Jan Hendrik Carstens, Clemens Gühmann
Maximum power point controller for
thermoelectric generators to support a
vehicle power supply
Article, Postprint version
This version is available at https://depositonce.tu-berlin.de/.
Suggested Citation
Carstens, Jan Hendrik; Gühmann, Clemens: Maximum power point controller for thermoelectric
generators to support a vehicle power supply. - Materials today : roceedings. - ISSN: 2214-7853. - 2
(2015), 2. - pp. 790–803. - DOI:10.1016/j.matpr.2015.05.099. (Postprint version is cited, page numbers
differ.)
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Maximum Power Point Controller for Thermoelectric Generators to
Support a Vehicle Power Supply
Jan Hendrik Carstensa,* , Clemens Gühmanna
aDepartment of Energy and Automation Technology, Chair of Electronic Measurement and Diagnostic Technology, TU Berlin, Einsteinufer 17,
10587, Berlin, Germany
Abstract
The growing mobility increases the world-wide fuel consumption. Yet the amount of fossil fuel is limited and the environmental
burden is increasing dramatically as well. Many governments have enacted laws to regulate and reduce the fuel consumption as
well as the CO2 emissions of combustion engines. An idea to save fuel and to reduce the environmental burden is to use
thermoelectric generators (TEGs) to recover the waste heat of the exhaust gas and convert into electric energy in automotive
applications. For the linking of TEGs to the vehicle is power supply, a DC-DC converter can be used. To support a wide range of
TEGs with different electric parameters, the control of DC-DC converter must be robust. Further, the control should track the
maximum power point (MPP) of the TEG for an efficient power recovery. This paper presents a digital cascade controller for a
boost-buck converter that charges a vehicle battery and supplies the load. To model and analyze the discontinuous converter, the
state-space-averaging (SSA) is used. The tracking of the MPP is realized with a gradient algorithm and an input current control.
An adaptive step size algorithm reduces the conversion time of the maximum power point tracking algorithm (MPPT).
Experiments verified the controller design and the efficiency of the MPPT.
Keywords: DC-DC converter; Maximum Power Point Tracking; Thermoelectric Generator; Digital Control
Nomenclature
r
A
area
BA,
control plant polynomials
C
controller
G
control plant
TSR ,,
controller polynomials
N
number of modules
P
power
S
switch
ch
T,
temperature at hot-side, cold-side
d
duty cycle
m
g
gain margin
i
current
* Corresponding author. Tel.: +49-30 314-21168; fax: +49-30 314-22120.
E-mail address: jan.h.carstens@tu-berlin.de
First publication, doi: 10.1016/j.matpr.2015.05.099 by Elsevier, in Materials Today: Proceedings
© 2016. This manuscript version is made available under the CC-BY-NC-ND 4.0 license http://creativecommons.org/licenses/by-nc-nd/4.0/.
2
l
length
u
voltage
s
f
switching frequency
r
α
temperature coefficient
εγδβα
,,,,
parameters
m
ϕ
phase margin
ρ
Seebeck coefficient
σ
electrical conductance
1. Introduction
Today, mobility increases world-wide and is accompanied by a rising fuel consumption. This trend is in conflict with
the limitation of fossil fuels. Additionally, the environmental burden is increasing dramatically. In consequence,
many governments have enacted laws to reduce the CO2 emissions of combustion engines. The resulting
requirements represent a formidable challenge for research and development. Conventional internal combustion
engines (ICEs) convert chemical energy, stored in fossil fuel, into mechanical energy. During this process the main
part of the energy (about 50%) is dissipated as heat [1].
The recovery of the waste heat has a high potential to increase the efficiency of an ICE and consequently to reduce
the fossil fuel consumption and to reduce toxic emissions. Especially the unused exhaust gas waste heat can be
converted into electric power through a thermoelectric generator (TEG) [1,2]. A TEG consists of couples of n- and
p-doted semiconductors. The Seebeck-effect causes a TEG to generate electrical power when a temperature gradient
is applied. The maximum power of a TEG depends on the material characteristics of the semiconductors in the TEG
as well as the geometric parameters of the couples [3,5]. These parameters and materials can be selected in relation
to various optimization criteria.
