Modified Virtual Impedance Control to Improve Real and Reactive Power Output in Islanded Microgrid

Pradeep Kumar Singh and Dharmendra Kumar Dheer*

Electrical Engineering Department, National Institute of Technology, Patna, India
E-mail: dkdheer@nitp.ac.in
*Corresponding Author

Received 11 January 2022; Accepted 11 March 2022; Publication 09 December 2022

Abstract

In this paper, modified virtual impedance control technique is proposed to bring back the sum of real power and reactive power output of all the distributed generators (DGs) to the nominal value. The value of real and reactive power output falls down in the conventional virtual impedance control technique for reactive power sharing improvement in islanded microgrid. The proposed technique modifies the d-axis component of virtual impedance voltage which in turns brings back the sum of real and reactive power output of distributed generators to nominal value keeping achieved reactive power sharing and output voltage intact. The impact of modified virtual impedance technique on the stability of the system is also investigated using eigenvalue analysis. No communication link or optimization technique is required in this work which reduces the complexity of the system making it more reliable and easier to design. The proposed technique works satisfactory for local load as well as the loads which are connected distantly from the distributed generators. The feasibility of the proposed technique is validated in time domain simulation in MATLAB/Simulink. The MATLAB R2020b version 9.9 is used in this research work.

Keywords: Islanded microgrid control, reactive power sharing, modified virtual impedance technique, reactive power sharing improvement..

1 Introduction

Distributed energy resources (DERs) are used to provide clean energy which not only helps in meeting the energy demand but also saves the environment. DERs are integrated into the system (either grid connected or islanded microgrid) which are mostly interfaced with the inverters at the front end [1]. Proportional power sharing between the DGs is one of the basic and important criteria for desired operation of DGs in standalone operation. P-ω and Q-V droop control technique is used to achieve the desired power sharing amongst the DGs [2]. The active power sharing in DGs operating in droop control technique is proportional to rating of DGs but it fails to share reactive power in proportion to the size of DGs. Imprecise reactive power sharing is primarily due to the unequal feeder impedance which needs improvement to avoid circulating current and overloading of smaller DGs.

Various control methods have been proposed in literature for the improvement of reactive power sharing which is reviewed in [3] and can be categorized into: droop-based control technique [49] and virtual impedance control technique [1020]. A self-adjusting nominal voltage-based control method to improve the reactive power (Q) sharing among sources in an islanded microgrid has been proposed in [6] and appreciable improvement in Q sharing has been achieved by adaptive nominal voltage as compared to fixed nominal voltage. An adaptive nq based method is used in [7] to improve reactive power sharing which uses different value of nq in different load conditions causing requirement of excessive computation for every change in load. Author in [9] applied communication link for the improvement in power sharing between the DG’s. The problem associated with the communication link is that DGs may operate unsatisfactory in case of communication failure or delay in communication.

The basic idea of virtual impedance (Zv) is to place high value impedance between interfacing converter outputs and the point of common coupling (PCC). This will minimize the impedance mismatch between the DGs and proportional reactive power sharing can be achieved. The value of virtual impedance should be chosen carefully and it should be accurate otherwise it may affect the stability of the system. To get the accurate value of Zv [10, 11] proposes a strategy to design and implement the virtual impedance. It also suggests a range of virtual impedance with which reactive power sharing can be improved without affecting the system stability. Authors in [14, 15] uses Genetic Algorithm (GA) based optimization and particle Swarm Optimization (PSO) respectively to design virtual impedance controller for reactive power sharing improvement among the DGs. The optimization used increases the computation burden and slows down response of the system. Authors in [1620] used adaptive virtual impedance method for the improvement of reactive power sharing amongst DGs in islanded microgrid.

