Influence of the Main Design Factors on the Optimal Fuel Cell-Based Powertrain Sizing

The design of the optimal power distribution system (PDS or powertrain) for fuel cell-based vehicles is a complex task due to PDS comprising one or more power converters, several types of secondary energy sources, a fuel cell, several control loops, and protections, among others. The optimized powertrain design tries to minimize the mass, volume, and cost, and also to improve system efficiency, fuel economy (both hydrogen and electricity), and vehicle autonomy. This paper analyzes the influence of four different factors that deeply affect the optimal powertrain design, in particular: the minimum power delivered by the fuel cell, the storage of the recovered energy from the regenerative braking periods, the battery technology, and the maximum battery state-of-charge variation. The analysis of these factors is carried out over a set of 9 different fuel cell-based architectures applied to a light vehicle, and a 10th architecture corresponding to a pure electric vehicle. This analysis provides the knowledge of how these design factors affect the mass, volume, and cost of the optimal power distribution architectures, and how they can be considered in the design.


Introduction
Fuel cell (FC)-based vehicles present growing reliability and autonomy [1][2][3], which is the reason they are beginning to be considered a strong alternative to internal combustion engine vehicles.One of the challenges of fuel cell-based vehicles is the design of the power distribution system (PDS or powertrain).The powertrain must be able to overcome the major drawbacks of the fuel cell: load-dependent output voltage, unidirectional power flow, slow dynamic response, and other operating characteristics, such as high-temperature startup, very long startup times, and overshoot or overdamped transient responses [4][5][6].
Fuel cell-based vehicles are strategically focused on improving the maximum speed, acceleration, autonomy, and cost [7].Therefore, minimizing the mass and cost of the powertrain is of great importance to the maximization of autonomy and fuel saving, and the achievement of a competitive price.The elements that comprise the propulsion system are the fuel cell system, the DC-DC power converters, and the energy storage devices (batteries and supercapacitors).
The selection of the most suitable fuel cell-based power distribution system is a complex task that has a significant influence on the vehicle mass, volume, cost, autonomy, efficiency, etc.In fact, there is an extensive range of possibilities in the design of a fuel cell-based power distribution system.These possibilities depend on the number, location, and kind of energy storage devices and power Energies 2018, 11, 3060 2 of 22 converters, as well as on the control strategy and the storage of energy from the regenerative braking periods [8][9][10][11][12].
Some papers in the literature analyze and compare different PDSs based on fuel cells and batteries [7,8,11,13], based on fuel cells and supercapacitors [9,[14][15][16][17], and, finally, based on fuel cells, batteries, and supercapacitors [10,[18][19][20][21][22].In [23], a complete analysis and comparison of 10 different power distribution systems are presented, considering all the possibilities in powertrain implementation (fuel cell and batteries, fuel cell and batteries and supercapacitors, fuel cell and supercapacitors).Also provided in [23] is an optimal sizing procedure for fuel cell-based architectures, in which the minimum cost and mass are calculated as a function of the maximum power delivered by the fuel cell.All the analyses are carried out for a light vehicle of 800 kg, operating during a working day of 8 h with the European urban driving cycle ECE-15.The subsystems considered in the PDS are the fuel cell stack, the fuel cell hydrogen tank, the battery, the supercapacitors, and the DC-DC power converters [24][25][26][27].
Considering, as a starting point, the optimal sizing procedure presented in [23], this paper analyzes the influence of four different design factors on the mass and cost of the PDS, continuing with the work presented in [28], in which the influence of the driving profile is analyzed.These factors are the minimum power delivered by the fuel cell, the energy storage from the regenerative braking periods, the battery technology, and, finally, the maximum battery state-of-charge variation.These design factors can vary significantly not only in the mass, volume, and cost of the complete PDS but also the selection of the optimal power distribution architectures.
This paper organizes as follows.Section 2 describes the power distribution architectures that constitute the power distribution systems, as well as the main vehicle characteristics.Section 3 reviews the influence of applying the different driving profiles described in [28].The influence of the minimum power delivered by the fuel cell is analyzed in Section 4. Section 5 describes the effect of considering the storage of the energy recovered from the regenerative braking periods when it is bigger than the energy delivered by the secondary energy sources.Section 6 describes the influence of using different battery technologies, and, finally, Section 7 analyzes the effect of imposing a different state-of-charge variation to the secondary energy sources.Section 8 summarizes the conclusions collected throughout this research paper.

Power Distribution Systems and Vehicle Characteristics
Different power distribution systems (PDSs) can be implemented depending on the number and location of the elements that comprise each architecture, particularly a fuel cell, a battery, one or more DC-DC power converters, and the supercapacitors [23] (see Figure 1).Of all of these elements, the fuel cell is the primary energy source.Additionally, for the sake of comparison, a 10th architecture is considered, which corresponds to a pure electric vehicle (0B).This architecture has been included in the analysis to highlight and compare the advantages and drawbacks between a pure electric car and a fuel cell-based vehicle, regarding mass and cost.
Applying the optimal sizing procedure described in [23], the minimum sum of battery mass and supercapacitor mass can be calculated depending on the maximum power delivered by the fuel cell.These results determine the most suitable range of the maximum fuel cell power for each architecture.Also, this procedure has allowed the grouping of architectures depending on the nature of the secondary energy sources: those that use only batteries, a combination of batteries and supercapacitors, or only supercapacitors, as shown in Figure 1.
All the analyses are developed for a light vehicle of 800 kg.The considered electrical efficiency from the wheels to the motor drive is 0.75, the unidirectional DC-DC power converter efficiency is 0.95, the bidirectional DC-DC power converter efficiency is 0.9, and the considered fuel cell system efficiency is 0.6.The battery and supercapacitor efficiencies are 0.95.For the case where a three-port converter is used, two equivalent two-port converters can be obtained with a mass, volume, and cost that are proportional to the power delivery by each port.Finally, the cost of every PDS is obtained Energies 2018, 11, 3060 3 of 22 considering the production of 500,000 units.All these data and the further interesting information discussed below has been obtained from [23].

Driving Profile Influence
The influence of the driving profile was already analyzed in [28].In this paper, this influence is reviewed for a better understanding of the rest of the paper.
Three different European driving profiles, listed in Table 1, are used to evaluate the internal combustion engines (ICE) regarding pollutant emissions and fuel economy [29]; these profiles are considered here to analyze the influence of the driving profile on the size, volume, and cost of the power distribution systems.Each driving profile implies a different power profile, as shown in Figure 2 [28].