This includes the temperature range of materials, the desired electrical rated power and the back pressure of the ICE
[1,4,5,6]. This implies that TEGs must be designed and optimized for individual applications. The result is that the
electrical characteristics can vary in a wide range of a TEG.
For the electrical linking of a TEG to a vehicle power supply, a DC-DC converter is necessary, if the voltage
amplitudes of source and load are different. Furthermore, a DC-DC converter works in different modes. The first is
the maximum power point tracking (MPPT) and the second is the trickle charging control (TCC) of the battery
voltage. The MPPT is used to search and match the maximum power point of the TEG, regardless of the temperature
gradient at the TEG. The result is that the alternator of the automobile needs to generate leas power. This increases
the efficiency of the ICE. When the battery is charged and the power of the TEG is higher than the necessary load
power, the trickle charge controller is active.
3
A MPPT is based on a gradient search method and is used in particular for photovoltaic cells. This method can be
applied to a TEG as well. An overview of different search algorithms is presented by Esram [7]. Beside the
algorithms, the implementation of a MPPT can be divided in two general concepts: Control with and without a
feedback signal [8,9,10,11].
The implementation of a feedback control loop requires a detailed system model of the converter, the load and the
TEG to ensure a stable closed loop dynamic. However, a closed loop system can compensate disturbances and a
desired closed loop dynamic behavior can be designed with the control parameters. In contrast to that, a MPPT
without a feedback control – also called direct control – is not able to compensate feedback signals like transient
oscillations which result in a higher conversion time or in a stagnation of the algorithm.
Nevertheless, the problem in designing a feedback control is the necessary knowledge of the control plants.
Especially because the control plant dynamic depends on the electrical parameters of the TEG. Presented control
structures [10,12] are designed based on the assumption, that the parameters of the TEG are nearly constant and well
known. With this assumption the use of the converter is limited to a small number of TEGs. In contrast to that, the
introduction of a robustness criterion allows to design the control parameters to compensate wide variations of the
electrical parameters from a TEG.
In this paper a boost-buck converter with a feedback controller for MPPT and a control of the trickle charge voltage
of the battery (see Fig. 1) is presented. The control design includes a robustness criterion to ensure a stable closed
loop dynamic. The result is a regulated DC-DC converter, which is able to support a wide range of TEGs with
different electrical parameters and different voltage levels of a vehicle power supply. In this context, this paper is
organized as follows: The brief overview of the characteristic from a TEG is presented in section 2. In section 3 the
model of the boost-buck converter is described. The digital control structure of the DC-DC converter is shown in
section 4. Experimental results are presented and discussed in section 5. Finally the methods and results are
summarized in section 6.
2. Thermoelectric Generator
A thermoelectric generator consists of one or more thermoelectric modules (TEMs), which are used in an
application. The TEM is based on a series connection of couples of thermoelectric elements (TEs). A TE is an n- and
p-doted semiconductor, with an electrical connection. Due to a temperature gradient of the TE, heat flows from the
hot to the cold side. The result is that the electrons and holes of the semiconductors diffuse to the cold side and a
voltage potential can be measured at the TE. This physical principle is called the Seebeck-effect, which describes the
voltage
te
u∆
in relation to the temperature gradient
)( c
T
h
T−
and Seebeck coefficent
ρ
Fig. 1. Overview of control structure from boost-buck converter. The alternator is neglected the vehicle power supply.
4
))((),( chnpte TTTu −−=∆
ρρρ
(1)
The resistor
te
r
of the couple depends on the geometry, the material parameters and the temperature
)1(/),( TAlTr
rrte
ασσ
+=∆
(2)
where
σ
is the electrical conductance,
r
α
is the temperature coefficient,
l
is the length and
r
A
is the area of a
couple. The design parameters allow a wide variation of the electrical parameters. A detailed overview of the
electrical conductance, in relation to the semiconductors is presented in Rowe [13].