Comparative study for the improvement in reactive power sharing among robust droop control strategy (RDCS) and virtual impedance technique is presented in [1]. It is observed that for the higher values of Xv, error in reactive power sharing (Qerr) decreases. However, the total sum of active power output (Ptotal) and reactive power output (Qtotal) of all the sources decreases from the nominal value of the sum of total load connected to the system which is not desirable. In this paper, the conventional virtual impedance technique is modified to reduce the decrement in Ptotal and Qtotal from its nominal value keeping the achieved reduction in Qerr intact.

The organisation of the paper is as follows: Modified virtual impedance control technique and system under study is presented in section-II. Section-III talk over the results obtained in time domain simulation studies. Stability analysis is performed in section-IV. Finally conclusion and scope of future work has been presented in section-V.

2 Modified Virtual Impedance Control and System Under Study

The microgrid is operating in convention droop control scheme for proportional active and reactive power sharing among the sources which is given in (1a) and (1b) respectively.

ω=ωn-mpP (1a)
Vod*=Vn-nqQ (1b)

where, ωn and Vn is nominal frequency and voltage respectively. mp and nq is active and reactive power droop coefficient respectively. Vod* is d-axis reference output voltage and ω is operating frequency. P is active power output and Q is reactive power output of the source.

The modified virtual impedance control scheme and the system under study are presented in this section.

2.1 Modified Virtual Impedance Control

In this section modified virtual impedance control scheme is introduced which reduces the decrements in Ptotal and Qtotal as in [1] keeping the achieved reduction in Qerr intact.

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Figure 1 Block diagram of voltage source inverter based DG operating with virtual/modified-virtual impedance control.

The conventional virtual impedance control is modified by adding a term (-XvaddIod) in the d-axis component of virtual impedance voltage (2) to mitigate the effect of decrement in Ptotal and Qtotal from its nominal value. Algebraic equations corresponding to modified virtual impedance control for Vvq and Vvd (Figure 2) is proposed as:

Vvd=RvIod-XvIoq-XvaddIod (2a)
Vvq=RvIoq+XvIod (2b)

Where Vvd and Vvq is d-axis and q-axis component of virtual impedance voltage. Rv and Xv are virtual resistance and virtual reactance respectively. Iod and Ioq are d-axis and q-axis components of current.

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Figure 2 Block diagram of Vvq for modified Virtual impedance technique.

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Figure 3 Test system MG1.

2.2 System Under Study

Line and load data of the microgrid under study (Figure 3 ) containing three DGs of rating 10kVA each is shown in Table 1 which is adapted from [1].

Table 1 MG network data

Line no. Impedance (Ω) R/X Load (kVA)
L1 0.20 + j 0.06 3.33 CL = 9 + j 4.5
L2 0.30 + j 0.09 3.33 LL = 1.5 + j 0.75
L3 0.40 + j 0.12 3.33

3 Simulation Results

A comparative study between modified virtual impedance control technique and virtual impedance technique for common load as well as common plus local load (Figure 3) was carried out while the local load is connected at DG1. The values of P, Q, Qerr and d-axis output voltage (Vodr) is obtained for the different cases which are given as follows:

• Case-1: Varying the Xv from 0.1 to 1.0 Ω in steps of 0.1 Ω while keeping the Rv constant at (Rv = 0.0 Ω) for common load as shown in Table 2.

• Case-2: Keeping Rv and Xv constant at 0.0 Ω and 1.0 Ω respectively while varying the Xvadd in terms of Xv for common load as shown in Table 3.

• Case-3: Varying the Xv from 0.1 to 1.0 Ω in steps of 0.1 Ω while keeping the Rv constant at (Rv = 0.0 Ω) for common plus local load as shown in Table 4.

• Case-4: Keeping Rv and Xv constant at 0.0 Ω and 1.0 Ω respectively while varying the Xvadd in terms of Xv for common plus local load as shown in Table 5.

