Keywords

1 Introduction

Nowadays, EVs are continuously increasing at higher rate for daily transportation purposes. According to the estimates and predictions, more than 125 million EVs will be on road by the year 2030 [1]. Lithium-ion (Li-ion) battery is the core of these innovative vehicles where it stores the energy [2]. Numerous aspects have worked to increase the penetration of renewable sources with EV charging. These aspects are greenhouse gases consequences on environment, continuously reducing PV module prices, rapid technical advancement in EVs [3]. Fuel cell (FC) and solar PV are the outmost capable renewable energy power producing mechanisms. FC has sluggish response and reaction that shall be compensated with super-capacitor bank or battery storage system [4]. Out of various renewable energy sources, FC has been attracting power source for engineers because of its cleanliness, high efficiency and profitable power source to consumers. The output of FC is DC in nature which can also be directly connected to the solar PV output, and it shall work as backup when standalone microgrid loads are considered [5, 6].

A microgrid system can be defined as an autonomous energy grid which shall operate independently or in parallel with conventional grid. Nowadays, the use of renewable energy resources (RER) integrated with microgrid is used across the world. In microgrid system, BESS is used as key component for stabilizing the voltage fluctuation. Mainly Li-on battery is used as storage system, but the lifetime of the Li-on battery is small for stable operation. Thus, to achieve long lifetime operation, a system for charging and discharging a battery is required [7,8,9,10]. The major obstruction in moving towards EV is time of recharge, battery size, instability of grid during peak load and inefficient power conversion. The above obstruction can be overcome by use of a system which has less dependency on the grid such as hybrid charging station. Therefore, more research is in practice by researcher and design engineer in the field of RERs connected EV charging system (EVCS) with a battery backup [11, 12]. The modelling of the battery can be classified into three major types. The first type is electrochemical modelling, and it gives high accuracy, but it is difficult to apply. The second type is mathematical modelling, and it can be applied in limited condition. The third and most common type is electrical modelling, and it is mainly used for implementing a battery in a charging system [13, 14].

There are two types of architecture used for charging stations, the first is AC architecture in which AC bus is used, and second is DC architecture in which DC bus is used [15, 16]. The general structure of DC bus architecture is represented in Fig. 1. In this architecture, energy sources are connected at one side of DC bus with the help of DC-DC converter, and another side of loads/charging EV is connected along with DC-DC converter. The converter used in the architecture is bidirectional DC-DC converters. Since last years, academicians and researchers have worked for EV charging methods, architectures and optimizations. Solar PV-based charging method is used for charging stations in [17,18,19]. Vehicle to grid method was proposed in [20] to sell energy back to grid, and same type of arrangement is described in [21] to inject excess energy to the grid. Paper [22] claims fast functioning outcomes and appropriate application at lower temperature, and reported FC is suitable for backup power with PV source. The architecture of fuel cell can be understood from paper [20]. The operation, control and performance of PV-FC hybrid system are demonstrated in [23]. A comparative study of AC and DC microgrid concept was reported in [24]. It is concluded that DC is more beneficiary because of safe operation, less power electronics (PE) conversion stages, no issues of reactive power control and high energy efficiency. PV-based energy management algorithm-based system is developed in [24]. The design of AC microgrid system also has some issues in synchronization along with frequency handling.

Fig. 1
figure 1

Microgrid architecture for charging station

Various converters have already been reported in literature for charging purposes in different architectures, i.e. Z-source converter, multilevel converters [25], single stage bidirectional DC-DC Z-source inverter [26], quasi Z-source bidirectional DC-DC converter [27] and grid tied neutral point clamped [25]. A paper has also reported T-source inverter for solar PV grid tied system [28] that can boost and buck the voltage according to required level with low output voltage ripple and input voltage along with easy control. A parallel three-level DC-DC converter with an integrated inductor was introduced for EV charging in [29, 30], but it has higher ripples due to high number of switching components, and three-phase hybrid boost converter was employed in [31] for same application that had less switching losses.