Driving Profile Influence
The influence of the driving profile was already analyzed in [28].In this paper, this influence is reviewed for a better understanding of the rest of the paper.
Three different European driving profiles, listed in Table 1, are used to evaluate the internal combustion engines (ICE) regarding pollutant emissions and fuel economy [29]; these profiles are considered here to analyze the influence of the driving profile on the size, volume, and cost of the power distribution systems.Each driving profile implies a different power profile, as shown in Figure 2 [28].Figure 3 shows the normalized battery and supercapacitor mass evolution depending on the maximum fuel cell power, obtained by the procedure described in [23].The influence of the driving profile can be noticed in the power level that limits each region, as shown in Table 2.
As can be noticed, for the lower fuel cell maximum power, only batteries achieve the PDS minimum mass.At the highest fuel cell maximum power range, the PDS minimum mass is achieved by only supercapacitors, although this power region is very narrow.Finally, in the intermediate range of fuel cell maximum power, the PDS minimum mass is achieved using both batteries and supercapacitors.Figure 3 shows the normalized battery and supercapacitor mass evolution depending on the maximum fuel cell power, obtained by the procedure described in [23].The influence of the driving profile can be noticed in the power level that limits each region, as shown in Table 2.
As can be noticed, for the lower fuel cell maximum power, only batteries achieve the PDS minimum mass.At the highest fuel cell maximum power range, the PDS minimum mass is achieved by only supercapacitors, although this power region is very narrow.Finally, in the intermediate range of fuel cell maximum power, the PDS minimum mass is achieved using both batteries and supercapacitors.Applying this analysis to every PDS shown in Figure 1, it is apparent that the optimal power distribution architectures are the same, independent of the applied driving profile.This optimal PDSs are 1B, 1BC, and 1C2.Also, in the case where energy and power delivery by the battery and the supercapacitors in the 1BC architecture cannot be controlled independently, the 1BC architecture can be replaced by the 2BC architecture.A more detailed explanation can be found in [28].

Influence of the Minimum Power Delivered by the Fuel Cell
Due to their performances, fuel cells are growing as an alternative for use in hybrid vehicles.However, their operating characteristics make it mandatory to design the PDS, control loops, and energy management strategies to mitigate their slow dynamic response, load-dependent output voltage, unidirectional operation, long startup times, low-temperature startup, and overshoot and overdamped transient responses [4,6,30,31].Indeed, since the startup time can last for tens of seconds, the minimum fuel cell-delivered power must be considered for avoiding unexpected fuel cell shutdowns, as Figure 4 depicts.Applying this analysis to every PDS shown in Figure 1, it is apparent that the optimal power distribution architectures are the same, independent of the applied driving profile.This optimal PDSs are 1B, 1BC, and 1C2.Also, in the case where energy and power delivery by the battery and the supercapacitors in the 1BC architecture cannot be controlled independently, the 1BC architecture can be replaced by the 2BC architecture.A more detailed explanation can be found in [28].