3.1 Common Load Case

Based on Table 2 it is found that keeping Rv at Rv = 0.0 Ω and increasing Xv from 0.1 Ω to 1.5 Ω , causes decrement in reactive power sharing error and improvement in output voltage from Vodr = 0.992 pu to Vodr = 0.995 pu. But with increased value of Xv, active power output and average reactive power output also decreases from P = 2.88 kW (Rv = 0.0, Xv = 0.1) to P = 2.555 kW (Rv = 0.0, Xv = 1.5) and Qexp = 1.42 kVAr (Rv= 0.0, Xv = 0.1) to Qexp = 1.2953 kVAr (Rv=0.0,Xv=1.5) respectively. Figure 4 also shows that active output power P and average reactive output power Qexp decreases with increased values of Xv which is not desired and needs improvement.

When system is modified by adding an addition term Xvadd and increasing its value in terms of Xv there is increment in the output power P as well as average reactive output power Qexp. The output power P improves to P = 2.92 kW (Xvadd=Xv/2) and the average reactive power Qexp improves to Qexp = 1.4167 kVAr (Xvadd=Xv/2) (Table 3). The Rv and Xv is kept constant at 0.0 Ω and 1.0 Ω respectively. Figure 5 also validate the the improvement in active output power P and average output reactive power Qexp after adding the Xvadd. It is also observed that reactive power sharing error is almost unchanged and output voltage is maintained at Vodr = 0.995 pu in this case.

Table 2 Virtual impedance implementation for common load case: Rv = constant, Xv = variable

Virtual P(1-3) Q(1-3) Qexp Qerr(1-3) vodr(1-3)
impedance (Ω) (kW) (kVAr) (kVAr) (%) (pu)
Rv = 0, Xv = 0.1 2.88 2.51, 1.35, 0.40 1.42 76.76, –4.93, –71.83 0.992, 0.996, 0.999
Rv = 0, Xv = 0.2 2.85 2.21, 1.36, 0.64 1.4033 57.48, –3.08, –54.4 0.993, 0.995, 0.998
Rv = 0, Xv = 0.3 2.83 2.03, 1.37, 0.79 1.3967 45.34, –1.90, –43.43 0.993, 0.995, 0.997
Rv = 0, Xv = 0.4 2.80 1.91, 1.37, 0.88 1.3867 37.74, –1.20, –36.54 0.994, 0.995, 0.997
Rv = 0, Xv = 0.5 2.78 1.81, 1.36, 0.945 1.3717 31.95, –0.85, –31.10 0.994, 0.995, 0.997
Rv = 0, Xv = 0.6 2.76 1.74, 1.35, 0.99 1.36 27.94, –0.74, –27.20 0.994, 0.995, 0.997
Rv = 0, Xv = 0.7 2.73 1.685, 1.345, 1.025 1.3517 24.66, –0.50, –24.16 0.994, 0.995, 0.996
Rv = 0, Xv = 0.8 2.71 1.635, 1.335, 1.05 1.34 22.01, –0.37, –21.64 0.994, 0.995, 0.996
Rv = 0, Xv = 0.9 2.69 1.595, 1.325, 1.068 1.3293 19.99, –0.32, –19.67 0.995, 0.996, 0.996
Rv = 0, Xv = 1.0 2.665 1.555, 1.31, 1.08 1.315 18.25, –0.38, –17.87 0.995, 0.996, 0.996
Rv = 0, Xv = 1.1 2.64 1.525, 1.303, 1.09 1.306 16.77, –0.23, –16.54 0.995, 0.996, 0.996
Rv = 0, Xv = 1.2 2.618 1.492, 1.290, 1.095 1.2923 15.45, –0.18, –15.27 0.995, 0.996, 0.996
Rv = 0, Xv = 1.3 2.595 1.468, 1.28, 1.1 1.2827 14.44, –0.21, –14.23 0.995, 0.996, 0.996
Rv = 0, Xv = 1.4 2.575 1.442, 1.268 , 1.102 1.271 16.45, –0.27, –13.18 0.995, 0.996, 0.996
Rv = 0, Xv = 1.5 2.555 1.418, 1.257 , 1.103 1.2953 12.60, –0.18, –12.42 0.995, 0.996, 0.996

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Figure 4 P/Q sharing and output voltages of DGs at Rv = 0.0 Ω and Xv = 1.0 Ω for common load case.

