltage increases (or decreases)
the power when operating on the left of the MPP and decreases (or increases)
the power when on the right of the MPP. Therefore, if there is an increase in
power, the subsequent perturbation should be kept the same to reach the MPP
and if there is a decrease in power, the perturbation should be reversed.
The process is repeated periodically until the MPP is reached. The
system then oscillates about the MPP. The oscillation can be minimized by
reducing the perturbation step size. However, a smaller perturbation size
slows down the MPPT. Hill climbing and PAO methods can fail under rapidly
changing atmospheric conditions. Two sensors are usually required to
measure the PV array voltage and current from which power is computed.
Two sensors are usually required to measure the PV array voltage and current
from which power is computed.
2.3.2 Incremental Conductance
The incremental conductance MPPT method implemented based on
the fact that the slope of the PV array power curve is zero at the MPP,
positive on the left of the MPP, and negative on the right.
= 0 at MPP (2.3)
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> 0 left of MPP (2.4)
< 0 right of MPP (2.5)
Also the change in current to change in voltage is related to track
maximum power.
I/ V = I/V, at MPP (2.6)
I/ V > I/V, left of MPP (2.7)
I/ V < I/V, right of MPP (2.8)
The maximum power is extracted from the solar PV module by
comparing the instantaneous conductance (I/V) to the incremental
conductance ( I/ V). Vref is the reference voltage at which the PV array is
forced to operate. At the MPP, Vref equals VMPP. Once the MPP is reached,
the operation of the PV array is maintained at this point unless a change in I
is noted, indicating a change in atmospheric conditions and the MPP. The
algorithm decrements or increments Vref to track the new MPP. The increment
size determines how fast the MPP is tracked. Fast tracking can be achieved
with bigger increments but the system might not operate exactly at the MPP.
By proper control of the power converter, the initial operating point is set to
match a load resistance proportional to the ratio of the open-circuit voltage
(VOC) to the short-circuit current (ISC) of the PV array.
In order to implement incremental conductance algorithm,
measurements of the instantaneous PV array voltage and current require two
sensors. IncCond method lends itself well to DSP and microcontroller control,
which can easily keep track of previous values of voltage and current and
make all the decisions.
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2.3.3 Fractional Open-Circuit Voltage
The near linear relationship between Vm and VOC of the PV array,
under varying irradiance and temperature levels, has given rise to the
fractional VOC method.
Vm R1VOC ` (2.9)
Where R1 is a constant of proportionality. Since R1 is dependent on
the characteristics of the PV array being used, it usually has to be computed
beforehand by empirically determining Vm and VOC for the specific PV array
at different irradiance and temperature levels. The factor R1 has been reported
to be between 0.71 and 0.78. Once R1 is known, Vm can be computed with
VOC measured periodically by momentarily shutting down the power
converter. However, this incurs some disadvantages, including temporary loss
of power. Once Vm has been approximated, a closed-loop control on the array
power converter can be used to asymptotically reach this desired voltage. The
PV array technically never operates at the MPP. Depending on the application
of the PV system, this can sometimes be adequate. Even if fractional VOC is
not a true MPPT technique, it is very easy and cheap to implement as it does
not necessarily require DSP or micro-controller control. The selection of the
value of R1 is no more valid if the solar module is partial shading (which
causes multiple local maxima) which proposes sweeping the PV array voltage
to update R1. This obviously adds to the implementation complexity and
incurs more power loss.
2.3.4 Fractional Short-Circuit Current
Fractional is used to track maximum power from solar PV module.
Under varying atmospheric conditions, Im is approximately linearly related to
the ISC of the PV array
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Im R2Isc (2.10)
where R2 is proportionality constant. Just like in the fractional VOC technique,
R2 has to be determined according to the PV array in use. The constant R2 is
generally found to be between 0.78 and 0.92.
Measuring ISC during operation is problematic. An additional
switch usually has to be added to the power converter to periodically short the
PV array so that ISC can be measured using a current sensor. This increases
the number of components and cost. Power output is not only reduced when
finding ISC but also because the MPP is never perfectly matched. To track
maximum power using this MPPT in the presence of multiple local maxima,
periodically sweeps the PV array voltage from open-circuit to short-circuit
which is required to update R2.