Influence of the Minimum Power Delivered by the Fuel Cell
Due to their performances, fuel cells are growing as an alternative for use in hybrid vehicles.However, their operating characteristics make it mandatory to design the PDS, control loops, and energy management strategies to mitigate their slow dynamic response, load-dependent output voltage, unidirectional operation, long startup times, low-temperature startup, and overshoot and overdamped transient responses [4,6,30,31].Indeed, since the startup time can last for tens of seconds, the minimum fuel cell-delivered power must be considered for avoiding unexpected fuel cell shutdowns, as Figure 4 depicts.The gray line represents the power demanded by the load, and the blue line represents the power delivered by the fuel cell.
Because the tendencies are the same for the three analyzed profiles, in this section, three different minimum power values are applied-0 W, 200 W, and 400 W, considering the same ECE-15 driving cycle only-to evaluate the influence of the fuel cell minimum power.
Figure 5 shows the new optimal power ranges for each group of architecture as a function of the fuel cell minimum power.It can be seen that both power limits (Linf and Lupp) are shifted toward lower fuel cell maximum power values when the minimum power increases.This effect is because a higher fuel cell minimum power implies a larger amount of energy delivered by the fuel cell.As a consequence, the power range with only batteries is reduced as the minimum fuel cell power increases, since the equivalent energy and power load requirements are lower.Figure 6 shows the optimal mass, volume, and cost of each architecture evaluated in their optimal power range with the three different minimum power values [23].The gray line represents the power demanded by the load, and the blue line represents the power delivered by the fuel cell.
Because the tendencies are the same for the three analyzed profiles, in this section, three different minimum power values are applied-0 W, 200 W, and 400 W, considering the same ECE-15 driving cycle only-to evaluate the influence of the fuel cell minimum power.
Figure 5 shows the new optimal power ranges for each group of architecture as a function of the fuel cell minimum power.It can be seen that both power limits (L inf and L upp ) are shifted toward lower fuel cell maximum power values when the minimum power increases.This effect is because a higher fuel cell minimum power implies a larger amount of energy delivered by the fuel cell.As a consequence, the power range with only batteries is reduced as the minimum fuel cell power increases, since the equivalent energy and power load requirements are lower.The gray line represents the power demanded by the load, and the blue line represents the power delivered by the fuel cell.
Because the tendencies are the same for the three analyzed profiles, in this section, three different minimum power values are applied-0 W, 200 W, and 400 W, considering the same ECE-15 driving cycle only-to evaluate the influence of the fuel cell minimum power.
Figure 5 shows the new optimal power ranges for each group of architecture as a function of the fuel cell minimum power.It can be seen that both power limits (Linf and Lupp) are shifted toward lower fuel cell maximum power values when the minimum power increases.This effect is because a higher fuel cell minimum power implies a larger amount of energy delivered by the fuel cell.As a consequence, the power range with only batteries is reduced as the minimum fuel cell power increases, since the equivalent energy and power load requirements are lower.Figure 6 shows the optimal mass, volume, and cost of each architecture evaluated in their optimal power range with the three different minimum power values [23].Figure 6 shows the optimal mass, volume, and cost of each architecture evaluated in their optimal power range with the three different minimum power values [23].Figure 6 shows, for each architecture group, the PDSs that present optimal mass, volume, and cost, depending on the fuel cell minimum power.Among them, the best performances are again achieved with the architectures 1B, 1BC, and 1C2, like in the previous section.Additionally, as the delivered minimum power by the fuel cell increases, the architectures based only on supercapacitors and those based on batteries together with supercapacitors, 1BC and 1C2, experience a decrease in their overall mass and volume.However, architecture 1B presents different behavior concerning architectures 1BC and 1C2.
Architecture 1B presents a mass, volume, and cost increase as the fuel cell minimum power increases, whereas architectures 1BC and 1C2 suffer a mass, volume, and cost reduction.It is because if the fuel cell minimum power increases, PFCmin, the design power limit for the PDS with only batteries, Linf, decreases.The higher the fuel cell minimum power, PFCmin, the higher the battery total mass needed to satisfy the load requirements.In other words, increasing the fuel cell minimum power, PFCmin, implies a smaller design power limit Linf, which means a lower fuel cell maximum power, and, therefore, the minimum battery mass must be higher, as Figure 7 depicts.Figure 6 shows, for each architecture group, the PDSs that present optimal mass, volume, and cost, depending on the fuel cell minimum power.Among them, the best performances are again achieved with the architectures 1B, 1BC, and 1C2, like in the previous section.Additionally, as the delivered minimum power by the fuel cell increases, the architectures based only on supercapacitors and those based on batteries together with supercapacitors, 1BC and 1C2, experience a decrease in their overall mass and volume.However, architecture 1B presents different behavior concerning architectures 1BC and 1C2.
Architecture 1B presents a mass, volume, and cost increase as the fuel cell minimum power increases, whereas architectures 1BC and 1C2 suffer a mass, volume, and cost reduction.It is because if the fuel cell minimum power increases, P FCmin , the design power limit for the PDS with only batteries, L inf , decreases.The higher the fuel cell minimum power, P FCmin , the higher the battery total mass needed to satisfy the load requirements.In other words, increasing the fuel cell minimum power, P FCmin , implies a smaller design power limit L inf , which means a lower fuel cell maximum power, and, therefore, the minimum battery mass must be higher, as Figure 7 depicts.Figure 6 shows, for each architecture group, the PDSs that present optimal mass, volume, and cost, depending on the fuel cell minimum power.Among them, the best performances are again achieved with the architectures 1B, 1BC, and 1C2, like in the previous section.Additionally, as the delivered minimum power by the fuel cell increases, the architectures based only on supercapacitors and those based on batteries together with supercapacitors, 1BC and 1C2, experience a decrease in their overall mass and volume.However, architecture 1B presents different behavior concerning architectures 1BC and 1C2.
Architecture 1B presents a mass, volume, and cost increase as the fuel cell minimum power increases, whereas architectures 1BC and 1C2 suffer a mass, volume, and cost reduction.It is because if the fuel cell minimum power increases, PFCmin, the design power limit for the PDS with only batteries, Linf, decreases.The higher the fuel cell minimum power, PFCmin, the higher the battery total mass needed to satisfy the load requirements.In other words, increasing the fuel cell minimum power, PFCmin, implies a smaller design power limit Linf, which means a lower fuel cell maximum power, and, therefore, the minimum battery mass must be higher, as Figure 7 depicts.Figure 7 shows the fuel cell system, battery, and DC-DC converter mass evolution for architecture 1B, depending on the fuel cell maximum power delivered, when two different values of the fuel cell minimum power are used, 0 W and 400 W. For a fuel cell minimum power value of 0 W, the power design limit for a battery-based PDS is L inf = 2.5 kW, as shown in Figure 5a.On the other hand, for a fuel cell minimum power of 400 W, the design power limit for a battery-based PDS is L inf = 1.8 kW, as in Figure 5c.The battery masses for these two limits are 47.4 kg (for L inf = 2.5 W) and 52.4 kg (for L inf = 1.8 kW), respectively (Figure 7).This means that the battery mass related to the lower design power limit, L inf = 1.8 kW, is larger than the battery mass related to the higher design power limit, L inf = 2.5 kW.
With the new lower power limit in the region of architecture 1B, the fuel cell and power converter mass, volume, and cost reduction are smaller than the battery mass, volume, and cost increment, as shown in Figure 7. Therefore, for those architectures that use only batteries as secondary energy sources, the overall mass, volume, and cost increase with the fuel cell minimum power P FCmin .
On the contrary, in architectures 1BC and 1C2, the fuel cell and power converter mass, volume, and cost reduction are more significant than the energy storage devices mass, volume, and cost increment.
Tables 3-5 show the optimal mass, volume, and cost for each architecture, evaluated in their optimal design power range, under the three considered FC minimum power values.Additionally, each table includes two columns, in which the mass, volume, and cost reduction are shown, in percentage.By considering 0 W as a reference, one column shows the percentage variations obtained when the minimum power is established as 200 W, and the other shows the percentage variations obtained when the minimum power is 400 W. The colors toward green and the upwards pointing arrows indicate an improvement in mass, volume or cost and, the colors toward red and the downward pointing arrows indicate a worsening in mass, volume or cost.Table 3. Influence of the fuel cell minimum power on PDS mass for the ECE-15 profile.
Figure 7 shows the fuel cell system, battery, and DC-DC converter mass evolution for architecture 1B, depending on the fuel cell maximum power delivered, when two different values of the fuel cell minimum power are used, 0 W and 400 W. For a fuel cell minimum power value of 0 W, the power design limit for a battery-based PDS is Linf = 2.5 kW, as shown in Figure 5a.On the other hand, for a fuel cell minimum power of 400 W, the design power limit for a battery-based PDS is Linf = 1.8 kW, as in Figure 5c.The battery masses for these two limits are 47.4 kg (for Linf = 2.5 W) and 52.4 kg (for Linf = 1.8 kW), respectively (Figure 7).This means that the battery mass related to the lower design power limit, Linf = 1.8 kW, is larger than the battery mass related to the higher design power limit, Linf = 2.5 kW.
With the new lower power limit in the region of architecture 1B, the fuel cell and power converter mass, volume, and cost reduction are smaller than the battery mass, volume, and cost increment, as shown in Figure 7. Therefore, for those architectures that use only batteries as secondary energy sources, the overall mass, volume, and cost increase with the fuel cell minimum power PFCmin.
On the contrary, in architectures 1BC and 1C2, the fuel cell and power converter mass, volume, and cost reduction are more significant than the energy storage devices mass, volume, and cost increment.
Tables 3-5 show the optimal mass, volume, and cost for each architecture, evaluated in their optimal design power range, under the three considered FC minimum power values.Additionally, each table includes two columns, in which the mass, volume, and cost reduction are shown, in percentage.By considering 0 W as a reference, one column shows the percentage variations obtained when the minimum power is established as 200 W, and the other shows the percentage variations obtained when the minimum power is 400 W. The colors toward green and the upwards pointing arrows indicate an improvement in mass, volume or cost and, the colors toward red and the downward pointing arrows indicate a worsening in mass, volume or cost.From the collected data in these tables, it can be concluded that: • The mass, volume, or cost of the battery-based architectures are affected by the minimum power level of the fuel cell.