Above-mentioned converter had the drawbacks of slow dynamic response, reduced voltage gain because of discontinuous mode of operation, high number of elements that reducing reliability and increasing the switching losses, unable for bidirectional power flow, etc. Hence, the T-source inverter was employed that has less number of switches and conversion stages, fast dynamic response and high gain that motivated authors to work on this topology for EV charging. Various controlling schemes has also employed for control of converters in literature which are as; phase locked loop (PLL) based soft switching technique [32], phase disposition pulse width modulation (PD-PWM) [33], sliding mode control [34], SVPWM PI controller [35, 36] and a cascade two PI controller were used in residential buildings EV charging station [37] that had sluggish dynamic response and resulted in slow charging. Hereafter, getting these above-mentioned controllers, it was concluded that PI controller can filter noise and gives zero steady state error that mainly used in bidirectional control. This paper has also employed modified double PI controller for bidirectional T-source converter (TSC). TSC provides galvanic isolation for converter and loads that enhances voltage stability and power quality, and closed loop control gives lesser current ripples and current THD and gives high voltage gain with double PI controller.

2 Microgrid Arrangement

Fig. 1 shows that battery, solar PV and FC are used as source and TSC is used as DC/DC converter for getting the desired DC voltage level of grid. It has also used T-source bidirectional converter for charging and discharging purposes of EV and buffer battery (Fig. 2).

Fig. 2
figure 2

T-source DC-DC converter circuit diagram

2.1 T-Source Converter

The TSC is a bidirectional DC-DC converter. The circuit of TSC is designed by combination of T-network, LC filter and switch. The T-network is formed by connecting two inductors (L1 and L2) which are mutually coupled and a capacitor in T-shape [38]. This converter is able to provide chosen DC voltage without any dependency on source voltage changes as in solar PV output changes due to weather conditions. The circuit diagram of the TSC is shown in Fig. 3. Depending on the switching condition, TSC is operated in two modes. The first mode of operation is non shoot through (NST), while second is shoot through (ST), and the circuit diagram during these modes is shown in Fig. 4a, b, respectively.

Fig. 3
figure 3

TSC working modes. a NST mode, b ST mode

Fig. 4
figure 4

Switching scheme for TSC

During NST mode of operation, the switch S1 is on, while switch S2 is off. In this duration, energy is transferred from source side to load side, and output voltage varies according to switch (S1) duty ratio. Further, inductor of output side is energized, and input current charges the input capacitor. In ST mode, switch S1 and switch S2 both are in on state. During this duration, charge stored in capacitor C1 and capacitor C2 is transferred to inductor L2 and inductor L3, respectively.

The switching scheme for TSC is shown in Fig. 5, which is obtained from double PI control scheme. In double PI control scheme, both current and voltage are controlled, and hence, it contains very less ripples in output. Here, GS1 is gate pulse for the switch S1, GS2 is gate pulse for the switch S2, and ST is the shoot-through pulse signal. The duration for which the shoot-through pulse is low is the NST duration, and duration for which it is high is ST duration. The ST duration is the duration for which both the pulse signal GS1 and GS2 are high.

Fig. 5
figure 5

Double PI control algorithm for T-source DC/DC converter

The voltage across capacitors and inductors (assuming both inductor identical) is given in Eqs. (1) and (2), respectively. The voltage across capacitor and inductors is given as

$${V}_{C}={V}_{C1}={V}_{C2}$$
(1)
$${V}_{L}={V}_{L1}={V}_{L2}$$
(2)

During NST mode,

$$V_{L1} = V_{S} - V_{C1}$$
(3)
$${V}_{d}={V}_{C1}-{V}_{L2}=2{V}_{C1}-{V}_{S}$$
(4)

During ST mode, inductor voltage (VL) and S2 voltage (Vd) are as

$${V}_{d}=0$$
(5)
$${V}_{L2}={V}_{C1}$$
(6)

The switching time over a period is summation of the switching time of NST and ST time and given as shown in Eq. (7).

$$T= {T}_{nst}+{T}_{st}$$
(7)

