# Enhancing LVRT Capability of DFIG-Based Wind Turbine Systems with SMES Series in the Rotor Side

Authors: Xiao Zhou; Yuejin Tang; Jing Shi
Journal: International Journal of Rotating Machinery
 (2017)

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## Abstract

The necessary Low Voltage Ride Through (LVRT) capability is very important to wind turbines. This paper presents a method to enhance LVRT capability of doubly fed induction generators- (DFIGs-) based wind turbine systems with series superconducting magnetic energy storage (SMES) in the rotor side. When grid fault occurs, series SMES in the rotor side is utilized to produce a desired output voltage and absorbs energy. Compared with other methods which enhance LVRT capability with Superconducting Fault-Current Limiter-Magnetic Energy Storage System (SFCL-MESS), this strategy can control the output voltage of SMES to suppress the transient AC voltage component in the rotor directly, which is more effective and rapid. Theoretical study of the DFIG under low voltage fault is developed; the simulation results are operated by MATLAB/Simulink.


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## Body

## 1. Introduction

Wind energy generation has experienced a fast development in the last two decades [1]. DFIG is the most widely used wind turbine, but it is vulnerable to low voltage fault. Many wind turbines trip off from the grid due to the lack of LVRT capability [2].There are many enhanced ways to solve this problem. Crowbar is a commonly used protection method to implement the LVRT capability [3–5]; it can effectively suppress overvoltage and overcurrent but it needs to absorb a large amount of reactive power from the grid, which will do harm to the grid. Improving control strategy of grid converter or rotor converter has been studied by many researchers [6–8], but it cannot work effectively when deep voltage drop occurs. Energy storage device is suitable for dynamic matching of intermittent wind power. The use of supercapacitors or batteries for WTGs has been studied by some researchers [9–11]. SMES used in DFIGs to reduce power fluctuation and alleviate the influence on power quality has been studied in some papers [12]. The application of SFCL-SMES in the rotor side of the DFIG has been carried out. But it is connected with the DFIG through a three-phase diode rectifier; thus the SFCL-MES is inserted into rotor circuit as an impedance, which will not provide help in enhancing the controllability of the RSC.This paper presents a new method to enhance LVRT capability of DFIG with SMES. SMES, with its high efficiency and quick response ability to power compensation, could be a good choice for ESD in DFIG. Most studies applied ESD to solve the problem which are usually in parallel with the DC side. The proposed method in this paper is to generate a desired output voltage utilizing series SMES in the rotor side. Through the analysis of the rotor side voltage under low voltage fault, counter-electromotive force generated by SMES can counteract overvoltage and then overcurrent quickly and effectively. The mathematical model of DFIG will be illustrated first. Then, behavior of the DFIG in normal situation and under low voltage fault will be analyzed and the control strategy of VSC-SMES will be introduced.


## 2. Math Model of DFIG

The stator windings of the DFIG wind turbine are directly connected to the grid. The rotor winding is connected to the grid via back-to-back transformers, where the converter near the grid side is called grid sided converter (GSC) while near the rotor side converter it is called rotor sided converter (RSC). The stator voltage is provided by the grid. The rotor voltage is provided by the back-to-back transformers, which can be adjusted in frequency, phase, and amplitude.In this paper, the control system is implemented considering a stator voltage oriented (SVO) control philosophy in thed/q reference frame [13]. In this kind of systems, the d/q-axes are aligned with the stator voltage. Thus, the park model of the DFIG can be expressed as follows:(1)udr=Rridr+dψdrdt-ω1-ωrψqruqr=Rriqr+dψqrdt+ω1-ωrψdruds=Rsids+dψdsdt-ω1ψqsuqs=Rsiqs+dψqsdt+ω1ψdsψds=Lsids+Lmidrψqs=Lsiqs+Lmiqrψdr=Lmids+Lridrψqr=Lmiqs+Lriqr,where ψ is the magnetic flux, L is the inductances, u and i are voltage and current, respectively, R is the resistance, subscripts s,r,m represent the stator, rotor, and mutual, respectively, and ω1 and ωr are the synchronous and rotating angular frequencies (ωs=ω1-ωr).Once there is a grid fault, the stator voltage will change immediately because it is connected to the grid directly. But, according to the principle of flux conservation, the amplitude of stator flux will not transition. At the moment when the voltage drops, the stator flux linkage contains an AC component and a DC component, which will induce overvoltage in rotor side with different frequencies.As analyzed in [14], the rotor back EMF voltage can be expressed as follows:(2)urdq=jLmLsωsψs2dq-jLmLsωrψs0dq-ψs2dqe-σte-jωst,where ψs0dq and ψs2dq are normal-state stator flux and fault-state stator flux. The rotor back EMF voltage is mainly decided by part two of (2) because the slip frequency is much smaller than rotor frequency. And the second part in (2) is decided by the stator flux which can be several times the default value.