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Figure 5 P/Q sharing and output voltages of DGs at Rv = 0.0 Ω, Xv = 1.0 Ω and Xvadd = Xv2 = 0.5 Ω for common load case.

Table 3 Variation in XVadd keeping RV = 0.0 and XV = 1.0 for common load case

XVadd P(1-3) Q(1-3) Qexp Qerr(1-3) vodr(1-3)
(Ω) (kW) (kVAr) (kVAr) (%) (pu)
XV10 2.70 1.58, 1.33, 1.095 1.335 18.35, –0.375, –17.975 0.995, 0.996, 0.996
XV9 2.71 1.58, 1.33, 1.097 1.336 18.26, –0.449, –17.889 0.995, 0.996, 0.996
XV8 2.72 1.58, 1.335, 1.10 1.338 18.08, –0.224, –17.788 0.995, 0.996, 0.996
XV7 2.73 1.59, 1.34, 1.10 1.343 18.39, –0.223, –18.093 0.995, 0.996, 0.996
XV6 2.74 1.60, 1.35, 1.105 1.3517 18.37, –0.126, –18.25 0.995, 0.996, 0.996
XV5 2.76 1.60, 1.35, 1.11 1.353 18.25, –0.221, –17.96 0.995, 0.996, 0.996
XV4 2.78 1.61, 1.36, 1.12 1.363 18.12, –0.22, –17.83 0.994, 0.995, 0.996
XV3 2.82 1.64, 1.38, 1.135 1.385 18.41, –0.36, –18.05 0.994, 0.995, 0.996
XV2 2.92 1.66, 1.42, 1.17 1.4167 17.17, 0.233, –17.41 0.994, 0.995, 0.996
XV Oscillatory Oscillatory Oscillatory

3.2 Common Plus Local Load Case

When the local load is also connected along with common load and varying Xv from 0.1 Ω to 1.5 Ω keeping Rv constant at (Rv = 0.0 Ω), the error in reactive power sharing decreases and output voltage maintained at almost same value. The active power output decreases from P = 3.35 kW to P = 2.905 kW and reactive power output decreases from Qexp=1.65 kVAr to Qexp = 1.4353 kVAr respectively (Table 4). Figure 6 also shows that active output power P and average reactive power Qexp decreases when Xv is increased with virtual impedance technique which is downside of this technique. When modified virtual impedance technique is applied and the Xvadd increases, active and average reactive power starts improving and reaches at P = 3.35 kW and Q = 1.64 kVAr respectively at (Xvadd=Xv/2) while keeping reactive power sharing error and output voltage almost constant (refer Table 5, Figure 7).

So, it can be seen from comparative results of virtual impedance technique and modified virtual impedance technique that at higher value of Xv, Qerr is reduced but output power P and average reactive power (Qexp) also reduces in case of virtual impedance technique compared to modified virtual impedance technique.

Table 4 Virtual impedance implementation for common plus local load case: Rv = constant, Xv = variable