2.3.5 Ripple Correlation Control
Ripple Correlation Control (RCC) makes use of ripple to perform
MPPT. RCC correlates the time derivative of the time-varying PV array
power (p) with the time derivative of the time-varying PV array current or voltage v to drive the power gradient to zero, thus reaching the MPP.
if v or i is increasing (v > 0 or > 0) and p is increasing (P > 0), then the operating point is below the MPP (V Vm or I > Im). Combining these observations, we
see that P v or P are positive to the left of the MPP, negative to right of the MPP, and zero at the MPP. Simple and inexpensive analog circuits can be
used to implement RCC.
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Another advantage of RCC is that it does not require any prior
information about the PV array characteristics.
The derivatives are usually undesirable, but AC-coupled
measurements of the PV array current and voltage can be used instead since
they contain the necessary phase information. The derivatives can also be
approximated by high-pass filters with cutoff frequency higher than the ripple
frequency. A different and easy way of obtaining the current derivative is to
sense the inductor voltage, which is proportional to the current derivative
2.3.6 Fuzzy Logic Control
Fuzzy logic control has the advantages of working with imprecise
inputs, not needing an accurate mathematical model, and handling nonlinearity.
Fuzzy logic control generally consists of three stages: fuzzification, rule base table
lookup, and defuzzification. During fuzzification, numerical input variables are
converted into linguistic variables based on a membership function.
In this case, five fuzzy levels are used: NB (negative big), NS
(negative small), ZE (zero), PS (positive small), and PB (positive big). Seven
fuzzy levels are used, probably for more accuracy. The inputs to an MPPT
fuzzy logic controller are usually an error E and a change in error E. The
user has the flexibility of choosing how to compute E and E.
E(n) = ( ) ( )( ) ( ) (2.11) E(n) = E(n) E(n 1) (2.12)
Once E and E are calculated and converted to the linguistic
variables, the fuzzy logic controller output, which is typically a change in
duty ratio D of the power converter, can be looked up in a rule base table.
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In the defuzzification stage, the fuzzy logic controller output is
converted from a linguistic variable to a numerical variable still using a
membership function. MPPT fuzzy logic controllers have been shown to
perform well under varying atmospheric conditions to track maximum power.
2.3.7 Neural Network
The maximum power is tracked from the solar PV module using
neural network. Neural networks commonly have three layers: input, hidden,
and output layers. The number of nodes in each layer varies and they are user-
dependent. The input variables can be PV array parameters like Voc and Isc,
atmospheric data like irradiance and temperature, or any combination of
these. The output is usually one or several reference signal(s) like a duty cycle
signal used to drive the power converter to operate at or close to the MPP.
How close the operating point gets to the MPP depends on the algorithms
used by the hidden layer and how well the neural network has been trained.
The links between the nodes are all weighted. Also the PV arrays have
different characteristics. A neural network has to be specifically trained for
the PV array with which it will be used. The characteristics of a PV array also
change with time, implying that the neural network has to be periodically
trained to guarantee accurate MPPT.