Generally, the voltage of a TE is between 50 μV/K and 300 μV/K [13]. For practical use, TEs are connected in series
to a TEM. The voltage
tem
u
and the resistor
tem
r
of a module yield to
∑
=
=
N
i
tetem iuu
1
)(
(3)
∑
=
=
N
i
tetem irr
1
)(
(4)
where
N
is the number of the TEs in a module. With the assumption that the temperature is homogeneously
distributed over a TEM and the materials are ideal, the electric equivalent circuit of a TEM can be illustrated as an
ideal voltage source with an internal resistor (see Fig. 2). The relation of the electrical characteristics of a TEM to
the temperature gradient is presented in Fig. 3. This example shows also the electrical power
( )
temintem
iuP =
curve. It
can be clearly seen that only one maximum power point exists at a given temperature gradient. In this point, the
output power of the TEM has the maximum.
3. Modeling of Boost-Buck converter
For the linking of the TEM to the on-board power supply, a boost-buck converter is selected. The advanteges are a
high efficiency and the possibility to generate a variable output voltage [14].
The physical principle of a DC-DC converter is to charge and discharge electric storage elements like inductors or
capacitors. The duration of the charging and discharging is controlled through electric switching elements, like
MOSFETs. As a result, the magnitude of current and voltage of storage elements can be manipulated. The boost-
buck converter includes four MOSFETs, where
21 /SS
and
43
/SS
are synchronized (see Fig. 4). This means, if
31
/SS
is switched on,
42
/SS
is off and vice versa. The MOSFETs are controlled with a pulse-width-modulation
Fig. 2. TEM Module with equivalent electric circuit.
5
signal (PWM) with a constant switching frequency
s
f
. Caused by the PWM, the converter is a non-linear time-
variant system in relation to the duty cycle
d
. The modeling of such a system can be complex. An alternative model
approach for a converter is the state-space-averaging (SSA) [15]. The idea of the SSA is to average the period
changing circuit over a switching period
ss
fT /1=
. The result is a continuous time-invariant model. This method is
accurate for frequencies up to
2/
s
f
[15]. The time derivations of voltages and currents in the boost-buck converter
are:
temLC
Cuiu
dt
du
321 11
1
ααα
++=
(5)
2161326154321
22
2
1211
1
ddidudidiuuui
dt
di
LCLLtemCCL
L
ββββββββ
−−+++++=
(6)
23121
211
2
didii
dt
du
LLL
C
γγγ
++=
(7)
21625243
321
2
1
122
dd
ididieui
dt
di
LLLblCL
L
δδδδδδ
+++++=
(8)
blCL
Ceui
dt
du
321
3
32
εεε
++=
(9)
where
1
d
,
2
d
are the duty cycles of
21 /SS
,
43
/SS
and
εδγβα
,,,,
are system parameters (see Appendix). The
derivatives of the states
[ ]
32211
,,,,
CLCLC
uiuiu=x
are nonlinear. For the following analysis of the converter the
averaged values are substituted by means of a DC and a small AC value [12]. This implies a linearization of (5) – (9)
and results to the small signal state space model for the converter at the operation point
BuAxx+=
(10)
Fig. 3. Voltage and current characteristics of a simulated PbTe TEM at different temperatures (gray line) and the power curves (black line).
6
where
A
is the state matrix,
B
is the input matrix and
[ ]
21,,, ddeu bltem
=u
the input vector. All states can be
measured and are filtered with a second-order low pass. The cutoff frequency is 1 kHz.
Fig. 4. Electric circuit of boost-buck converter with TEM and load.