•
The battery-and-supercapacitor-based architecture and the supercapacitor-based architectures present the highest advantage of the FC minimum power increment, except architecture 3C.
Architecture 3C shows a cost increment when the fuel cell minimum power increases due to the high number of power converters it uses.From the collected data in these tables, it can be concluded that: • The mass, volume, or cost of the battery-based architectures are affected by the minimum power level of the fuel cell.

•
The battery-and-supercapacitor-based architecture and the supercapacitor-based architectures present the highest advantage of the FC minimum power increment, except architecture 3C.
Architecture 3C shows a cost increment when the fuel cell minimum power increases due to the high number of power converters it uses.
From the collected data in these tables, it can be concluded that:

•
The mass, volume, or cost of the battery-based architectures are affected by the minimum power level of the fuel cell.

•
The battery-and-supercapacitor-based architecture and the supercapacitor-based architectures present the highest advantage of the FC minimum power increment, except architecture 3C.
Architecture 3C shows a cost increment when the fuel cell minimum power increases due to the high number of power converters it uses.

•
Since the mass and size reductions are very similar for the best architectures, the selection of the optimal architecture must be made based on the cost.So, regarding cost, the optimal architectures are 1BC and 1C2, which reduce their cost by 12%.

•
The last conclusion is related to the fuel cell hydrogen consumption.From the manufacturer's point of view, an increase in the delivered minimum power by the fuel cell implies a mass, volume, and cost reduction.However, at the same time, an increase in the delivered minimum power by the fuel cell means an increase in the energy delivered by the fuel cell throughout the working day.Therefore, the final user consumes more hydrogen every month.
Figure 8 shows, as an example, the evolution of the mass, volume, and cost, depending on the fuel cell maximum power, for a fuel cell minimum power equal to 400 W and for each architecture.This information has been used to obtain the data in Tables 3-5.As can be seen, each plot has three regions: only battery, battery and supercapacitor, and only supercapacitors.The L inf and L upp shown in Figure 8 (vertical gray lines) match with those shown in Figure 5c and separate the three design regions.For these conditions, the minimum mass, volume, and cost are obtained for a fuel cell maximum power around 5 kW, inside the battery and supercapacitor region.Similar results are obtained when the fuel cell minimum power is 0 W and 200 W, but with different limits and values, as shown in Tables 3-5.

•
Since the mass and size reductions are very similar for the best architectures, the selection of the optimal architecture must be made based on the cost.So, regarding cost, the optimal architectures are 1BC and 1C2, which reduce their cost by 12%.

•
The last conclusion is related to the fuel cell hydrogen consumption.From the manufacturer's point of view, an increase in the delivered minimum power by the fuel cell implies a mass, volume, and cost reduction.However, at the same time, an increase in the delivered minimum power by the fuel cell means an increase in the energy delivered by the fuel cell throughout the working day.Therefore, the final user consumes more hydrogen every month.
Figure 8 shows, as an example, the evolution of the mass, volume, and cost, depending on the fuel cell maximum power, for a fuel cell minimum power equal to 400 W and for each architecture.This information has been used to obtain the data in Tables 3-5.As can be seen, each plot has three regions: only battery, battery and supercapacitor, and only supercapacitors.The Linf and Lupp shown in Figure 8 (vertical gray lines) match with those shown in Figure 5c and separate the three design regions.For these conditions, the minimum mass, volume, and cost are obtained for a fuel cell maximum power around 5 kW, inside the battery and supercapacitor region.Similar results are obtained when the fuel cell minimum power is 0 W and 200 W, but with different limits and values, as shown in Tables 3-5.

Influence of the Storage of the Energy Recovered from Regenerative Braking Periods
This section describes the effect of considering the storage of the net amount of energy when the energy recovered from the regenerative braking is greater than the energy delivered by the secondary energy sources to complement the energy provided by the fuel cell.If such is the case, then the net amount of energy along the driving cycles in a working day (8 h) is negative, since the secondary energy sources charge in each cycle.

Influence of the Storage of the Energy Recovered from Regenerative Braking Periods
This section describes the effect of considering the storage of the net amount of energy when the energy recovered from the regenerative braking is greater than the energy delivered by the secondary Energies 2018, 11, 3060 energy sources to complement the energy provided by the fuel cell.If such is the case, then the net amount of energy along the driving cycles in a working day (8 h) is negative, since the secondary energy sources charge in each cycle.
The power and energy that the secondary energy sources must provide are P diff (P) and E diff (P), which are determined as follows.The power P diff (P) is calculated as the difference between the peak power of the load profile and the maximum power delivered by the fuel cell, P(W), as depicted in Figure 9. On the other hand, the energy E diff (P) is the net amount of energy delivered by the secondary energy sources for all the driving cycles in a working day.This is the difference between the energy demanded by the load that the fuel cell is not able to provide (yellow areas in Figure 9) and the energy recovered and stored from the regenerative braking periods (blue areas) for all the driving cycles in the working day (8 h).
Energies 2018, 11, x 11 of 22 The power and energy that the secondary energy sources must provide are Pdiff(P) and Ediff(P), which are determined as follows.The power Pdiff(P) is calculated as the difference between the peak power of the load profile and the maximum power delivered by the fuel cell, P(W), as depicted in Figure 9. On the other hand, the energy Ediff(P) is the net amount of energy delivered by the secondary energy sources for all the driving cycles in a working day.This is the difference between the energy demanded by the load that the fuel cell is not able to provide (yellow areas in Figure 9) and the energy recovered and stored from the regenerative braking periods (blue areas) for all the driving cycles in the working day (8 h).The normalized battery mass obtained after applying the optimization procedure [23], including the possibility that the energy recovered from regenerative braking can be greater than the energy delivered by the secondary energy sources, is represented in Figure 10, as a function of the maximum power delivered by the fuel cell.As it can be seen, as the maximum fuel cell power increases, the net amount of energy that must be delivered by the secondary energy sources, Ediff(P), decreases.However, it is expectable that for high values of fuel cell maximum power, the net amount of energy Ediff(P) becomes negative since the energy recovered from the braking is bigger than the energy delivered to the load by the secondary energy sources.This effect is easily identifiable in Figure 10, and it corresponds to the turning point placed at 6.2 kW.
In Figure 10, three different regions are highlighted based on the maximum power delivered by the fuel cell that minimizes the cost and mass in each region.For fuel cell maximum powers below Linf (0 < P < Linf), architectures that implement only batteries as secondary energy sources are the recommended ones.For Linf < P < Lupp, the use of batteries and supercapacitors as secondary energy sources is suggested.These two regions are only affected in the values of both the limits and the evolution of the normalized battery mass inside the region in which the batteries and supercapacitor are recommended.However, it is noticeable that now the architectures recommended for the third region (P > Lupp) are no longer based on only supercapacitors, but they are based on implementing only batteries as secondary energy sources.The normalized battery mass obtained after applying the optimization procedure [23], including the possibility that the energy recovered from regenerative braking can be greater than the energy delivered by the secondary energy sources, is represented in Figure 10, as a function of the maximum power delivered by the fuel cell.As it can be seen, as the maximum fuel cell power increases, the net amount of energy that must be delivered by the secondary energy sources, E diff (P), decreases.However, it is expectable that for high values of fuel cell maximum power, the net amount of energy E diff (P) becomes negative since the energy recovered from the braking is bigger than the energy delivered to the load by the secondary energy sources.This effect is easily identifiable in Figure 10, and it corresponds to the turning point placed at 6.2 kW.
In Figure 10, three different regions are highlighted based on the maximum power delivered by the fuel cell that minimizes the cost and mass in each region.For fuel cell maximum powers below L inf (0 < P < L inf ), architectures that implement only batteries as secondary energy sources are the recommended ones.For L inf < P < L upp , the use of batteries and supercapacitors as secondary energy sources is suggested.These two regions are only affected in the values of both the limits and the evolution of the normalized battery mass inside the region in which the batteries and supercapacitor are recommended.However, it is noticeable that now the architectures recommended for the third region (P > L upp ) are no longer based on only supercapacitors, but they are based on implementing only batteries as secondary energy sources.
Figures 11 and 12 show the cost and mass of architectures 1B and 2B in both the lower and the upper power ranges.It can be observed in Figure 11 that the mass and cost evolution of the propulsion systems 1B and 2B are not affected by considering that the energy from the regenerative braking periods is bigger than the energy demanded by the load that the fuel cell cannot satisfy throughout the 8 h working day.

