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Aalborg Universitet Controlled Inverters with Seamless Transition between Islanding and Grid Connected Operations Hu, ShangHung ; Kuo, ChunYi ; Lee, TzungLin; Guerrero, Josep M. Published in: Proceedings of the 3rd IEEE Energy Conversion Congress and Exposition (ECCE 2011) DOI (link to publication from Publisher): 10.1109/ECCE.2011.6064059 Publication date: 2011 Document Version Early version, also known as preprint Link to publication from Aalborg University Citation for published version (APA): Hu, SH., Kuo, CY., Lee, TL., & Guerrero, J. M. (2011). Controlled Inverters with Seamless Transition between Islanding and GridConnected Operations. In Proceedings of the 3rd IEEE Energy Conversion Congress and Exposition (ECCE 2011) (pp. 21962201 ). IEEE Press. https://doi.org/10.1109/ecce.2011.6064059 General rights Copyright and moral rights for the publications made accessible in the public portal are retained by the authors and/or other copyright owners and it is a condition of accessing publications that users recognise and abide by the legal requirements associated with these rights.? Users may download and print one copy of any publication from the public portal for the purpose of private study or research.? You may not further distribute the material or use it for any profitmaking activity or commercial gain? You may freely distribute the URL identifying the publication in the public portal? Take down policy If you believe that this document breaches copyright please contact us at vbn@aub.aau.dk providing details, and we will remove access to the work immediately and investigate your claim. Downloaded from vbn.aau.dk on: november 21, 2018

Controlled Inverters with Seamless Transition between Islanding and GridConnected Operations ShangHung Hu ChunYi Kuo TzungLin Lee Department of Electrical Engineering National Sun Yatsen University TAIWAN Email: tllee@mail.ee.nsysu.edu.tw Josep M. Guerrero Dept. Energy Technology Aalborg University DENMARK Email: joz@et.aau.dk Abstract This paper presents a seamless transition method for droopled inverters to operate in both islanding and gridconnected modes. A local PLL and a virtual inductance are designed to ride through transient when the inverter switches between two modes with no synchronization. The proposed method can cooperatively work with welldeveloped droop s so that the inverters are able to share load among them as well as subsist under transient events of the utility. Theoretical analysis and experimental results validate effectiveness of the proposed method. I. INTRODUCTION Inverterbased distributed power generation systems (DPGSs) have received much attention recently due to flexible powerling capability. Usually, the inverter with the gridfollowing is used to accomplish power conversion between the grid and DPGSs. However, this method may suffer from voltage stability, frequency variation, voltage harmonics, and cannot work in the islanding situation. Instead of the gridfollowing, the gridforming inverter is preferred because it is able to provide many ancillary services defined in IEEE Std. 1547[1], such as load regulation, reactive power compensation, and power quality improvement. In order to integrate various DPGSs into the utility, Microgrid[2] concept was presented to assure the system with high quality and high reliability in both gridconnected and islanding operations. In the islanding mode, frequencyand voltagedroop s are realized among inverters to share real power and reactive power in a decentralized fashion [3,4]. When going into the gridconnected mode, the inverter is led as a current source instead. Obviously, a coordinating system is definitely required to accomplish proper transition without undergoing transient current. led inverter has been presented to operate in both gridconnected and islanding modes. Acceptable steadystate performance can be accomplished, such as load sharing and voltage regulation. In case of mode transition, however, the inverter may undergo severe current transient, which might be large enough to trigger protection of the inverter due to low line impedance. Uility Z g STS R load E C f L f Figure 1. Circuit of the inverter connected to local load. V dc Virtual inductance concept was proposed to limit inrush current for plugin of the inverter [4]. However, transient current is still significant when the upcoming inverter is out of phase with the grid. This paper presents a seamless transition method for droopled inverters. Zerocurrent is proposed to suppress transient current due to asynchronous paralleling. Simultaneously, a local phaselockedloop (PLL) is designed to obtain the angle of the inverter output voltage for correcting the angle of voltage command in the droop. After that, the virtual inductance is realized to suppress inrush current coming from drooping operation of the inverter. Based on this algorithm, transient current between the inverter and the grid could be avoided even with no phasesynchronization used. The method could be further extended for inverterbased DPGSs to ride through powerquality events, such as voltage sag and swell. II. OPERATION PRINCIPLES Fig. 1 shows a droopled voltage source inverter intended to supply power to the local load as well as the utility. Circuit parameters are given in TABLE I. In this paper, a seamless transition method for riding through transient is proposed to allow inverters switching between the islanding and the gridconnected modes with no requirement of grid information. The stateoftheart droop will be presented first, followed by the ridingthrough algorithm. A. The overall of the inverter is shown in Fig. 2. When both SW 1 and SW 2 are at position 1, the inverter is operated in the droopled mode. This work is supported by National Science and Technology Program Energy of TAIWAN under grant NSC 992628E110009.