4. Digital Control Structure
The design of the boost-buck converter is supposed to meet three requirements: The first is the maximum power
point tracking (MPPT), the second is the trickle charge controller (TCC) of the load and the third is the robustness
and stability of the controllers. An overview of the control structure is shown in Fig. 1. The MPPT is based on a
gradient search algorithm, which uses the input current and voltage of the TEM to detect the actual power. This is
realized with the boost converter. The buffer capacitor
2
C
is used to decouple the two converters. A cascade
controller regulates the voltage magnitude of 2
C
and the output current 2L
i
to supply the load and charge the
battery. In case, the output voltage
3C
u
is reaching the maximum charging voltage of the battery, the MPPT will be
disabled and the trickle voltage charge controller is activated. The controllers are implemented on a microcontroller.
In the next subsections the digital control structure is presented, in relation to a robustness criterion. Additionally,
the MPPT algorithm and TCC are presented.
4.1. Control design
In general, the discrete time transfer function from input signal
u
to output signal
y
is defined as
)(
)(
)(
)(
)( 1
1
1
1
1
−
−
−
−
−== zA
zB
zu
zy
zG
plant
(11)
where
A
and
B
are the plant polynomials. The closed loop of a feedback control can be described by
)(
)()(
)(
)(
)(
1
11
1
1
1
−
−−
−
−
−
== zA
zBzT
zr
zy
zG
cl
cl
(12)
where
r
is the reference signal,
T
the pre-filter polynomial of the controller and
)()()()()(
11111 −−−−−
+= zBzRzAzSzA
cl
(13)
is the characteristic polynomial of the closed loop dynamic, in relation to the control polynomials
R
and
S
. The
detailed digital control structure is shown in Fig. 5. In relation to (5) - (10) the transfer function of the boost-buck
converter follow to
)(
)(
)( 1
2
1
12
22 −
−
−=zd
zu
zG C
ud C
(14)
7
)(
)(
)( 1
2
1
12
22 −
−
−=zd
zi
zG L
id L
(15)
)(
)(
)(
1
1
1
1
3
31
−
−
−
=zd
zu
zG
C
ud
C
(16)
)(
)(
)( 1
1
1
1
1
11
−
−
−=zd
zi
zG L
id
L
(17)
The control plants are sensitive to changes of the series resistance of the TEM. In Fig. 6 the frequency response of
the control plant is given for different values of
tem
r
. It can be noted that the gains of
31 C
ud
G
and
22 L
id
G
are
significantly sensitive to
tem
r
. For small values of the resistance, the DC gain shows a maximum and decreases for
higher values. However,
22 C
ud
G
and
11 L
id
G
seem to be smoother, in contrast to
31 C
ud
G
and
22 L
id
G
but also an
influence of the parameter variation from the resistance can be detected. Hence, in all bode plots it can be seen that
the control plants depend on the resistor value of the TEM. If these influences are not taken into account during the
design of control parameters, the stability of the closed loop cannot be guaranteed.
In the context of the analytic results for control parameter design, the robustness criterions gain
m
g
and phase
margin
m
ϕ
of the open loop
)()(
)()(
)( 11
11
1
−−
−−
−=zSzA
zRzB
zGol
(18)
can be specified [16]. A widely used approach is to define
6≥
m
g
dB and
29≥
m
ϕ
°, which must satisfy all values of
Fig. 5. Digital control loops of boost-buck converter.
8
tem
r
. For this reason, the nominal resistance value of 0.1 Ω is selected, because the DC gains of
22 L
id
G
and
31 C
ud
G
are maximal at this value. For higher values of the resistance, the gain and phase margin increase with a
positive effect on the robustness. This characteristic is vice versa for
11 L
id
G
and
22 C
ud
G
, but the variation can be
compensated from the controller with the selected robustness criterion. In context to this criterion, the control
polynomials of the digital controller
1L
i
C
,
3C
u
C
,
2L
i
C
and
2C
u
C
must be designed. The control parameterization is
based on a two-degree of freedom design [16]. The desired closed loop system is chosen as a second order system
−
=
−
−
s
sG
Z
z
zG dcl
cl
)(
1
1
)(
1
!
1
(19)
22
2
2
)(
oo
o
dcl sDs
sG
ωω
ω
++
=
(20)
where
o
ω
is the natural frequency,
D
is the damping factor and
Z
is the discrete time transformation.