L upp L inf
Maximum power delivered by the fuel cell (kW) Normalized battery mass Figures 11 and 12 show the cost and mass of architectures 1B and 2B in both the lower and the upper power ranges.It can be observed in Figure 11 that the mass and cost evolution of the propulsion systems 1B and 2B are not affected by considering that the energy from the regenerative braking periods is bigger than the energy demanded by the load that the fuel cell cannot satisfy throughout the 8 h working day.Figures 11 and 12 show the cost and mass of architectures 1B and 2B in both the lower and the upper power ranges.It can be observed in Figure 11 that the mass and cost evolution of the propulsion systems 1B and 2B are not affected by considering that the energy from the regenerative braking periods is bigger than the energy demanded by the load that the fuel cell cannot satisfy throughout the 8 h working day.

L upp L inf
Maximum power delivered by the fuel cell (kW) Normalized battery mass Figure 12 shows the mass and cost evolution of architectures 1B and 2B in the upper design power range, from 10 kW to 15.6 kW.In both architectures, the minimum mass and cost are achieved at Lupp (10 kW).It can be noticed that the higher the maximum power delivered by the fuel cell, the bigger the battery mass, since the batteries must be able to store a larger amount of remaining energy from the difference between the energy delivered to the load by the secondary energy sources and the energy recovered from the braking periods.Regarding the cost, it presents an increasing trend analogous to the battery mass increase as the maximum power of the fuel cell increases.
Therefore, Figures 11 and 12 show that architectures 1B and 2B have minimum mass when they are designed at 10 kW, since the battery mass increment is lower than the mass increment experienced by the fuel cell.On the other hand, the minimum cost of powertrains 1B and 2B is achieved when they are designed at 2.5 kW due to the fact that the fuel cell and converter cost increments are bigger than the battery cost decrement.
Figure 13 depicts the mass and cost evolution as a function of the maximum power delivered by the fuel cell of powertrains 1BC, 2BC, and 3BC.In this case, all the architectures reach the minimum mass and cost at the turning point placed at 6.2 kW.Also, it can be noticed that the total mass of powertrains 1BC, 2BC, and 3BC is imposed by the fuel cell system mass, including the hydrogen tank.From the three architectures, 1BC presents the minimum mass.Regarding the cost, and due to the reduced number of power converters, propulsion system 1BC is the cheapest.Figure 12 shows the mass and cost evolution of architectures 1B and 2B in the upper design power range, from 10 kW to 15.6 kW.In both architectures, the minimum mass and cost are achieved at L upp (10 kW).It can be noticed that the higher the maximum power delivered by the fuel cell, the bigger the battery mass, since the batteries must be able to store a larger amount of remaining energy from the difference between the energy delivered to the load by the secondary energy sources and the energy recovered from the braking periods.Regarding the cost, it presents an increasing trend analogous to the battery mass increase as the maximum power of the fuel cell increases.
Therefore, Figures 11 and 12 show that architectures 1B and 2B have minimum mass when they are designed at 10 kW, since the battery mass increment is lower than the mass increment experienced by the fuel cell.On the other hand, the minimum cost of powertrains 1B and 2B is achieved when they are designed at 2.5 kW due to the fact that the fuel cell and converter cost increments are bigger than the battery cost decrement.
Figure 13 depicts the mass and cost evolution as a function of the maximum power delivered by the fuel cell of powertrains 1BC, 2BC, and 3BC.In this case, all the architectures reach the minimum mass and cost at the turning point placed at 6.2 kW.Also, it can be noticed that the total mass of powertrains 1BC, 2BC, and 3BC is imposed by the fuel cell system mass, including the hydrogen tank.From the three architectures, 1BC presents the minimum mass.Regarding the cost, and due to the reduced number of power converters, propulsion system 1BC is the cheapest.The fuel cell power limit affected by the different battery technologies is the lower one, L inf (see Figure 14a), which is the reason that only the cost, mass, and volume of the PDSs using batteries as the only secondary energy source are affected, as shown in Table 7. Architectures 1BC, 2BC, and 1C2 are not affected since their optimal mass, volume, and cost are calculated with a fuel cell maximum power different from the lower limit (L inf ).
Figure 14a shows, for the four different battery technologies, the normalized battery mass along with the lower power limit.Depending on the L inf power limit, the amount of energy that the secondary energy source must be able to supply is modified (Table 8), and also their total required mass, as Figure 14b shows.The L inf and L upp power limits (yellow dots in Figure 14) represent the values of maximum power delivered by the fuel cell in which the optimal design changes the combination of secondary energy sources: that is, it changes from one region to another, e.g., using battery and supercapacitors instead of only battery, or using only supercapacitors instead of battery and supercapacitor [23].Table 8.Maximum power limit delivered by the fuel cell for the optimal design of the 1B architecture, and energy delivered by the battery using lithium-ion, lead-acid, nickel-metal hydride, and nickel-cadmium technologies.The batteries with a larger relation between energy density and power density, in addition to bringing forward lower Linf (Figure 14a), require a lower secondary power source total mass for the same load requirements (Figure 14b).That is, with fewer kilograms of battery, more energy is supplied.