Virtual P(1-3) Q(1-3) Qexp Qerr(1-3) vodr(1-3)
impedance (Ω) (kW) (kVAr) (kVAr) (%) (pu)
Rv = 0, Xv = 0.1 3.35 3.66, 1.17, 0.12 1.65 121.8, –29.1, –92.7 0.988, 0.996, 1.000
Rv = 0, Xv = 0.2 3.31 3.12, 1.31, 0.49 1.64 90.2, –20.1, –70.1 0.990, 0.996, 0.998
Rv = 0, Xv = 0.3 3.28 2.78, 1.37, 0.71 1.62 71.6, –15.4, –56.2 0.991, 0.995, 0.998
Rv = 0, Xv = 0.4 3.24 2.55, 1.40, 0.85 1.6 59.4, –12.5, –46.9 0.991, 0.996, 0.997
Rv = 0, Xv = 0.5 3.21 2.39, 1.42, 0.95 1.59 50.6, –10.5, –40.1 0.992, 0.996, 0.997
Rv = 0, Xv = 0.6 3.18 2.26, 1.43, 1.02 1.57 44.0, –8.9, –35.0 0.992, 0.995, 0.997
Rv = 0, Xv = 0.7 3.15 2.16, 1.43, 1.08 1.56 38.9, –8.0, –30.9 0.993, 0.995, 0.996
Rv = 0, Xv = 0.8 3.12 2.07, 1.43, 1.12 1.54 34.4, –7.1, –27.3 0.993, 0.995, 0.996
Rv = 0, Xv = 0.9 3.09 2.0, 1.43, 1.14 1.52 31.3, –6.1, –25.1 0.993, 0.995, 0.996
Rv = 0, Xv = 1.0 3.05 1.94, 1.42, 1.16 1.51 28.7, –5.7, –23.0 0.993, 0.995, 0.996
Rv = 0, Xv = 1.1 3.03 1.887, 1.422, 1.182 1.497 26.05, –5.01, –21.04 0.994, 0.995, 0.996
Rv = 0, Xv = 1.2 3.0 1.838, 1.413, 1.193 1.4813 24.08, –5.01, –21.04 0.994, 0.995, 0.996
Rv = 0, Xv = 1.3 2.97 1.793, 1.403, 1.202 1.466 22.30, –4.30, –18.0 0.994, 0.995, 0.996
Rv = 0, Xv = 1.4 2.935 1.751, 1.392, 1.207 1.45 20.76, –4.0, –16.76 0.994, 0.995, 0.996
Rv = 0, Xv = 1.5 2.905 1.714, 1.382, 1.210 1.4353 19.41, –3.71, –15.70 0.994, 0.995, 0.996

Table 5 Variation in XVadd keeping RV = 0.0 and XV = 1.0 for common plus local load case

XVadd P(1-3) Q(1-3) Qexp Qerr(1-3) vodr(1-3)
(Ω) (kW) (kVAr) (kVAr) (%) (pu)
XV10 3.10 1.97, 1.45, 1.185 1.535 28.34, –5.53, –22.80 0.993, 0.995, 0.996
XV9 3.11 1.975, 1.455, 1.185 1.5383 28.39, –5.41, –22.97 0.993, 0.995, 0.996
XV8 3.12 1.98, 1.455, 1.185 1.54 28.57, –5.52, –23.05 0.993, 0.995, 0.996
XV7 3.13 1.99, 1.46, 1.19 1.5467 28.66, –5.60, –23.06 0.993, 0.995, 0.996
XV6 3.15 1.99, 1.47, 1.195 1.5517 28.25, –5.27, –22.98 0.993, 0.995, 0.996
XV5 3.17 2.0, 1.475, 1.205 1.56 28.2, –5.45, –22.75 0.993, 0.995, 0.996
XV4 3.19 2.02, 1.49, 1.215 1.575 28.26, –5.40, –22.86 0.993, 0.995, 0.996
XV3 3.25 2.05, 1.51, 1.235 1.5983 28.26, –5.52, –22.73 0.993, 0.995, 0.996
XV2 3.35 2.10, 1.55, 1.27 1.64 28.05, –5.49, –22.563 0.993, 0.995, 0.996
XV Oscillatory Oscillatory Oscillatory

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Figure 6 P/Q sharing and output voltages of DGs at Rv=0.0Ω and Xv=1.0Ω for common plus local load case.

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Figure 7 P/Q sharing and output voltages of DGs at Rv=0.0Ω, Xv=1.0Ω and Xvadd=Xv2=0.5Ω for common plus local load case.