2.4 APPLICATION-BASED SELECTION OF MPPT
ALGORITHM
An MPPT method that has quick response characteristics and is
able to make good use of the electrical power generated under any weather
condition is needed to optimize the system management. Many MPPT control
methods have been proposed that search for the maximum operating
conditions from the output power and voltage characteristics of solar arrays
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using differential techniques, like the hill-climbing method or fuzzy rules. The
main aspects for selection of the MPPT techniques are essentially:
The ease of implementation is an important factor in deciding
which MPPT technique to use. Some techniques require
analogue circuitry and others digital circuitry, even if that may
require the use of software and programming
The number of sensors required to implement MPPT also
affects the selection process. It is easier and more reliable to
measure voltage than current. Moreover, current sensors are
usually expensive and bulky. It is also uncommon to find
sensors that measure irradiance levels, as needed in the linear
current controls and the maximum power point current
(IMPP) and maximum power point voltage (VMPP)
computation methods
The occurrence of multiple local maxima due to partial
shading of the PV array can be a real hindrance to the proper
functioning of an MPP tracker. Considerable power loss can
be incurred if a local maximum is tracked instead of the real
MPP;
It is hard to mention the monetary costs of every single MPPT
technique unless it is built and implemented. A good cost
comparison can be made by knowing whether the technique is
analogue or digital, whether it requires software and
programming, and the number of sensors. Analogue
implementation is generally cheaper than digital, which
normally involves a microcontroller that needs to be
programmed;
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Different MPPT techniques will suit different applications. For
example, in space satellites and orbital stations that involve a large amount of
money, the costs and complexity of the MPP tracker are not as important as
its performance and reliability. The tracker should be able to continuously
track the true MPP in minimum amount of time and should not require
periodic tuning. In this case, hill climbing/PAO, IncCond, and RCC are
appropriate. Solar vehicles would mostly require fast convergence to the
MPP. Fuzzy logic control, neural network, and RCC are good options in this
case. Since the load in solar vehicles consists mainly of batteries, load current
or voltage maximization should also be considered. The goal, when using PV
arrays in residential areas, is to minimize the payback time and to do so, it is
essential to constantly and quickly track the MPP. Since partial shading (from
trees and other buildings) can be an issue, the MPPT should be capable of
bypassing multiple local maxima. Therefore, the two-stage IncCond and the
current sweep methods are suitable. Since a residential system might also
include an inverter, the open circuit voltage MPPT can also be used. PV
systems used for street lighting only consist of charging up batteries during
the day. They do not necessarily need tight constraints; easy and cheap
implementation might be more important, making fractional VOC or ISC viable.
The method considered in this research work is a PAO method.
This method is widely diffused because of its low-cost and ease of
implementation. When atmospheric conditions are constant or change slowly,
the PAO method oscillates close to MPP. However, when these change
rapidly, this method fails to track MPP and gives rise to a waste of part of the
available energy.
The main limitation of this kind of algorithm is connected with the
opposite exigencies required by the fast dynamic response and the steady-
state stability. Indeed, to improve the dynamic performance it is necessary to
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use a large perturbation value, whereas a smaller value is necessary to ensure
good stability. During cloudy days, the solar irradiation can vary many times
and quickly. Because of this, so as not to lose great quantities of energy, it is
necessary to achieve a good dynamic response for the system. The basic
principle of the algorithm proposed is to adapt the perturbation amplitude to
the actual operating conditions. In particular, far from the MPP, large
perturbation amplitudes are chosen, whereas small ones are used in proximity
to the maximum. It is therefore necessary to have knowledge of the maximum
position. However, a perfect knowledge is not required because working at
the real maximum is ensured by the PAO technique. An adaptive PAO
method is discussed and implemented in this research. It has faster dynamics
and improved stability compared to the traditional PAO.
2.5 ADAPTIVE PERTURB AND OBSERVER MPPT
In the PAO algorithm, the operating voltage of the PV array is perturbed by a small increment, and the resulting change in power, P, is measured. If P is positive, the perturbation of the operating voltage moves the PV arrays operating point closer to the MPP. Thus, further voltage perturbations in the same direction (that is, with the same algebraic sign) should move the operating point towards the MPP. If P is negative, the system operating point moves from the MPP, and the algebraic sign of the perturbation should be reversed towards the MPP. Though PAO algorithm is simple and easy to implement, it fails when the atmospheric conditions change rapidly. To overcome this problem, the adaptive PAO algorithm improves the dynamic response without affecting stability. In this algorithm, high perturbation is selected when the operating point is far away from MPP and low perturbation is selected when the operating point is closer to MPP. The adaptive PAO algorithm has been implemented in ATMEGA16 micro-controller to generate gate pulse which can be given to the switches of DC-DC converter.
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The flow chart of the adaptive perturbs and observer MPPT algorithm is illustrated in Figure 2.9. The parameter K is the step given to the PWM signal. This parameter can vary depending on the working point of th e DC-DC converter. To get a faster convergence, high value of K is selected to avoid big oscillations near to the MPPT. The PAO MPPT control algorithm is implemented in a micro-controller (ATMEGA16) that has ten 10-bits analogue-to-digital converter (ADC) and two fast PWM mode signals with 10-bits of resolution. The control circuit compares the PV output power before and after a change in the duty-cycle of the DC-DC converter control signal and acts in conformity. The PWM_old is the sample of the PWM signal in the previous iteration of the algorithm and PPV is the variation of the delivered power to the load.