Bat
Table 7 shows that the total mass of powertrain 1B increases as the ratio of energy density to power density in the battery becomes lower, except for lead-acid ones.The reason for this exception is that, in the lead-acid battery technology, Linf of the fuel cell for the designed architectures is very high at 5 kW (see Figure 14a), which means that the battery manages significantly less energy (Table 8), and, therefore, its mass decreases, as can be seen in Figure 15a.Regarding the overall cost of the 1B architecture, two aspects must be taken into account when different battery technologies are applied: the fuel cell maximum power along with the power density of the technology, and the price per kWh of each technology.It is observed that the higher cost is The batteries with a larger relation between energy density and power density, in addition to bringing forward lower L inf (Figure 14a), require a lower secondary power source total mass for the same load requirements (Figure 14b).That is, with fewer kilograms of battery, more energy is supplied.
Table 7 shows that the total mass of powertrain 1B increases as the ratio of energy density to power density in the battery becomes lower, except for lead-acid ones.The reason for this exception is that, in the lead-acid battery technology, L inf of the fuel cell for the designed architectures is very high at 5 kW (see Figure 14a), which means that the battery manages significantly less energy (Table 8), and, therefore, its mass decreases, as can be seen in Figure 15a.The batteries with a larger relation between energy density and power density, in addition to bringing forward lower Linf (Figure 14a), require a lower secondary power source total mass for the same load requirements (Figure 14b).That is, with fewer kilograms of battery, more energy is supplied.
Table 7 shows that the total mass of powertrain 1B increases as the ratio of energy density to power density in the battery becomes lower, except for lead-acid ones.The reason for this exception is that, in the lead-acid battery technology, Linf of the fuel cell for the designed architectures is very high at 5 kW (see Figure 14a), which means that the battery manages significantly less energy (Table 8), and, therefore, its mass decreases, as can be seen in Figure 15a.Regarding the overall cost of the 1B architecture, two aspects must be taken into account when different battery technologies are applied: the fuel cell maximum power along with the power density of the technology, and the price per kWh of each technology.It is observed that the higher cost is Regarding the overall cost of the 1B architecture, two aspects must be taken into account when different battery technologies are applied: the fuel cell maximum power along with the power density of the technology, and the price per kWh of each technology.It is observed that the higher cost is obtained by using Ni-MH battery technology due to its high mass and price, while the lower cost is obtained by using lead-acid battery technology (Figure 15b) due to its reduced mass.
Finally, it can be concluded that battery technology has a high influence on the total mass, volume, and cost of PDSs that only implement batteries as secondary energy sources.The lower the ratio of the energy density to the power density of the battery, the higher the power limit L inf .Consequently, the use of more powerful fuel cells implies the selection of batteries that manage less energy, and, therefore, its total mass is lower.The battery technologies that provide PDSs with higher total mass, in ascending order, are lead-acid, lithium-ion, nickel-metal hydride, and nickel-cadmium (see the yellow dots in Figure 15a).Similarly, in ascending order, the technologies that provide the most expensive power distribution systems are lead-acid, nickel-cadmium, lithium-ion, and nickel-metal hydride (see the yellow dots in Figure 15b).The amount of energy that manages the battery in each case is significantly different, as seen in Table 8, since the optimal design is found for a different fuel cell maximum power.

Influence of the Battery State-of-Charge Variation
Finally, this section evaluates the influence of the allowed maximum battery state-of-charge variation on the optimal design of each group of PDSs.
L inf is the only fuel cell power limit affected by the variations of the state-of-charge of the batteries (Figure 16a), and the reason is that only the optimal cost, mass, and volume of the batteries are affected in powertrains using batteries as the only secondary energy source.The total mass of the secondary sources is shown in Figure 16b for when the variation in the state-of-charge of the battery is 50% and 75%.It can be concluded that the larger the allowed variation in the state-of-charge, the lower the value of L inf , and the lower the mass of the secondary energy sources.
obtained by using Ni-MH battery technology due to its high mass and price, while the lower cost is obtained by using lead-acid battery technology (Figure 15b) due to its reduced mass.
Finally, it can be concluded that battery technology has a high influence on the total mass, volume, and cost of PDSs that only implement batteries as secondary energy sources.The lower the ratio of the energy density to the power density of the battery, the higher the power limit Linf.Consequently, the use of more powerful fuel cells implies the selection of batteries that manage less energy, and, therefore, its total mass is lower.The battery technologies that provide PDSs with higher total mass, in ascending order, are lead-acid, lithium-ion, nickel-metal hydride, and nickel-cadmium (see the yellow dots in Figure 15a).Similarly, in ascending order, the technologies that provide the most expensive power distribution systems are lead-acid, nickel-cadmium, lithium-ion, and nickelmetal hydride (see the yellow dots in Figure 15b).The amount of energy that manages the battery in each case is significantly different, as seen in Table 8, since the optimal design is found for a different fuel cell maximum power.