4 Stability Analysis

To investigate the effect of modified virtual impedance control technique on the small signal stability margin of the system, the dynamic model of distributed generators operating in modified virtual impedance control scheme, lines and loads are firstly obtained separately and then are combined to obtain the complete dynamic model of microgrid which is expressed as:

[ΔXINVΔIlineDQΔIloadDQ]˙=Amg[ΔXINVΔIlineDQΔIloadDQ] (3)

Where XINV is states of all inverters. IlineDQ and IloadDQ are the states of all lines and loads respectively. There are thirteen states of the inverter: δ (angle between inverter reference frame and common reference frame), P (active power output), Q (reactive power output), ϕd (d-axis voltage flux), ϕq (q-axis voltage flux), γd (d-axis current flux), γq (q-axis current flux), ild (d-axis line current), ilq (q-axis line current), vod (d-axis output voltage), voq (q-axis output voltage), iod (d-axis output current), ioq (q-axis output current).

Amg is state space matrix of complete system and its size is (13s+2n+2p)×(13s+2n+2p), where s number of sources, n is number of lines and p is number of loads connected to the system. In this manuscript the system under study has s = 3, n = 3, and p = 1 for common load case and s = 3, n = 3 and p = 2 for common plus local load case. Small signal stability analysis of the system (Figure 3 ) operating in modified virtual impedance technique is performed with the help of dynamic Equation (3). The steady state operating conditions of the system are obtained through MATLAB/Simulink. The complete eigenvalues of the system is shown in Figure 8. It is found that eigenvalues are mainly classified into three clusters including low frequency modes, medium frequency modes and high frequency modes Figure 8. The low frequency modes are mainly associated with the power controller state variables and the virtual impedances including Rv, Xv and Xvadd. The medium frequency modes are mainly associated with the state variables of voltage and current controllers and the high frequency modes are mainly associated with the LC filter with coupling inductor.

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Figure 8 Eigenvalue plot with modified virtual impedance control.

Eigenvalue trace by varying the value of mp (0.00005:0.00005:0.003) for Rv=0.0 Ω, Xv=1.0Ω, Xvadd=0.1Ω and nq=1.0×10-4 V/(VAr) is obtained and shown in Figure 9. It is found that λ12 and λ13 are most sensitive eigenvalues subjected to system stability and are related to the low frequency modes of inverter 1–2 and inverter 1–3 respectively. It is also found that λ12 reaches the imaginary axis before λ13 at the of mp=19.88×10-4.

Eigenvalue trace by varying the value of nq (0.0001:0.0001:0.007) for Rv = 0.0 Ω, Xv = 1.0 Ω, Xvadd = 0.1 Ω and mp=5.0×10-5 rad/(W.s) is obtained and shown in Figure 10. It is found that λ12 and λ13 are most sensitive eigenvalues subjected to system stability and are related to the low frequency modes of inverter 1-2 and inverter 1-3 respectively. It is also found that λ12 reaches the imaginary axis before λ13 at the of nq=56.68×10-4.

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Figure 9 Eigenvalue trace for low frequency modes with modified virtual impedance control: 0.00005 mp 0.003.

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Figure 10 Eigenvalue trace for low frequency modes with modified virtual impedance control: 0.0001 nq 0.007.

Table 6 Effect of variation in Rv and Xv on mp,max for conventional virtual impedance technique at nq=1.0×10-4 V/(VAr)

Virtual mp,max Virtual mp,max
impedance (Ω) rad/(W.s) impedance (Ω) rad/(W.s)
Rv = 0, Xv = 0.1 1.96 × 10-4 Rv = 0.1, Xv = 0.1 3.76 × 10-4
Rv = 0, Xv = 0.2 1.79 × 10-4 Rv = 0.1, Xv = 0.2 3.08 × 10-4
Rv = 0, Xv = 0.3 2.02 × 10-4 Rv = 0.1, Xv = 0.3 3.13 × 10-4
Rv = 0, Xv = 0.4 2.52 × 10-4 Rv = 0.1, Xv = 0.4 3.58 × 10-4
Rv = 0, Xv = 0.5 3.29 × 10-4 Rv = 0.1, Xv = 0.5 4.37 × 10-4
Rv = 0, Xv = 0.6 4.44 × 10-4 Rv = 0.1, Xv = 0.6 5.57 × 10-4
Rv = 0, Xv = 0.7 6.15 × 10-4 Rv = 0.1, Xv = 0.7 7.48 × 10-4
Rv = 0, Xv = 0.8 8.81 × 10-4 Rv = 0.1, Xv = 0.8 10.52 × 10-4
Rv = 0, Xv = 0.9 13.38 × 10-4 Rv = 0.1, Xv = 0.9 16.06 × 10-4
Rv = 0, Xv = 1.0 21.72 × 10-4 Rv = 0.1, Xv = 1.0 27.36 × 10-4