Ridingthrough mode E E qd s qd e qd s i ref i qd i qd E qd E qd i qd P&Q Calculation k pi P Q Activated signal Z(s) L v Virtual inductacne PLL LPF LPF qd s f E P Q ω s 1 E 2 θ 1 SW1 qd s E droop =E cos(θ) E droop E ref V ref k p k d s qd s 2 1 SW2 PWM mode Figure 2. The proposed block diagram. TABLE I. CIRCUIT PARAMETERS. Start Local Load R load 50 ohm Filter Inductor L f 5 mh Filter Capacitance C f 20 μf Line Transmission 0.2 Z impedance g ohm j1.885 mode Voltage SW1=1 SW2=1 Applying virtual inductance Ridingthrough mode Time delay The voltage command is determined according to both frequencyreal power and voltagereactive power droops. equations and their definitions are given in (1). Thus, various inverters are able to share workloads if their droop coefficients are chosen in inverse proportion to their rated capacities, as given in (2). ω = ω o m (P o P); E = E o n (Q o Q) (1) m 1 P o1 = m 2 P o2 = m 3 P o3 (2) n 1 Q o1 = n 2 Q o2 = n 3 Q o3 Where the ω o is the nominal frequency, P o is the output rated real power, E o is the nominal voltage, Q o is the rated output reactive power, m is the Pf droop coefficient and n is the Q v droop coefficient. Based on the voltage command, a proportional plus the feedforward of the voltage command is realized to regulate output voltage in the stationary reference frame [5]. Due to the feedforward, inverter voltage can be led with acceptable steadystate and transient behavior. In addition, the differentiating of capacitor voltage is fed back in order to reduce the resonance on the filter capacitor C f. As can be seen, a proportional gain K d can be designed to accomplish a critical damped response for the voltage loop of the inverter. Finally, PWM is realized to produce the switching signals of the inverter. B. Ridingthrough algorithm In order to maintain proper operation of the inverter, we present a seamless transition method to help the inverter ride Generating voltage command No Over current? Yes SW1=2 SW2=2 Figure 3. Flow chart of the proposed strategy. Current (iref=0) and PLL through large transient current due to asynchronous grid connection. Fig.2 shows the proposed method, including phaselock loop (PLL), current, and virtual inductance. The ridingthrough will be triggered when the inverter current exceeds presetting limitation. Fig.3 shows the flow chart to illustrate detailed operation. If the transient current is large enough at the closing of the STS, the inverter will temporarily switch to the ridingthrough mode (SW 1 and SW 2 are at position 2). During this period, the inverter will operate at the current mode with zero current command and the PLL will replace the angle command in the droop ler. This can correct angle difference between the inverter and the utility due to asynchronous connection. A short time delay is then required for PLL to reach the steady state. After that, a virtual inductance defined in (3) will start in operation, L v = L vf (L vi L vf ) e t τ (3) di qds V Lqds = L v (4) dt where L vf and L vi are final and initial inductances, respectively, and τ represents time constant. Thus, a reacted voltage in (4) is produced to reduce transient current due to angle variation of the droop. The stability of the inverter can also be improved by the virtual inductance. After this short transient, the inverter will transfer back to the droopled mode (SW 1 and SW 2 are at position 1).

.01.01.0001.0001.01 Figure 4. Root locus of the inverter Pf coefficient changes from 0.0001 to 0.1. Figure 5. Root locus of the inverter Pf and Qv coefficients both change from 0.0001 to 0.1 I o E ref V ref 1 kp k V I L I dq m (PWM) sl f r f E dq K d s R load 1sC f R load E dq Figure 6. Multiloop voltage block diagram III. DESIGN CONSIDERATIONS A. coefficients According to (2), the droop coefficient needs to be designed for proper load sharing. Here, we present design considerations based on the dynamic equation and root locus method. Fig.4 shows the movement of roots for varying the Pf droop coefficient m inv. Note that the utility is assumed as a stiff voltage source. As can be seen, two roots become complex number when m inv varies from 0.0001 to 1. Thus, this is a stable system with damping oscillation only. Next, we consider varying both n inv and m inv. Fig.5 shows the roots will move to the righthalf of the plane with increasing both coefficients. Results show the system will become unstable for large n inv. Based on the above observation, m inv and n inv can be chosen with an acceptable transient behavior in the stable range. B. Multiloop voltage Fig.6 shows the modeling of multiloop voltage, in which the dashbox represents the plant model, V ref is the normalized modulation signal and E dq is the output voltage of the inverter. E dq to V ref and E dq to E ref transfer functions are given in (4) and (5), respectively. G(s) = E dq V ref = k m 1 L f C f s 2 L f K d R R L f C f s 1 L f C f = k m G LC (s) (4) E dq E ref = (1 k p )G(s) (5) Differential gain K d can be designed with critically damping condition of (4) as defined in (6). > 0.5, (under damping) Q = 1 = L fk d R : = 0.5, (critical damping) 2ξ R L f C f < 0.5, (over damping) As can be seen from Fig.7, the high frequency resonance may harmonics or even cause instability when K d = 0. In case of K d = 0.00535, the resonance is clearly suppressed and phase lagging is improved. For overdamping condition (K d = 0.001064), stability is also improved, but its time response is lower than that of the critically damping case. After determining K d, the proportional gain k p can be obtained according to the frequency response of the voltage loop. Fig.8 shows bode plot of the open loop. Accordingly, we can choose suitable bandwidth and phase margin. C. Virtual inductance Fig.9 shows the simplified circuit diagram including the virtual inductance. Similarly, the dynamic equation and root locus are used for the purpose of stability analysis. Fig.10 shows the root locus when the virtual inductance L v decreases from 5H to 80uH. As demonstrated, roots will be close to the realaxis. That means the stability of the system is improved with increasing the virtual inductance. I. EXPERIMENTAL RESULTS A labscaled prototype was developed to verify the proposed seamless transition strategy. Test circuit is shown in Fig.11 and the parameters are given as TABLE II. (6)