For the current control dynamic it is necessary to select an adequate bandwidth to compensate disturbances like load
changes of the vehicle power supply and to reduce the convergence time of the desired input current of the MPPT.
In contrast to that, the voltage controller can be designed with a smaller bandwidth to compensate for lower
frequency control errors. The selected closed loop parameters of the controllers are presented in Table 1.
Table 1. Design parameters for controllers
Controller
o
ω
[kHz]
D
Rise time [ms]
1L
i
C
3.14 0.95 1
2L
i
C
3.14 0.95 1
2C
u
C
0.628 0.95 5
3C
u
C
1.57 0.95 2.5
4.2. Maximum Power Point Tracking
In Fig. 3 the quality characteristic of a TEM and the power curves in relation to different temperature gradients are
presented. In general the electric characteristics and the temperature at the TEM are unknown. The idea is to search
and track the maximum power point by using a gradient algorithm. A gradient algorithm has the advantage, that not
prior knowledge is necessary. In [17] a hill climbing algorithm (HC) for a boost-buck converter is presented.
However, the HC algorithm uses a direct control of the MOSFETs without a feedback signal of the state signals.
The problem is that signal feedbacks or disturbances can result in oscillations. In the case, that the HC recovers
enough energy to charge the buffer capacitor
2
C
, the cascade controller increases the output current
2
L
i
and the
voltage of the capacitor
2
C
u
drops down and results in a feedback signal at the signals
1
C
u
and
1
L
i
. If the HC samples
the disturbance signals, the algorithm interprets this as a power change of the TEM. The algorithm reduces the duty-
cycle and the input power drops down to zero. A new start of the algorithm can result in an oscillation during the
start phase.
An alternative MPPT algorithm is the perturb and observe method (P&O) [7]. This algorithm uses the same gradient
search method as the HC, however the P&O estimates only one new desired operation point of the input current
rL
i1
.
9
This desired current is the reference signal of the input current controller
1L
i
C
. In contrast to the direct control of the
MOSFETs, the controller compensates disturbances of the feedback signal. The desired input current
rL
i
1
is
calculated in relation to the actual input power
)(kP
tem
and compared with the previous power
)1( −kP
tem
. If the
difference
)1()()( −−=∆ kPkPkP temtem
is negative, the desired input current
rL
i
1
is decreased. If
0)( >∆ kP
, the
desired input current is increased. The MPP is reached if
0)( =∆ kP
. The algorithm for P&O yields to
[ ]
)()()1( 11 kPsignkiki rLrL ∆+=+
µ
(21)
[ ]
<∆−
=∆
>∆+
=∆
0,1
0,0
0,1
:)(
P
P
P
kPsign
where
µ
is a constant step size. The selection of the step size influences the performance time of the P&O. For a
large
µ
the P&O converges faster to the MPP. However, the algorithm can oscillate around the exact MPP. In
contrast, the MPPT converges slower for a smaller
µ
, nevertheless the tracked power is closer on the MPP. An
adaption of the step size combines the fast convergence time and the accuracy of a P&O:
<
∆
≤
∆
≤+
>
∆
=
∆
=+
2
)(
)(
)(
,
2
)(
)(2
)(
)(
2
)(
),1(
)(2
)(
)(
),(2
:
)(
)(
)1(
k
k
kP
k
k
k
kP
k
k
k
k
kP
k
k
kP
satk
µ
µ
µ
µ
µ
µ
µ
µ
µ
µ
µ
µ
(23)
The step size reduces for a small gradient of
)(kP∆
and vice versa. The saturation is a boundary of the adaption size.
4.3. Trickle Charge Controller
The TCC is activated in case the load voltage reaches the maximum battery voltage
+
o
u
. The idea of the presented
control structure (see Fig. 5) is to disable the MPPT and use the controller
3C
u
C
to regulate the output voltage on the
desired voltage
rC
u3
. For the selection of MPPT and TCC a switch
C
S
is used. The activation function of
C
S
is
defined as
≥
<<
≥
=
+
+−
−
oC
oCo
Co
C
uu
uuu
uu
S
3
3
3
,2
,21
,1
:
(24)
where
−
o
u
is the defined low voltage magnitude to restart the MPPT.