## 3. Methodology of DFIG and SMES Model

Unlike SFCL-MES, this paper controls the SMES output voltage through converter switch control, which could suppress the overvoltage in rotor side.The topology of the whole system is shown in Figure1. SMES is connected to the rotor side by a Voltage Source Converter (VSC). Topology of VSC-SMES is given in Figure 2. SMES can exchange active and reactive power with the system quickly and independently [13].Figure 1
Topology of the whole system.Figure 2
Topology of VSC-SMES.In the case of normal power supply, SMES is in standby mode. In this case, the series SMES will introduce resistance and reactance to DFIG. Thus the rotor voltage will not equate to rotor converter voltage. As shown in Figure3, Ri and Li are the introduced resistance and reactance, respectively. In order to eliminate the influence of the rotor voltage by series SMES, the control of series SMES is to realize(3)ur=urc.Figure 3
Equivalent circuit of the series SMES.When low voltage fault occurs, the SMES outputs the voltage to suppress the rotor back EMF voltage induced by stator; thus the rotor current is supposed to be zero when fault occurs and the rotor back EMF voltage induced by statoru∗r can be shown as follows:(4)u∗dr=Lmdidsdtu∗qr=Lmdiqsdt.The stator current under grid fault after doing Laplace transform can be expressed as follows [15]:(5)ids=Ls+Rsuds+ω1LsuqsLs2s2+2LsRss+Rs2+ω12Ls2-Lss2+Rss+ω12LsLmidr-Rsω1LmiqrLs2s2+2LsRss+Rs2+ω12Ls2iqs=Ls+Rsuqs-ωsLsudsLs2s2+2LsRss+Rs2+ω12Ls2-Lss2+Rss+ω12LsLmiqr+Rsω1LmidrLs2s2+2LsRss+Rs2+ω12Ls2.Considering thatR2s,RsωsLm are approximately 0, the equation can be simplified as:(6)ids=1Ls2Lss+Rss2+2Rs/Ls+ω12·uds-LmLs·idriqs=1Ls2-Lsω1s2+2Rs/Ls+ω12·uds-LmLs·iqr.According to the above analysis, if the rotor side converter could provide relative excitation voltage tou∗r, the low LVRT capability of DFIG will be enhanced. Thus set u∗r as the reference voltage of VSC-SMES under grid fault. The VSC-SMES reference voltage calculation process is presented in Figure 5.


### 3.1. SMES Control

#### 3.1.1. VSC Control

As shown in Figure2, through the park transformation, the mathematical model of VSC in the dq reference frame is expressed as follows:(7)Ldiddt=-Rid+ωLiq+usd-uDCsdLdiqdt=-Riq-ωLid+usq-uDCsqCduDCdt=32iqsq+idsd-ichopper.The current inner loop control of VSC adopts the internal model control strategy [14]; the control block diagram is shown in Figure 4. The closed-loop transfer function of the current inner loop is(8)Wcis=1Tf2s2+2ξTfs+1.Figure 4
The current inner loop control stratagem.Figure 5
The control stratagem for SMES.For achieving the purpose of rapid response of the current inner loop, letTf be equal to 0.0002 s.