By equating inductor voltage to zero over one cycle of period, the capacitor voltage is calculated and given by Eq. (8).

$${V}_{C1}=\left(\frac{{T}_{nst}}{{T}_{nst}-{T}_{st}}\right){V}_{S}=\left(\frac{1-D}{1-2D}\right){V}_{S}$$
(8)
$$V_{{{\text{om}}}} = \frac{1}{T}\mathop \smallint \limits_{0}^{T} V_{d} \left( t \right){\text{d}}t = \frac{{T_{st} .0 + T_{nst} \left( {2V_{CZ} - V_{S} } \right)}}{T}$$
(9)

The relation between duty ratio and output voltage is given by Eq. (10)

$$V_{oD} = \left( {\frac{{T_{nst} }}{{T_{nst} - T_{st} }}} \right)V_{S} = \left( {\frac{1 - nD}{{1 - D\left( {n + 1} \right)}}} \right)V_{S}$$
(10)

where D = TS/T is the shoot-through duty cycle ratio of converter.

2.2 Solar PV and Fuel Cell

The solar PV array is considered the most essential and prerequisite sustainable resource due to its free and abundant availability in the atmosphere. The solar power in the model mainly depends upon irradiance and ambient temperature. Solar cell radiation is measured by air mass, incident angle and radiation to measure cell power (S) given in Eq. 11 below:

The cell power is calculated by the help of Eq. (11)

$$\mathrm{S}=\mathrm{M}\left({G}_{b}{R}_{b} {(\tau \alpha )}_{b} \right)+ {G}_{d}{(\tau \alpha )}_{d}\frac{1+\mathrm{cos}\beta }{2}+ {G}_{pg}{(\tau \alpha )}_{g}\frac{1+ \mathrm{cos}\beta }{2}$$
(11)

Temperature and irradiance are two major factors on which solar power depends as given in Eq. (12).

$$T_{{{\text{mod}}}} = T_{{{\text{air}}}} + K_{{\text{T}}} G$$
(12)

Equation (13) gives the efficiency of cell

$$\eta_{{{\text{cell}}}} = \frac{{I_{\max } * V_{\max } }}{{P_{{{\text{in}}}} }}$$
(13)

The power output is given in Eq. (14) which is a function of temperature.

$$P = P\left( {S,T_{{{\text{mod}}}} } \right)$$
(14)

Equation (15) gives the cell output power in kWh.

$$P = \frac{{P_{{{\text{peak}}}} *S}}{1000}$$
(15)

FC is an electromechanical conversion device, in which electrical energy is produced from chemical energy with water and heat as by-products using H2 energy. In existing research, proton exchange membrane fuel cell (PEMFC) is used due to its low-temperature operation suitability and quick response. The output voltage and power of fuel cell are calculated by the help of the Eqs. (16) and (17), respectively.

$$V_{{{\text{FC}}}} = E - V_{{{\text{act}}}} - V_{{\Omega }} - V_{{{\text{con}}}}$$
(16)
$$P_{{{\text{FC}}}} = N* V_{{{\text{FC}}}} *I_{{{\text{FC}}}}$$
(17)

The efficiency of fuel cell is given by Eq. (18)

$$\eta_{{{\text{FC}}}} = \frac{{P_{{{\text{FC}}}} }}{{M_{{{\text{H}}_{2} }} {\text{HHV}}_{{{\text{H}}_{2} }} }}$$
(18)

Here, MH2 is flow rate of fuel, and PFC, IFC and VFC are FC power output and voltage. Nearly, a FC can yield 0.6–0.75 V, and the power and voltage level can fluctuate from 2 kW to 50 MW and a couple of volts to 10 kV [21], individually relying upon the connections and picked arrangements plan.