Figure 2.9 Flow chart of Adaptive perturb and observer algorithm
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2.6 DIRECT CONTROL METHOD
Conventional MPPT systems have two independent control loops to
control MPPT. The first control loop contains the MPPT algorithm and the
second one is usually a Proportional Integral (PI) controller. Perturb and
observer algorithm is used to generate an error signal which is zero at MPP;
however, it is not zero at most of the operating points under rapid change in
atmospheric conditions. The main purpose of the second control loop is to
make the error from the MPPs near to zero. Simplicity of operation, ease of
design, inexpensive maintenance and low cost made PI controllers very
popular in most linear systems. However, MPPT system of standalone
photovoltaic in space applications is a non-linear control problem due to the
non-linearity nature of PV and unpredictable environmental conditions and,
hence, PI controllers do not generally work well.
The research work discusses direct control adaptive perturb and
observer algorithm. The PI control loop is eliminated and duty cycle is
adjusted directly in the algorithm using ATMEGA16 micro-controller. The
control loop is simplified and the computational time for tuning controller
gains is eliminated. To compensate for the lack of PI controller in the
proposed system, a small marginal error of 0.002 was allowed. The objective
of this work is to eliminate the second control loop and to show that
sophisticated MPPT methods do not necessarily obtain the best results but
employing them in a simple manner for complicated electronic subjects is
considered necessary. Feasibility of the proposed system is investigated with
a DC-DC Cuk converter which is configured as the MPPT.
2.7 DC-DC CONVERTERS IN A SOLAR PV SYSTEM
PV interfacing is a challenging task and there is a need for
clarification of the existing DC-DC converter topologies used in the PV
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applications. DC-DC converter shown in Figure 2.10 is an essential element
in the MPPT process and this process can be performed either by controlling
the input current or voltage of the interfacing converter. Also it is known that
DC-DC converters increase or decrease the magnitude of the DC-voltage
and/or invert its polarity. This is accomplished by the pulse width modulation
technique, usually to a constant frequency. The duty cycle (d) is the ratio of
the time of conduction (TON) to the switching period (Ts). The three basic
configurations of converters (buck, boost and buckboost derived) are similar
to a DC transformer, both in continuous conduction mode (CCM) and
discontinuous conduction mode (DCM). In a DC transformer, the relationship
of transformation can be controlled electronically by changing the duty cycle
of the converter from the range 0 to 1.
The power electronics interface is connected between a solar panel
and a load or battery bus is a pulse width modulated DC-DC converter or their
derived circuits operating in Discontinuous Inductor Current Mode (DICM) or
Discontinuous Capacitor Voltage Mode (DCVM) is used to extract maximum
power from solar PV panel. The DCDC converter has the input resistance
characteristics being proportional or inversely proportional to the switching
frequency. Hence, by adjusting the nominal duty cycle of the main switch of DC-
DC converter, the input resistance can be made equal to the equivalent output
resistance of the solar PV panel and ensures the maximum power transfer.
Figure 2.10 MPPT process using DC-DC converter
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The input voltage and the equivalent input resistance of the DC-DC
converter are V and R , respectively. As the input power Pi to the converter is equal to the output power Po of the solar panel,
Pi =Po = (2.13)
The rate of change Pi with respect to V and R can be shown p = V - R (2.14)
At the MPP, the rate of change of Pi equals zero and R = Reqp =0, hence = (2.15)
The Equation gives the required dynamic resistance characteristics
of the tracker at MPP.
Resistor emulation techniques have been used previously, most
commonly in Power Factor Correction (PFC) applications. Some approaches
for PFC are based on converters with natural resistor emulation at the input
port (without current feedback), including boost type converters in critical
conduction mode and buckboost-type converters in DCM. At higher current
levels, most PFC circuits operate in CCM with more advanced current and
voltage feedback control.
The natural emulation techniques and approximations to them are
used in this work to achieve resistor emulation and characterize current
voltage curves of PV modules using open loop control circuitry. The
relationships among the input resistance (Ri, the emulated resistance at the
output terminals of the PV module), equivalent inductance (Leq), and load (R)
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connected to the converter for CCM and DCM are to be analyzed for all the
conventional DC-DC converters. These relationships have been obtained by
assuming converters without losses and with small switching ripple compared
with their respective DC components. In each case, the dimensionless
parameter K is a measure of the tendency of a converter to operate in DCM.