Effect on the stability margin of the system for modified virtual impedance control (Equation 2) is studied and compared with the stability margin obtained with conventional virtual impedance control. The study is performed in the following manner:

• Effect of variation in Xv (0.1:0.1:1.0 Ω) for the values of Rv = 0.0 and 0.1 Ω respectively is studied for conventional virtual impedance control and value of mp,max is obtained at nq=1.0×10-4 V/(VAr) which is depicted in Table 6.

• Effect of variation in Xv (0.1:0.1:1.0 Ω) for the values of Rv = 0.0 and 0.1 Ω respectively is studied for conventional virtual impedance control and value of nq,max is obtained at mp=5.0×10-5 rad/(W.s) which is depicted in Table 7.

• Effect of variation in Xvadd (0.1:0.1:1.0 Ω) on mp,max is studied for modified virtual impedance technique at Rv=0.0 Ω, Xv=1.0 Ω, nq=1.0×10-4 V/(VAr) which is depicted in Table 8.

• Effect of variation in Xvadd (0.1:0.1:1.0 Ω) on nq,max is studied for modified virtual impedance technique at Rv=0.0 Ω, Xv=1.0 Ω, mp=5.0×10-5 rad/(W.s) which is depicted in Table 9.

Table 7 Effect of variation in Rv and Xv on nq,max for conventional virtual impedance technique at mp=5.0×10-5 rad/(W.s)

Virtual nq,max Virtual nq,max
impedance (Ω) V/(VAr) impedance (Ω) V/(VAr)
Rv = 0, Xv = 0.1 8.85 × 10-4 Rv = 0.1, Xv = 0.1 9.88 × 10-4
Rv = 0, Xv = 0.2 14.13 × 10-4 Rv = 0.1, Xv = 0.2 14.84 × 10-4
Rv = 0, Xv = 0.3 19.57 × 10-4 Rv = 0.1, Xv = 0.3 20.02 × 10-4
Rv = 0, Xv = 0.4 24.85 × 10-4 Rv = 0.1, Xv = 0.4 25.13 × 10-4
Rv = 0, Xv = 0.5 30.18 × 10-4 Rv = 0.1, Xv = 0.5 30.88 × 10-4
Rv = 0, Xv = 0.6 35.47 × 10-4 Rv = 0.1, Xv = 0.6 36.02 × 10-4
Rv = 0, Xv = 0.7 40.73 × 10-4 Rv = 0.1, Xv = 0.7 41.17 × 10-4
Rv = 0, Xv = 0.8 46.06 × 10-4 Rv = 0.1, Xv = 0.8 46.91 × 10-4
Rv = 0, Xv = 0.9 51.36 × 10-4 Rv = 0.1, Xv = 0.9 51.56 × 10-4
Rv = 0, Xv = 1.0 56.57 × 10-4 Rv = 0.1, Xv = 1.0 56.84 × 10-4

The findings of the results are as follows:

• For the conventional virtual impedance control, the value of mp,max increases with the increasing value of Xv except for the value of Xv = 0.2 Ω when nq are kept constant (refer to Table 6).

• For the conventional virtual impedance control, the value of nq,max increases with the increasing value of Xv when mp are kept constant (refer to Table 7).