10
5. Experiments
In section 3 and 4 the modeling and the control structure are presented. To verify the theoretical design, an
experimental device is used. The TEM is simulated with a constant voltage source and a series resistor. The load is a
12.5 V 72 Ah lead acid battery. The converter is controlled by a 320F28069 microcontroller from Texas
Instruments, with a sampling frequency of 10 kHz. The hardware specifications of the converter are presented in
Table 2.
Fig. 6. Bodeplot of control plants.
11 L
id
G
is presented in (1) and (3),
31 C
ud
G
is presented in (2) and (4),
22 L
id
G
is presented in (5) and (7) and
22 C
ud
G
is presented in (6) and (8).
5.1. Verification of Control Design
In relation to the control requirements from Table 1 and the parameters of the converter from Table 2, the controllers
1L
i
C
,
2L
i
C
,
2C
u
C
and
3C
u
C
are designed for a nominal value of
30=
tem
u
V and
1.0=
tem
r
Ω. To verify the feedback
controllers, the step response of each closed loop is measured (see Fig. 7). Each measured output signal of the
control loop matches the desired dynamic of the control design. The deviations of the measurements are caused by
noise and quantization effects of the microcontroller.
11
Table 2. Parameter of converter
HL
µ
45
1
FC
µ
20
1
FC
µ
30
3
Ωmr
L
2.43
1
ΩmrC2.1
1
Ωmr
C
8.0
3
HL
µ
4.22
2
FC
µ
88
2
Vebl 5.12
Ωmr
L
7.17
2
Ωmr
C
1.17
2
Ωmrbl 100
4321
,,, SSSS
Infineon IPP80N06S2L-07 ,
s
f
= 100 kHz
Fig. 7. Step responses of the control loops. The red dashed line is the reference signal. The black line is the desired output signal and grey the
measurement. (1) shows the controlled signal of
1
L
i
, (2) the signal of
3
C
u
, (3) the signal of
2
L
i
and (4)
2
C
u
.
5.2. Verification of Maximum Power Point Tracking
In this experiment, the TEM is simulated with nominal values
15=
tem
u
V and
1.3=
tem
r
Ω at the beginning. To verify
the convergence and adaption, the resistor and the voltage are changed.
In Fig. 8 the signals of the converter and the simulated TEM are shown. After 1.5 s the MPPT is enabled and the
algorithm starts to calculate the desired reference input current, which is regulated with the input current
controller
1L
i
C
. After approximately 1 s the MPP is reached and the algorithm has converged. This can also directly
be recognized from the measurement, because
temin uu 2/1=
in this case. At 3.7 s the resistor changes to 1.8 Ω. The
reaction of the MPPT has a dead time of nearly 300 ms before an adaption of the new MPP can be observed. The
12
dead time is the result of the adaptive P&O algorithm (23), because the step size is reduced in relation to the
previously small power difference
P∆
. After the detection of the power change, the step size must increase. This
dead time can also be observed when the input changes to
30=
tem
u
V.
However, at the moment when the input voltage increases, a peak of value at the input current can be detected. This
disturbance is compensated by the input controller. Without the control, it would lead to an undesired increase of the
current signal. Finally, the estimated gradient of the input power could be incorrect.
Nevertheless, the P&O algorithm converges in all three cases to the MPP with a maximum converge time of 2 s.
Fig. 9 shows the detailed calculation and adaption of the desired input current
rL
i
1
of the MPPT algorithm for the
time spans (a), (b) and (c) from Fig. 8 in relation to the actual power curves of the TEM.