TABLE II. EXPERIMENTAL SETUP PARAMETERS. Figure 7. Frequency response of three different K d Nominal voltage E 0 174.7 V Inverter output power P o 1000 W Nominal Frequency ω 0 377 rad/s Pω droop m 0.0005 rad/j QV droop n 0 V/VAr Filter Cutoff Frequency ω c 62.8 rad/s Nominal Virtual Inductor L vi 80 μh Initial Virtual Inductor L vf 3 H Time Constant τ 0.3 1/sec Proportional gain k p 0.3 Differential coefficient K d 0.000532 E Figure 8. Bode plot of the open loop for k p =0.3. (crossover frequency=762hz, phase margin=68 ). Inverter L v R g R Load L g Grid Figure 9. Simplified circuit which inverter connects to grid through a virtual inductance Lv=5 H Lv=80 106 H Lv=80 106 H Lv=80 106 H V g Lv=5 H Fig.12 shows the steadystate waveform when the inverter supplies a three phase load at the islanding mode, where. The inverter output a three phase balance voltage at 60Hz because of the droop ler. In order to guarantee the feasibility of the proposed seamless transition strategy, the inverter is switched to the gridconnected operation with no grid information. Fig.13 shows the voltages transient when the gridconnected happens at the phase difference 169.8. At T 1, the inverter current exceeds the limitation because of the nonsynchronization of the inverter and grid. At the moment, the inverter automatically switches to the ridingthrough mode. The current ler of the riding through mode brings the inverter output current to almost zero which is shown in Fig.14 and the PLL updates the phase angle of the voltage command at the same time. After a specific time delay, the virtual inductance is initiated at T 2 and the inverter switches back to the droop mode. As shown, the virtual inductance can help reduce oscillating current due to the droop. The designed virtual inductance is shown in Fig.15 with the initial value 3H and exponentially decreasing feature. Fig.16 shows transient result with no virtual inductance. Obviously, the inverter current is still high enough to trigger protection, compared with Fig.14. At the steadystate of the gridconnected operation, the inverter output rated power 1kW shows in Fig.17. Fig.18 shows the inverter output power and the output current when the load is changed to 25Ω at T 3. At the transient, the inverter supplies the increased load. When reaching the steady state, the load is still shared by the inverter and the grid according to the designed droop. The inverter supplies rated power 1kW and the other is from the utility. As, can be seen from Fig.19, the grid current is increased after load change. Lv=80 106 H Figure 10. Root locus of the different virtual inductance

Uility E L f V dc Uility Z g R load C f Figure 11. Experimental circuit Figure 12. Inverter output voltage (islanding operation) Inverter output voltage Control T 1 T 2 Control Figure 15. The implement virtual inductance value (1H /1div) T 1 T 2 Grid voltage Figure 13. Inverter output voltage and grid voltage (transient of inverter switching to gridconnected operation) T 1 T 2 Figure 16. Inverter output current without virtual inductance Figure 14. Inverter output current with virtual inductance Figure 17. The invert output power(500w/v)

T 3 Inverter output power II. CONCLUSION A droopled inverter with seamless transition between islanding and gridconnected operations is presented. By implementing a local PLL and a virtual inductor, the inverter could ride through paralleling transient to the utility with no synchronization. This method could integrate with droopled algorithms so that the inverters could share load among them as well as subsist under transient events, such as voltage sag, swell, and harmonics. Figure 18. The invert output power and the output current of load change (500W/V) T 3 REFERENCES [1] IEEE Standard for Interconnecting Distributed Resources with Electric Power Systems, IEEE Std 1547.2 2008. [2] R. Lasseter, Microgrids, in IEEE Power Engineering Society Winter Meeting, 2002, pp. 305 308. [3] M. C. Chandorkar and D. M. Divan, Control of parallel connected inverters in standalone AC supply system, IEEE Trans. Ind. Applicat., vol. 29, no. 1, pp. 136 143, Jan. /Feb. 1993. [4] J. M. Guerrero, J. C. Vasquez, J. Matas, M. Castilla, and L. G. de Vicuna, Control strategy for flexible microgrid based on parallel lineinteractive UPS systems, IEEE Trans. Ind. Electron., vol. 56, no. 3, pp. 726 736, Mar. 2009. [5] Q. Lei, S. Yang, and F. Z. Peng, Multiloop algorithms for seamless transition of gridconnected inverter, in IEEE 25th Applied Power Electronics Conference and Exposition, 2010. Figure 19. The grid current of load change