Large values of K lead to CCM, whereas small values lead to DCM. The
critical value of K at the boundary between modes (Kcrit) is a function of the
duty cycle. If K is greater than one, then the converter operates in CCM for all
duty cycles. Usually, the mode boundary is given in terms of the load
resistance R rather than the dimensionless parameter K. The various
conventional DC-DC converters are discussed and their suitability to solar PV
power conditioning process is analyzed in the below section.
2.7.1 Buck Converter
The basic circuit configuration used in the buck converter is shown
in Figure 2.11. There are only four main components: switching power
MOSFET S, flywheel diode, inductor L, and output filter capacitor C. When S
is turned on, current begins flowing from the input source through S and L,
and then into C and the load R. The magnetic field in L, therefore, builds up,
storing energy in the inductor,with the voltage drop across L opposing or
bucking part of the input voltage. Then when S is turned off, the inductor
opposes any drop in current by suddenly reversing its Electromotive Force
(EMF), and now supplies current to the load itself via D. Without going too
deeply into its operation, the DC output voltage which appears across the load
is a fraction of the input voltage, and this fraction turns out to be equal to the
duty cycle.
= d (2.16)
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where d is the duty cycle, and equal to Ton/Ts. So by varying the switching
duty cycle, the buck converter output voltage can be varied as a fraction of the
input voltage.
Figure 2.11 Buck converter
For the buck converter, the input resistance Ri (Continuous
conduction mode) must have a value in the interval Ri (CCM) [R, )] and Riis equal to R/d2 and the input resistance Ri (Discontinuous conduction mode)
must have a value in the range
Ri = ( ( R/4)*(1+ (1 + 4 K ) )^2 , ) (2.17)where R is the load resistance and K = 2 L / R Ts
According to this expression, a buck converter cannot emulate
smaller impedances than the load impedance, and therefore, it does not reach
values near the short-circuit current of the PV module when it is used to
obtain I-V curves. Hence, it is concluded that buck converter is not useful in
MPP tracking process of a solar PV powered system.
2.7.2 Boost Converter
The basic circuit configuration used in the boost converter is shown
in Figure.2.12. When S is switched on, current flows from the input source
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through L and S, and energy is stored in the inductors magnetic field. There
is no current through diode D, and the load current is supplied by the charge
in C. Then when S is turned off, L opposes any drop in current by
immediately reversing its EMF. So that the inductor voltage adds to the
source voltage and current due to this boosted voltage now flows from the
source through L, D and the load, recharging C as well. The output voltage is,
therefore, higher than the input voltage, and it turns out that the voltage step-
up ratio is equal to:
= (2.18)
Figure2.12 Boost converter
The input resistance Ri (CCM) of the boost converter is equal to
R*(1-d) 2 and Ri (DCM) is equal to ( )^ . This expression indicates that a boost converter cannot emulate impedances greater than the impedance
of load, and, therefore, it does not reach values near the open circuit voltage
of the PV module. Hence, it is observed that boost converter may not be
useful for PV applications.
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2.7.3 Buck- Boost Converter (Single Inductor)
The basic circuit configuration used in the buck-boost converter is
shown in Figure 2.13. When MOSFET S is turned on, inductor L is connected
directly across the source voltage and current flows through it, storing energy
in the magnetic field. No current can flow through the load since during the
on- time of the switch S, the diode is connected and it is reverse biased.
Capacitor C must supply the load current in this Ton time of the switch. But
when S is turned off, L is disconnected from the source. The inductor L
opposes any tendency for the current to drop, and instantly reverses its EMF.
This generates a voltage which forward biases D, and current flows into the
load and to recharge C. The ratio between the output and input voltages is
given by
= (2.19)
The output voltage is always reversed in polarity with respect to the
input. So the buck-boost converter is also a voltage inverter.
