Analysis of Control Strategies for a 3 Phase 4 Wire Topology for Transformerless Solar Inverters W.-Toke Franke, Claudia Kürtz, Friedrich W. Fuchs Institute of Power Electronics and Electrical Drives Christian-Albrechts-University of Kiel Kaiserstr. 2 24143 Kiel, Germany Phone: +49 431 8806106 Fax: +49 431 8806103 Email: tof@tf.uni-kiel.de, fwf@tf.uni-kiel.de URL: http://www.tf.uni-kiel.de Abstract—Three different current control strategies including P+Resonant controller, PI-controller in dq0-reference frame and hysteresis controller for a three-phase-four-wire solar inverter are investigated and compared concerning their influences on the leakage current at the solar array, the grid harmonics, the step response and the resulting power losses in the power devices. I. I NTRODUCTION During the last years many topologies of solar inverters have been proposed [1]–[5]. In general, they can be classified into topologies with and without a transformer. The advantages of the transformerless topologies are higher efficiency and less volume which are the reasons to select these topologies for the marked. However, the lack of the transformer also leads to some drawbacks: The main problems are the leakage currents between the solar panel and earth. These leakage currents are a risk for humans touching the panel.Another point is that for many solar systems the output voltage of the solar array is smaller than the required DC link voltage. The voltage can easily be boosted by a transformer [6]. In case of a transformerless topology the voltage has typically to be boosted by a DC-DC converter. Because of the leakage current at the PV arrays, typically three single phase converters are connected in parallel to achieve the three phase grid connection. In case that a three phase topology is applied, it is essential for low leakage current to connect the midpoint of the DC link to neutral (earth). Typically, the neutral point clamped (NPC) and the voltage source inverter with split capacitors and earthed midpoint are used [4]. In this paper the three phase four wire topology is proposed and analysed. The fourth wire that connects the midpoint of the DC-link to neutral leads to three independent phases which have to be controlled individually. For that purpose, three different control strategies are proposed and investigated concerning their influence on grid harmonics, leakage current, efficiency of the inverter and step response. The paper is structured as following: In section II the system is described. In the next section the investigated control strategies are proposed. In sections IV and V simulation and experimental results are presented. In the last section there is a conclusion. 978-1-4244-6391-6/10/$26.00 ©2010 IEEE Figure 1. Solar inverter with earthed dc link midpoint Table I E XEMPLARY ELECTRICAL DATA OF THE PV ARRAY open circuit voltage max. MPP voltage MPP range max. Power 1000 V 800 V 500 - 800 V 5 kW II. S YSTEM D ESCRIPTION The variable output voltage of the PV array is fed to the grid by the inverter topology given in figure 1. The system is based on a PV array with the data given in table I. However the results are also valid for other PV arrays. It consists of a voltage source inverter (VSI) and a boost converter (BC) in the DC link to cover the whole voltage range of the solar array. The MPP tracking is realized by both the BC for low and by the VSI for high input voltages. The connection to the grid is realized via an LCL filter. Special about this topology is the fourth wire which connects the midpoint of the split DC capacitors with the neutral phase of the grid. The advantage of the fourth wire is a great reduction of the leakage current at the PV array that arises due to the variation of the dc link potential to ground generated by the switching pattern. Assuming that the grid is y-connected the midpoint of the DC link has four different potentials to ground during one switching period. During one of the two zero-states all three phases of the grid are short circuited by having all upper devices conducting and the lower ones blocking or vice versa. In this state the upper or lower rail of the DC link is connected to ground 658 so that the midpoint of the DC link is at ± VDC 2 . During the active states one device of each phase is conducting whereas at least one of them is in the upper half and one is in the lower half. In case that two upper devices and one lower device are conducting two phases are switched in parallel and connected to the upper DC link rail. Thus the voltage drop across the upper DC link rail of the load is only half of the voltage drop of the phase that is connected to the lower DC link rail. That leads to a midpoint voltage of the dc link to ground VDC of − VDC 6 and to 6 in case that two devices in the lower half are conducting. The reduction of the leakage current by connecting ground and the midpoint of DC link is given by CPV the factor of 2C . However the fourth wire also leads to two DC √ drawbacks. The first is that the DC link voltage has to be 2/ 3 higher than for the system without the fourth wire to deliver the same grid voltage. The second issue is that the widely used current control strategy in rotating dq-reference frame is not feasible since the three phases are independent. In the next section three suitable current control strategies are proposed and compared concerning their influence on the efficiency, the harmonic distortion and leakage current at the PV array to each other. The LCL filter is designed according to [7]. 