3 Simulation Model

The DC microgrid model was designed on MATLAB Simulink tool which has used solar PV, battery and FC as source along with TSC for connecting them to DC link of microgrid. The load or EV for charging was also connected to the DC link with bidirectional TSC. The double PI control scheme was designed for making it closed loop control with voltage and current of battery being charged. The outer voltage control loop regulates the voltage, and the inner loop ensures a ripple free charging current as shown in Fig. 6. Specification for TSC converter is given in Table 1. The battery was charged with each power source at different time, and once all the sources were used for charging the battery. The DC link voltage for microgrid was 48 V, and it is easy to connect each source with DC/DC converter with DC link. Battery used has the energy capacity of 100Ah with 48 V.

Fig. 6
figure 6

SOC variation of battery during charge (a) with SPV (b) with FC (c) with DC source

Table 1 Specifications of TSC converter

4 Result Analysis

The suggested architecture is designed according to Table 1 with different source of energy. Different sources connected to the battery along with TSC converter are discussed here, and charging performance is analysed in this section. The results obtained for state of charge (SOC) of the battery are represented in Fig. 7 in which Fig. 7a shows the result of battery with SPV source as an input, Fig. 7b shows the result of battery with FC as an input source and Fig. 7c shows the result of battery with DC source as an input. It is observed that battery is charged 0.007% (63.831–63.838%) in duration of 0.5 s (1.5–2.0) when connected with SPV source and is charged 0.005% (63.824–63.829%) in duration of 0.5 s (1.5–2.0) when connected with FC as an input source and charged 0.014% (63.851–63.856%) in duration of 0.5 s (1.5–2.0).

Fig. 7
figure 7

Current of battery during charge (a) with SPV (b) with FC (c) with DC source

The result obtained for current flowing through battery is represented in Fig. 7 in which Fig. 7a shows the result when SPV is connected as input source and the current flowing is 106.9 A, Fig. 7b shows the result when FC is connected as input source and current flowing is 107.5 A, and Fig. 7c shows the result when DC source is connected as input source and current flowing is 106.7 A.

The result obtained for voltage of battery is represented in Fig. 8 in which Fig. 8a shows the result when SPV is connected as input source and the voltage is 52.47 V, Fig. 8b shows the result when FC is connected as input source and the voltage is 52.28 V, and Fig. 8c shows the result when DC source is connected as an input source and the voltage is 53.19 V.

Fig. 8
figure 8

Voltage of battery during charge (a) with SPV (b) with FC (c) with DC source

5 Dynamic Response

The nature of renewable sources and load of the charging structure is variable as the charging vehicles at charging station possess connected/disconnected every time. Hence, it is important to find out the dynamic load checking of this converter. The TSC charging current is around 7–8% higher than conventional buck converter, when checked by comparing as shown in Fig. 9b. Higher gain offered due to impedance network of TSC is the reason behind higher charging current. The charging time reduces with TSC converter integrated charging arrangement as compared to other topologies as given in Table 2.

Fig. 9
figure 9

Dynamic response of TSC. a Charging voltage. b Charging current. c Step change in solar irradiance

Table 2 TSC converter comparison with other DC-DC converter topologies

Figure 9a depicts the TSC charging voltage which is marginally greater than conventional buck converter with less ripples. Switching stress on TSC converter will reduce comparatively by this approach. Charging voltage and current are shown in Fig. 9a, b, and step change response in irradiance from 800 to 600 w/m2 for buck and TSC is shown in Fig. 9c. The response time for TSC converter is around 50 ms, while buck converter has 250 ms which is five times higher. Figure 9c shows that at 0.42 s during step change of solar irradiance the response goes for smooth transition for both converters, but it is comparatively less in response of TSC.

6 Conclusion

Fast charging stations are the need of hour for increasing EV on the roads, and TSC converter has been found that it is an ideal converter with double PI controller for charging the EV. This converter provides constant current and voltage for battery charging with low THD, reduced number of switches, less ripple, high gain and fast charging. The designed DC microgrid is also helpful for the charging purposes where the grid availability is not available/possible. DC microgrid with RERs is designed and simulated for EV charging purpose at MATLAB Simulink platform. The charging SOC results with different source of supplies show that the results are satisfactory. The dynamic response is also presented in the study for better understanding, and the fast charging is claimed on the basis of higher charging current, so it will take less time to charge battery than conventional buck converter.