• For the modified virtual impedance control, the value of mp,max decreases with the increasing value of Xvadd when Rv, Xv and nq are kept constant (refer to Table 8).

• For the modified virtual impedance control, the value of nq,max remains almost constant with the increasing value of Xvadd when Rv, Xv and mp are kept constant (refer to Table 9).

Table 8 Effect of variation in Xvadd on mp,max for modified virtual impedance technique at Rv=0.0 Ω, Xv=1.0 Ω, nq=1.0×10-4 V/(VAr)

Xvadd mp,max Xvadd mp,max
(Ω) rad/(W.s) (Ω) rad/(W.s)
0.1 19.88 × 10-4 0.6 12.04 × 10-4
0.2 18.17 × 10-4 0.7 10.76 × 10-4
0.3 16.37 × 10-4 0.8 9.46 × 10-4
0.4 14.88 × 10-4 0.9 8.22 × 10-4
0.5 13.33 × 10-4 1.0 Oscillatory

Table 9 Effect of variation in Xvadd on nq,max for modified virtual impedance technique at Rv=0.0 Ω, Xv=1.0 Ω, mp=5.0×10-5 rad/(W.s)

Xvadd nq,max Xvadd nq,max
(Ω) V/(VAr) (Ω) V/(VAr)
0.1 56.68 × 10-4 0.6 57.38 × 10-4
0.2 56.82 × 10-4 0.7 57.47 × 10-4
0.3 56.98 × 10-4 0.8 57.53 × 10-4
0.4 57.13 × 10-4 0.9 57.67 × 10-4
0.5 57.27 × 10-4 1.0 Oscillatory

5 Conclusion

The proposed modified virtual impedance control bring back the sum of real and reactive power output of all the distributed generators to the nominal value. The proposed technique is based on insertion of an additional term (-XvaddIod) in d-axis component of virtual impedance voltage keeping q-axis component unchanged so as to keep the reactive power sharing error almost constant for different values of Xvadd. The proposed method is simulated in MATLAB/Simulink environment and found suitable for different network configurations. Small signal stability analysis is performed and it is found that the proposed control scheme reduces the system stability. Improvement in the stability margin of the system with the modified virtual impedance technique is the scope of future work.

References

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Biographies

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Pradeep Kumar Singh. He is born in Kushinagar, UP, India. He received the B.Tech. degree in electrical engineering from UPTU Lucknow, India, in 2007, the M.Tech. degree in control and instrumentation with specialization voltage regulation from National Institute of Technology Jalandhar, India, in 2009. Currently he is Ph.D scholar at the department of electrical engineering, National Institute of Technology Patna, Bihar. He has 10 years of experience in the field of teaching, research. His current research interest includes microgrid operations and control.

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Dharmendra Kumar Dheer. He is born in Bhagalpur, Bihar, India. He received the B.Sc. engineering degree in electrical engineering from Muzaffarpur Institute of Technology Muzaffarpur, India, in 2007, the M.Tech. degree in electrical engineering with specialization in power system engineering from Indian Institute of Technology Kharagpur, India, in 2010, and the Ph.D. degree in power and energy systems engineering from the department of Energy Science and Engineering, Indian Institute of Technology Bombay, Mumbai, India, in 2017. Currently he is serving as an assistant professor at the department of electrical engineering, National Institute of Technology Patna, Bihar. He has one and half year of teaching experience after M.Tech. degree, six month of research experience as a research associate at IIT Bombay and five and half months of research experience as a postdoctoral researcher at Arizona State University (ASU), USA. His current research interest includes stability and control of microgrids, stability aspects of conventional power systems, active distribution network and solar photovoltaic.

Abstract

1 Introduction

2 Modified Virtual Impedance Control and System Under Study

2.1 Modified Virtual Impedance Control

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2.2 System Under Study

3 Simulation Results

3.1 Common Load Case

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3.2 Common Plus Local Load Case

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4 Stability Analysis

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5 Conclusion

References

Biographies