1 After the PI control block the signal is inverse transferred for the PWM generation by 1 ! r √ 1 0 2 2 i1 cos θ − sin θ 0 id √ 2 3 1 1 √ −2 i2 = sin θ cos θ 0 iq . (3) 2√ 2 2 3 − 1 − 3 √1 i3 0 0 1 i0 2 2 2 2 Figure 2 shows the control structure. The DC link voltage is controlled by a PI controller. The output of the DC link voltage controller is the d-component for the current controller. The q- and 0-component are set to zero for this investigations. The inverter states are generated by a sine-triangular PWM. G1 2 C2 G2 C3 G3 DC DC2 3 f1-3 DC d q 0 0 q d Figure 2. frame III. C URRENT C ONTROL S TRATEGIES The current control strategies can be divided into linear and non-linear approaches. Since the investigated topologies consist of a three phase four wire system, the most promising linear control schemes are the control in dq0-reference frame and the resonant control, where every phase is controlled individually. As a non-linear control technique the hysteresis controller is investigated. For both linear control strategies the same method for generating the PWM pulses can be applied. In contrast the hysteresis control delivers directly the pulse pattern. A. PI Current Control in dq0-Reference Frame The standard PI controller in the form of 1 GPI = KP + KI · (1) s has an infinite open loop gain at 0 Hz. For that reason the steady state error can only be eliminated for DC signals. On account of this the AC signals have to be transferred into DC signals in a rotating reference frame by 1 −1 −1 ! r i1 id √2 √2 2 cos θ sin θ 0 3 − sin θ cos θ 0 i2 iq = 0 − 23 (2) 2 √1 √1 √1 3 0 0 1 i3 i0 2 2 2 C1 DC1 Control structure of the PI current controller in dq0 reference Figure 3. P-resonant controller Figure 4. Frequency response characteristic of the open loop p-resonant controller B. Resonant Control The resonant controller is a generalized PI controller that is able to control not only DC but also AC variables. Figure 3 shows the structure of the resonant controller according to [3], [8]–[10]. In addition to a forward integrator there is another integrator in the feedback loop. The transfer function is given by s . (4) GPR = KP + KI · 2 s + ω20 Figure 4 shows the bode diagram of the resonant controller for a resonance frequency of 50 Hz. At 50 Hz there is an infinite open loop gain and thus it is able to eliminate the steady state error at this frequency. If ω would be zero the resonant controller has the same structure as the well known PI controller. 659 Figure 5. Functionality of the hysteresis control 1 Figure 7. Leakage current reduction by connecting the midpoint to earth (top), leakage current with the fourth wire connencted (bottom) 2 A. Leakage Currents 3 1 Figure 6. 2 3 Control structure of the hysteresis controller The control structure is similar to that of the PI control in dq0-reference frame in figure 2. Only the current PI controller is substituted by the P-resonant controller and therefore the output signal of the voltage controller is transferred into the abc-reference frame. The outputs of the current controller can now directly be transferred to the PWM unit. C. Hysteresis Control In this investigation a standard hysteresis controller with variable frequency is used. Therefore for each phase a tolerance band of a given amplitude 2h is allocated around the phase current. If the phase current exceeds the tolerance band the converter switches its state into the opposite direction. This functionality can be seen in figure 5. Since the amplitude of the tolerance band is given and because the sinusoidal grid voltage leads to a variable counter voltage and thus to a variable gradient of the current, the switching frequency depends on the actual value of the grid voltage. To achieve the same average switching frequency fs,av in the nominal operating point as for the other control strategies the magnitude of the tolerance band h is adjusted by [11]: VDC Mn2 2h = 1− (5) 4 · LC · fs,av 2 There Mn is the modulation index in the nominal operating point. IV. S IMULATION R ESULTS AND C OMPARISON All three control strategies have been investigated by simulation with MATLAB Simulink and Plecs. The power circuit is implemented in Plecs for a detailed analysis of the leakage current and power losses. For the simulation the same parameters are used as for the experimental setup, given in table II. Before comparing the different control methods to each other a simulation shall clarify, how the leakage currents are reduced by the split DC capacitors