Influence of the Battery State-of-Charge Variation
Finally, this section evaluates the influence of the allowed maximum battery state-of-charge variation on the optimal design of each group of PDSs.
Linf is the only fuel cell power limit affected by the variations of the state-of-charge of the batteries (Figure 16a), and the reason is that only the optimal cost, mass, and volume of the batteries are affected in powertrains using batteries as the only secondary energy source.The total mass of the secondary sources is shown in Figure 16b for when the variation in the state-of-charge of the battery is 50% and 75%.It can be concluded that the larger the allowed variation in the state-of-charge, the lower the value of Linf, and the lower the mass of the secondary energy sources.Table 9 shows the mass, volume, and cost of the electric power distribution systems 1B, 1BC, and 1C2 for the ECE-15 driving profile when the variation in the state-of-charge of the battery is 50% and 75%.Table 9 shows the mass, volume, and cost of the electric power distribution systems 1B, 1BC, and 1C2 for the ECE-15 driving profile when the variation in the state-of-charge of the battery is 50% and 75%.A lower variation in the state-of-charge implies higher maximum power delivered by the fuel cell, that is, an increase in the lower limit Linf of maximum power delivered by the fuel cell (Figure 16a).As a result of the increase in the maximum power delivered by the fuel cell, there is an increase in the mass of the fuel cell itself, an increase in the mass of the converters, and a reduction in the total mass required from secondary energy sources.In particular, if powertrain 1B is analyzed, a decrease in the allowed variation in the state-of-charge in the battery involves reducing the mass of the battery itself, along with an increase in the mass of the fuel cell system and the converters.As the mass reduction of the battery is greater than the mass increment of the fuel cell system along with the converters, architecture 1B shows a lower value of its total mass when the variation in the state-ofcharge is lower (Figure 17a).The influence of varying the state-of-charge of the battery on the overall volume of the architectures is analogous to the influence owing to the mass.
Regarding the cost, it can be seen in Table 9 that the lower the maximum variation in the stateof-charge of the battery, the higher the overall cost of the PDS.In Figure 17b, it is verified that a smaller allowed variation in the state-of-charge of the battery implies a higher value of Linf, which is the lower limit of the maximum power of the fuel cell for the proposed electric power distribution systems.Therefore, a lower variation in the state-of-charge of the battery causes a lower cost of the battery and higher cost of the converter and fuel cell system.The increase in the cost of the converter and of the fuel cell system is more significant than the decrease in the battery cost, because the overall cost of the electric power distribution system increases when a smaller state-of-charge of the battery is allowed.The conclusion is that the variation in the state-of-charge of the batteries affects fundamentally the architectures that implement only batteries as a secondary energy source.A greater variation in the state-of-charge implies higher secondary energy source total mass, a higher PDS mass, as well as The conclusion is that the variation in the state-of-charge of the batteries affects fundamentally the architectures that implement only batteries as a secondary energy source.A greater variation in the state-of-charge implies higher secondary energy source total mass, a higher PDS mass, as well as a lower design power limit of the fuel cell, L inf .These results are strongly dependent on the evolution of the price and the battery technology.

Conclusions
This paper analyzes, using the optimal sizing procedure described in [23] as a baseline, the influence of four different design factors on the size and cost of nine different propulsion systems based on the fuel cell, batteries and supercapacitors, and a pure battery vehicle.Also, it reviews an additional design factor presented in [28].All the analyses have been carried out considering a light vehicle of 800 kg when the driving cycle is applied during a working day of 8 h.The result of the analysis is the knowledge of how the main design factors affect the mass, volume, and cost of the optimal power distribution architectures, and how they can be considered in the design.
Regarding the influence of the driving profile, there are different power range limits suggested for the architectures based on batteries, batteries and supercapacitors, or supercapacitors to optimize mass, cost, and volume.However, the optimal power distribution architectures are the same and independent of the applied driving profile.These optimal PDSs are 1B, 1BC, and 1C2.Also, in the case where the energy and power delivery by the battery and the supercapacitors in the 1BC architecture cannot be controlled independently, the 1BC architecture can be replaced by the 2BC architecture.A more detailed explanation can be found in [28].
Attending to the influence of the minimum power delivered by the fuel cell, as the minimum fuel cell power increases, the power range limits are shifted toward lower power values since the amount of energy that the fuel cell delivers is bigger.The size and cost of the architectures based on batteries and supercapacitors based on only supercapacitors decrease as the minimum delivered power by the fuel cell increases.The preferred power distribution architectures, 1B, 1BC, and 1C2, are the same and independent of the minimum energy delivered by the fuel cell.
The storage of the energy from the regenerative braking periods throughout a working day (8 h) also affects the PDS design.It can be remarked that as the fuel cell maximum power increases, the net amount of energy delivered by the secondary energy sources decreases.Therefore, there is a maximum fuel cell power beyond which the net amount of energy becomes negative.That is, the energy recovered from the braking periods is larger than the energy delivered by the secondary energy sources to fulfill the load demand that the fuel cell cannot.This consideration modifies the recommended architectures for the highest fuel cell maximum power range (P > L upp ), dismissing those architectures that are based on only supercapacitors as a secondary energy source, and suggesting the use of architectures with secondary energy sources implemented using only batteries.On the other hand, for the lower fuel cell power level, the recommended architectures are still the same: for P < L inf , the use of only batteries as a secondary source is suggested, while, for L inf < P < L upp , the recommended secondary source combines the use of supercapacitors and batteries.As a conclusion, for this case, the final suggested recommendation is the use of architecture 1B at 2.5 kW with the objective of minimizing the cost, or at 10 kW with the objective of minimizing the mass, and architecture 1BC at 6.2 kW.
The battery technology has a high influence on the total mass, volume, and cost of PDSs that only implement batteries as a secondary energy source.The lower the ratio of the energy density to the power density of the battery, the greater the power limit L inf .Consequently, the use of more powerful fuel cells implies the selection of batteries that manage less energy, and, therefore, its total mass is lower.The battery technologies that provide PDSs with higher total mass, in ascending order, are lead-acid, lithium-ion, nickel-metal hydride, and nickel-cadmium.Similarly, in ascending order, the technologies that provide the most expensive power distribution systems are lead-acid, nickel-cadmium, lithium-ion, and nickel-metal hydride.
Finally, the variation in the state-of-charge affects those architectures that implement only batteries as secondary energy sources.A greater variation in the state-of-charge implies, for the 1B architecture, higher secondary energy source total mass, a higher PDS mass, as well as a lower design power limit of the fuel cell, L inf .In any case, these results are strongly dependent on the evolution of the price and the battery technology.

Figure 4 .
Figure 4. Fuel cell-delivered power: a minimum value of 400 W and maximum value of 4.7 kW for the ECE-15 profile applied to a light vehicle.

Figure 5 .
Figure 5. Influence of the fuel cell (FC) minimum power on the normalized battery mass: (a) FC minimum power of 0 W. (b) FC minimum power of 200 W. (c) FC minimum power of 400 W.

Figure 4 .
Figure 4. Fuel cell-delivered power: a minimum value of 400 W and maximum value of 4.7 kW for the ECE-15 profile applied to a light vehicle.

Figure 4 .
Figure 4. Fuel cell-delivered power: a minimum value of 400 W and maximum value of 4.7 kW for the ECE-15 profile applied to a light vehicle.