Figure 2.13 Buck-Boost converter
The input resistance Ri during the continuous conduction mode is
given by
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R i (CCM) [0, ]
Ri (CCM) = ( )
(2.20)
The input resistance Ri during the discontinuous conduction mode
is given by
Ri (DCM) = (2.21)
Therefore, the buck-boost converter is capable of sweeping the
whole I-V curve of a PV module in CCM from open circuit voltage (Voc) to
short circuit current (Isc) condition. The buck-boost converter has the
advantage of true resistance emulation. As a result, the I-V characteristic
curve of solar PV module can be covered and measured quickly (in ms) to
have a reliable real-time measure of their evolution. But the buck-boost
converter has discontinuous input current characteristics because the switch S
is placed in a series with the panel causing high harmonic distortion in
current and hence high input ripples and noise were present. So the buck
boost converter with single inductor may not be a suitable converter in MPP
tracking processes.
2.7.4 SEPIC Converter
In a Single Ended Primary Inductor Converter (SEPIC) converter,
the output voltage can be higher or lower than the input voltage. Unlike the
buck-boost, the output is not inverted. The SEPIC converter shown in
Figure 2.14 uses two inductors, L1 and L2. The capacitor C1 isolates the input
from the output and provides protection against a shorted load when the
switch S is turned on. The first inductor, L1, is charged from the input voltage
source during this time. The second inductor takes energy from the first
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capacitor, and the output capacitor is left to provide the load current. The fact
is that both L1 and L2 are disconnected from the load when the switch is on.
When the power switch is turned off, the first inductor charges the capacitor
C1 and also provides current to the load. The second inductor is also
connected to the load during this time. The output capacitor sees a pulse of
current during the off time, making it inherently noisier than a buck converter.
The relation between input and output currents and voltage is given
by
= ( ) (2.22) = ( ) (2.23)
The input current is non-pulsating. In SEPIC converter, link-
capacitor (C1) voltage must follow the input voltage, and this means that the
capacitor size can be smaller. So the SEPIC converter is suitable in MPP
tracking process.
Figure 2.14 SEPIC converter
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2.7.5 Cuk Converter
The basic circuit configuration used in Cuk converter is shown in
Figure 2.15. Cuk converter has two modes of operation. The first mode of
operation is when the switch (MOSFET) is closed (ON) and it is conducting
as a short circuit as shown in Figure 2.16. In this mode, the current through
inductor L1 rises. At the same time, the voltage of capacitor C1 reverse biases
the diode D and turns it off. The capacitor (C1) releases its stored energy to
the load. The second operating mode is when the switch (S) is open (OFF),
diode (D) is forward biased and conducting energy to the output as shown in
Figure 2.17. Capacitor C1 is charging from input supply and the energy stored
in the inductor L2 is transferred to the load. The diode D and switch (S)
provide a synchronous switching action
The relation between input and output currents and voltage is
given by
( ) (2.24) ( ) (2.25)
Figure 2.15 Cuk converter
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Figure 2.16 Mode 1: Switch S is ON
Figure2.17 Mode 2: switch S is OFF
The input resistance of Cuk converter Ri during the continuous
conduction mode is given by
R i (CCM) [0, ]
Ri (CCM) = (2.26)
where Leq = L1 // L2 and fs switching frequency
The input resistance Ri during the discontinuous conduction mode
is given by
Ri (DCM) = (2.27)
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Therefore, the Cuk converter is capable of sweeping the whole I-V
curve of a solar PV module in CCM from open circuit voltage (Voc) to short
circuit current (Isc) condition.
Due to the input and output inductor in Cuk converter, the input
current is non-pulsating. Therefore, the sweep of the I-V curve is carried out
in a more reliable and less noisy way. So Cuk converter is more suitable in
MPP tracking circuits. The Cuk converter is preferred in power conditioning
process of solar PV system since Cuk converter works based on the energy
transfer of the capacitor and hence less EMI
2.8 CONCLUSION
This chapter explained the operating characteristics of solar PV
module, modelling of solar PV in MATLAB/Simulink and provided an
overview of various MPP algorithms used for maximum power tracking. This
study dealt with general ways to select MPP algorithms based on the solar PV
application. This chapter also explained the detailed analysis of MPP tracking
process using various DC-DC converters used for PV application and
concluded that DC-DC Cuk converter is a good choice to be used in MPP
tracking process in solar PV powered system.