C3 = C4 = 1000µF. Therefore, a simulation test with and without earthed midpoint is done for a parasitic solar array capacity of 150 nF for 1 kW according to [5]. The results are given in figure 7 for the P+resonant controller, where the fourth wire is connected at 50 ms to ground. However the results look similar for the other control strategies. Without the fourth wire the leakage currents rise up to a value of 5 A whereas it is reduced to about 1.5 mA (Fig. 7 bottom) when the fourth wire is connected to the midpoint of the split capacitor. The current ripple is 20 kHz. B. Influence on Grid Harmonics To clarify the influence of the proposed control strategies on grid harmonics the resulting grid currents have been analyzed. For this purpose a sinusoidal reference voltage replaces the grid in simulation. In the case that an ideal sinusoidal waveform is used no harmonics greater than 0.1% show up. Figure 8 shows the harmonic spectrum when a non ideal sinusoidal waveform is utilized. Here on each of the third, fifth and seventh harmonic a disturbance of 1.5% is superimposed. The red stems describe the maximum allowed harmonics concerning DIN VDE 0126-1-1. The P-resonant control performs similar to the PI control in dq0-reference frame. Both control methods slightly amplify the given harmonics. No other harmonic numbers appear. With the hysteresis control the given harmonics are attenuated but other harmonic numbers are added even though they are only insignificant. C. Step Response for Optimal Control Parameters Figure 9 displays the step responses to a step of the DC link power. Here, the d-component of the output current is depicted, whereas the value is normalized to 1. Therefore the output currents are transferred in dq0-reference frame for measurement reasons. Comparing the time period until the system is in steady state, both the PI controller in dq0reference frame as well as the P+resonant controller take 4 ms 660 a) b) c) Figure 8. Harmonics current spectrum with a disturbed grid voltage (1.5 % of the 3rd, 5th and 7th added) for a) PI controller in dq0 reference frame; b) P-resonant controller; c) hysteresis controller 1.5 1 0.5 0 −0.5 0.01 0.015 0.02 t in s 0.025 0.03 1.5 1 Figure 10. 0.5 Efficiency of the inverter with different control strategies 0 −0.5 0.01 0.015 0.02 t in s 0.025 0.03 Figure 9. Step responses top: PI control in dq0 reference frame, middle: P+resonant, bottom: hysteresis due to the LCL filter. Applying the hysteresis controller the overshoot subsides after approximately 1.5 ms. After that there is some ringing for another 4 ms. The faster step response results in a higher overshoot of the current of 55%. Whereas the p-resonant controller only has 25% and the PI control in dq0-reference frame has even less with 22%. D. Power losses and Efficiency To demonstrate the efficiency of the analyzed control structures it is simulated at different input power. Therefore the DC link voltage is kept constant at 800 V and the input current is adjusted between 0.625 A and 6.25 A. The examined power losses are the conducting and switching power losses of the IGBTs and diodes. They were simulated by means of a thermal simulation in Plecs. Therefore the switching and conducting losses were measured on a real device at different temper- atures, blocking voltages and currents [12]. After that, these results have been implemented in the Plecs model. The results are presented in figure 10 and show promising values between 94, 5% and 97.6% depending on the current and control strategy. The highest efficiency is achieved by the hysteresis controller since the highest switching frequency occurs when the magnitude of sinusoidal output current is at its minimum. For the maximum current only low switching frequencies occur. The two linear control methods show very similar efficiencies because both lead to the same PWM-pattern. Due to the constant switching frequency their efficiency is lower than for the hysteresis control. Here, some improvements may be achieved by applying a discontinuous PWM method by injecting the third harmonic. This will lead to a 50% reduction of the switching losses since the highest current carrying IGBT is turned on permanently for 1/6 switching period [13]. V. E XPERIMENT R ESULTS For the experimental results a three phase four wire VSI inverter has been built up on PCB (figure 11). The focus was on a circuit with lowest stray inductances to enable high switching frequencies and short turn-on and turn-off times. The output filter is an LCL filter designed concerning to [7]. The input voltage is delivered by a solar simulator that is on the one hand able to produce a fixed DC voltage and on the other hand can deliver a current and voltage according to a given V/I-characteristic of a solar array. The control of the inverter is realized on a TriCore µ-controller from Infineon Technologies. The significant parameters of the experimental setup are given in table II. 661 Figure 11. Experimental solar converter setup: PCB of the