5.3. Verification of Trickle Charge Controller
In this experiment, the battery was charged to 13.3 V. At the beginning of the experiment
15=
tem
u
V and
Ω= 1.3
tem
r
are selected and the MPPT is active (see Fig. 10). The resistor value changes from 3.1 Ω to 1.8 Ω at 40
ms and the MPPT increases the input current and also the input power. As a result, the output voltage increases up to
the selected maximum battery voltage
6.13=
+
o
u
V. At this time, the TCC is activated and the desired voltage
4.13
3
=
rC
u
V is regulated. To match this voltage, the input current is reduced to 2.1 A. At 500 ms the resistor
changes to
Ω= 1.3
tem
r
and the input power is not sufficient to hold on the trickle voltage. As a consequence, the
output voltage decreases and the TCC increases the input current to match the desired battery voltage. At the point
that the output voltage drops down to
3.13=
−
o
u
V, the MPPT is reactivated.
Fig. 10. Verification of TCC algorithm. The grey line is
tem
u
, the blue line is
in
u
and the red line is the input current
tem
i
at the top
ill t ti I th b tt i h th t t lt ith th t d t t f th
Fig. 8. Verification of MPPT algorithm. The grey line is
tem
u
, the blue line is
in
u
, the grey dashed line is the output voltage
3
C
u
and the red
line is the input current
tem
i
.
Fig. 9. Step size adaption of MPPT algorithm for the time spans (a), (b) and (c) from Fig. 8.
13
6. Conclusions
In this paper a control concept for a boost-buck converter is presented. A variation of the electrical characteristics of
the TEGs is analysed in the frequency domain. The series resistance of the TEG influences the state dynamic of the
control plants. The operation point for the state space model is selected for the resistor value, which caused the
highest DC gain of the plants. Based on this selected operation point, the linear digital controllers are designed. A
robustness criterion is defined to ensure the stability of the closed loop dynamic for a variation of the electrical
parameters of the TEG.
The presented MPPT is based on a perturbe and observation algorithm, which determines a desired input current. In
contrast to a direct control algorithm, an oscillation at the start phase of the algorithm or disturbances can be
compensated. The perturbed and observation algorithm is extended with a variable step size to reduce the oscillation
at the MPP and to adapt the step size in relation to the power gradient of the actual power from the TEG. An
overvoltage protection for the battery is realized with a trickle charging control. In this case, the MPPT algorithm is
disabled and the desired trickle charge voltage is controlled with a cascade voltage controller. The control and
algorithms are proven in experiments.
The next steps are to analyse and optimize the electrical wiring of explicit TEMs for a DC-DC converter to optimize
the power efficiency. Furthermore a TEG prototype with DC-DC converter should be integrated and verified at an
exhaust gas system of internal combustion engine.
Acknowledgements
The project “Thermoelektrische Generatoren 2020” (03X3553E) is supported by the German ministry of education
and research (BMBF). The authors would like to thank Texas Instruments for the support through their innovative
products.
Appendix
)(
1
1
1
3
2
1
temCtem
rrCr +
−=−==
α
α
α
(25)
)(
)()()(
1
2122111
1
1
Ctem
temdsCtemdsCtemCLCtem
rrL
rrrrrrrrrrr
+
++++++
=
β
(26)
)(
1
1
2
Ctem
tem
rrL
r
+
=
β
(27)
1
6
3
1
1
LrC
−=−=
β
β
(28)
)(
1
1
1
4
Ctem
C
rrL
r
+
=
β
(29)
1
5
)( 122
L
rrr
dsdsC
−+
=
β
(30)
2
321
1
C
=−=−=
γγγ
(31)
)2
1
3
3333223
(
blC
bldsCdsblCLblLC
rrL
rrrrrrrrrr
+
++++
−=
δ
(32)
14
)(
3
2
32
blC
bl
rrL
r
+
−=−=
δδ
(33)
2
4
342
L
rrr
dsdsC
−+
−=
δ
(34)
2
65 2
L
r
C
=−=
δδ
(35)
)(
1
3
3
3
1
2
blCbl
rrCr +
−=−=−=
ε
ε
ε
(36)
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