Figure 5 .
Figure 5. Influence of the fuel cell (FC) minimum power on the normalized battery mass: (a) FC minimum power of 0 W. (b) FC minimum power of 200 W. (c) FC minimum power of 400 W.

Figure 5 .
Figure 5. Influence of the fuel cell (FC) minimum power on the normalized battery mass: (a) FC minimum power of 0 W. (b) FC minimum power of 200 W. (c) FC minimum power of 400 W.

Figure 6 .
Figure 6.Influence of the fuel cell minimum power the power distribution system (PDS): (a) Mass, (b) Volume.(c) Cost.

Figure 7 .
Figure 7. Battery, fuel cell system, and DC-DC converter mass evolution depending on the maximum power delivered by the fuel cell in architecture 1B.

Figure 6 .
Figure 6.Influence of the fuel cell minimum power the power distribution system (PDS): (a) Mass, (b) Volume.(c) Cost.

Figure 6 .
Figure 6.Influence of the fuel cell minimum power the power distribution system (PDS): (a) Mass, (b) Volume.(c) Cost.

Figure 7 .
Figure 7. Battery, fuel cell system, and DC-DC converter mass evolution depending on the maximum power delivered by the fuel cell in architecture 1B.

Figure 7 .
Figure 7. Battery, fuel cell system, and DC-DC converter mass evolution depending on the maximum power delivered by the fuel cell in architecture 1B.

Figure 8 .
Figure 8. Analysis of every architecture depending on the fuel cell maximum power for a minimum fuel cell power of 400 W. (a) Mass.(b) Volume.(c) Cost.

Figure 8 .
Figure 8. Analysis of every architecture depending on the fuel cell maximum power for a minimum fuel cell power of 400 W. (a) Mass.(b) Volume.(c) Cost.

Figure 9 .
Figure 9. Demanded power by the load along one ECE-15 driving cycle.

Figure 9 .
Figure 9. Demanded power by the load along one ECE-15 driving cycle.

Figure 11 .
Figure 11.1B architecture cost and mass in the lowest design power range for the ECE-15 profile.

Figure 10 .
Figure 10.Normalized battery mass, considering the maximum energy delivered from the secondary energy sources during a driving cycle, as well as the storage of the energy from the regenerative braking periods, for the ECE-15 driving cycle.

Figure 10 .
Figure 10.Normalized battery mass, considering the maximum energy delivered from the secondary energy sources during a driving cycle, as well as the storage of the energy from the regenerative braking periods, for the ECE-15 driving cycle.

Figure 11 .
Figure 11.1B architecture cost and mass in the lowest design power range for the ECE-15 profile.

Figure 11 . 22 Figure 12 .
Figure 11.1B architecture cost and mass in the lowest design power range for the ECE-15 profile.

Figure 12 .
Figure 12. 1B architecture cost and mass in the highest design power range for the ECE-15 profile.

Figure 14 .
Figure 14.Mass of the battery and the secondary sources when lithium-ion, lead-acid, nickel-metal hydride, and nickel-cadmium batteries are used, considering the same vehicle with the ECE-15 driving profile and a variation in the state-of-charge of 75%.(a) Normalized battery mass.(b) Total mass of secondary energy sources.

Figure 15 .
Figure 15.The fuel cell system and the converter of powertrain 1B with different battery technologies, with a variation in the state-of-charge of 75%, when the ECE-15 driving profile is applied.(a) Mass.(b) Cost.

Figure 14 .
Figure 14.Mass of the battery and the secondary sources when lithium-ion, lead-acid, nickel-metal hydride, and nickel-cadmium batteries are used, considering the same vehicle with the ECE-15 driving profile and a variation in the state-of-charge of 75%.(a) Normalized battery mass.(b) Total mass of secondary energy sources.

Figure 14 .
Figure 14.Mass of the battery and the secondary sources when lithium-ion, lead-acid, nickel-metal hydride, and nickel-cadmium batteries are used, considering the same vehicle with the ECE-15 driving profile and a variation in the state-of-charge of 75%.(a) Normalized battery mass.(b) Total mass of secondary energy sources.

Figure 15 .
Figure 15.The fuel cell system and the converter of powertrain 1B with different battery technologies, with a variation in the state-of-charge of 75%, when the ECE-15 driving profile is applied.(a) Mass.(b) Cost.

Figure 15 .
Figure 15.The fuel cell system and the converter of powertrain 1B with different battery technologies, with a variation in the state-of-charge of 75%, when the ECE-15 driving profile is applied.(a) Mass.(b) Cost.

Figure 16 .
Figure 16.Identification of the optimal design power range for each group of architectures, depending on the variation in the state-of-charge of the battery.(a) Normalized battery mass.(b) Total mass of secondary energy sources.

0Figure 16 .
Figure 16.Identification of the optimal design power range for each group of architectures, depending on the variation in the state-of-charge of the battery.(a) Normalized battery mass.(b) Total mass of secondary energy sources.

Figure 17 .
Figure 17.Evolution of the mass and the cost of the battery of the fuel cell system and the converters of electric power distribution system 1B, with variations in the state-of-charge of the battery of 50% and 75% for the ECE-15 driving profile.(a) Battery mass.(b).Battery cost.

Figure 17 .
Figure 17.Evolution of the mass and the cost of the battery of the fuel cell system and the converters of electric power distribution system 1B, with variations in the state-of-charge of the battery of 50% and 75% for the ECE-15 driving profile.(a) Battery mass.(b).Battery cost.
Figure 1.Power distribution architectures based on the fuel cell, supercapacitors, and battery [23].

Table 2 .
Power range limits for the analyzed European driving profiles.

Table 2 .
Power range limits for the analyzed European driving profiles.

Table 3 .
Influence of the fuel cell minimum power on PDS mass for the ECE-15 profile.

Table 4 .
Influence of the fuel cell minimum power on PDS volume for the ECE-15 profile.

Table 4 .
Influence of the fuel cell minimum power on PDS volume for the ECE-15 profile.

Table 5 .
Influence of the fuel cell minimum power on PDS cost for the ECE-15 profile.

Table 5 .
Influence of the fuel cell minimum power on PDS cost for the ECE-15 profile.Energies 2018, 11, x 9 of 22

Table 4 .
Influence of the fuel cell minimum power on PDS volume for the ECE-15 profile.

Table 5 .
Influence of the fuel cell minimum power on PDS cost for the ECE-15 profile.

Table 9 .
Mass, volume, and overall cost of the electric power distribution systems selected from each group of architectures, with variations in the battery charge state of 50% and 75%, for the ECE-15 driving profile.