converter, measurement unit and LCL filter bottom Figure 12. Solar inverter, control in dq reference frame: DC-link voltage 100 V/div (Ch 1), AC contents of the voltage across CPV (Ch 2) grid current 5A/div (Ch 3) and leakage currents 200 mA/div (Ch 4) Table II PARAMETERS OF THE EXPERIMENTAL SETUP Input voltage Input power DC-link Capacitance Semiconductors Switching frequency Converter side inductor Grid side inductor Filter capacitor 500 - 1000 V 5000 W 660 µF IKW08T120 20 kHz three powder cores 2.6 mH laminated steel 0.5 mH 4.4 µF A. Leakage Currents Figures 12, 13 and 14 show the leakage current through a 450 nF capacitor connected to ground for the control in dq0-reference frame, the P+resonant control and the hysteresis control, respectively. The output current in each phase is 5 Arms . The leakage current consists of a ringing of 200 mA for operating with the linear control strategies and about 100 mA for the hysteresis controller. The rms values are 78.8 mA, 81.3 mA and 43.1 mA, respectively and therefore well below the allowed 300 mA concerning VDE 0126-14-2. Compared to the simulation results the leakage current is significant higher. The reason is that in the simulation ideal capacitors for the DC link are applied. For the experimental test the DC link consists of electrolyte capacitors with not negligible parasitic inductances and resistances, while for CPV a film capacitor with much lower parasitic effects is used. This leads to higher equalizing current through this path. It is expected that for real solar arrays the leakage current is lower. Figure 13. Solar inverter, P+resonant controller: DC-link voltage 100 V/div (Ch 1), AC contents of the voltage across CPV (Ch 2) grid current 5A/div (Ch 3) and leakage currents 200 mA/div (Ch 4) has switching frequency that is between 2.5 kHz and 30 kHz and therefore not visible in the first 40 harmonics. The THD is calculated to 1.2 % for the first 40 harmonics and to 7.7 % for the total spectrum. C. Efficiency The measured power losses for all proposed control strategies are shown in figure 16. The efficiency is calculated from the measured input and output power of the inverter that is done by the DEWETRON 2010. Its power accuracy is B. Harmonic spectrum The measured harmonic spectra for the three control strategies are given in figure 15. It is obvious that the spectra for the current control in dq-reference frame and with the P+resonant controller have a similar appearance, since the same switching frequency, grid filter and pwm modulation are applied. The THD values are calculated to 3.074 % and 2.966 % for the current control in dq0 reference frame and for P+resonant controller, respectively. For the hysteresis controller for most frequencies the spectrum is smaller as for the other two control strategies, even though the current has much higher ringing as shown in figure 14. This is caused by the fact that the ringing Figure 14. Solar inverter, Hysteresis controller: DC-link voltage 100 V/div (Ch 1), AC contents of the voltage across CPV (Ch 2) grid current 5A/div (Ch 3) and leakage currents 200 mA/div (Ch 4) 662 controller leads to the lowest losses but depicts a wide harmonic spectrum due to the variable switching frequency. The behavior of the PI controller in dq0 reference frame and the P+Resonant controller show very similar results. Regarding the processing power of the µ-controller the P+Resonant controller has some advantages compared to the PI controller due to lack of the dq0-transformation. The switching losses for the linear control strategies can be reduced by applying loss optimized modulation strategies, which however will lead to higher harmonics in the grid current. ACKNOWLEDGMENT Figure 15. Harmonic current spectra of the investigated control strategies This work is sponsored by the Rainer Lemoine Stiftung (RLS). R EFERENCES Figure 16. Measured efficiencies with DEWE2010 determined to about 0.5 %. For both linear strategies the same results are achieved, since they lead to the same switching pattern. Due to the IGBTs with their current independent forward voltage drop and fix power losses caused by balancing resistors for the DC link capacitors, the efficiency is reduced for very low input power but increases up to 2.5 kW. After that it starts to decrease slightly. For the hysteresis controller the grid filter was changed to an L-filter with 4.5 mH, due to the ringing of the output current. Using damping resistors would lead to lower efficiency compared to the larger Lfilter. The power losses for the hysteresis control depend very much on the input power. The spectrum has shown that the average switching frequency increases with the reduction of the modulation index, leading to increasing switching losses. This also approves (5). For the input power above 2.5 kW the average switching frequency is already reduced to 5 kHz. This explains the better efficiency of the hysteresis controller compared to the other controllers. VI. 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