#### 3.1.2. DC-DC Chopper Control

Chopper has two basic modes of operation: (1) magnetizing mode; (2) releasing magnetic mode. The mathematical model of chopper is(9)Lscdimagdt=-Rscimag+D1+D2-1uDCCduDCdt=-D1+D2-1imag+iDC,where imag is the current of magnet and D is the switch state of each switch; if switch 1 is on, D1 is equal to 1.In normal operation, the control of chopper is to limit the magnet current in a setting scale. When low voltage fault happens, the control of chopper is to maintain the stability of the DC voltage. The control strategy of SMES is shown in Figure5.


### 3.2. RSC Control

In normal operation, the control ofd/q component of rotor current is to control the active and reactive power of DFIG. Generally, the purpose of control system is to obtain the max wind power.The essence of the maximum wind energy tracking is to control the DFIG output active power and control electromagnetic torque to achieve the best speed control. When the mechanical output of the wind turbine achieves maximum output power, the reference active power of DFIGPs∗ is equal to stator power Ps, as shown as follows:(10)Ps∗=11-sPmax-Pms-Pcus,where Pms is the mechanical loss of wind turbine and Pcus is the copper loss of stator, which is related to Is and Rs. After doing identity transformation, (9) can be expressed as follows:(11)APs∗2+BPs∗+C=0A=Rs3Us2,B=1,C=1s-1kwωw3-Pms+Rs3Us2Qs.The reactive reference power valueQs∗ can be calculated by achieving the lowest loss of DFIG or improving the system’s ability to regulate power. In this paper, Qs∗ is calculated to achieve the lowest loss of DFIG. Thus the expression of Qs∗ is shown as follows:(12)Qs∗=-3XsRrUs2RsXm2+RrRs2+RrXs2.The reference power calculation model of DFIG is shown in Figure6.Figure 6
Reference power calculation model of DFIG.When a fault occurs, the control strategy of rotor converter is irrelevant. Considering SMES will absorb the wind energy,i∗dr and i∗qr can be set to zero to prevent the energy through the converter. Thus, the capacitor in DC side will not absorb a lot of energy and its voltage will not increase sharply. The control stratagem of RSC, in normal situation and when voltage drop happens, is shown in Figure 7.Figure 7
Control block diagram of the RSC.


### 3.3. GSC Control

The purpose of GSC control is to maintain DC capacitor voltage stability and control the factor of input power. The GSC control system is divided into two parts: the outer voltage loop and the inner current loop, which is shown in Figure8. Compensation of load disturbances is achieved by feedforward of the load current iload. System is decoupled by introduced current state feedback w1Lgigd, w1Lgigq.Figure 8
Control block diagram of the GSC.


## 3.1. SMES Control

### 3.1.1. VSC Control

As shown in Figure2, through the park transformation, the mathematical model of VSC in the dq reference frame is expressed as follows:(7)Ldiddt=-Rid+ωLiq+usd-uDCsdLdiqdt=-Riq-ωLid+usq-uDCsqCduDCdt=32iqsq+idsd-ichopper.The current inner loop control of VSC adopts the internal model control strategy [14]; the control block diagram is shown in Figure 4. The closed-loop transfer function of the current inner loop is(8)Wcis=1Tf2s2+2ξTfs+1.Figure 4
The current inner loop control stratagem.Figure 5
The control stratagem for SMES.For achieving the purpose of rapid response of the current inner loop, letTf be equal to 0.0002 s.


### 3.1.2. DC-DC Chopper Control

Chopper has two basic modes of operation: (1) magnetizing mode; (2) releasing magnetic mode. The mathematical model of chopper is(9)Lscdimagdt=-Rscimag+D1+D2-1uDCCduDCdt=-D1+D2-1imag+iDC,where imag is the current of magnet and D is the switch state of each switch; if switch 1 is on, D1 is equal to 1.In normal operation, the control of chopper is to limit the magnet current in a setting scale. When low voltage fault happens, the control of chopper is to maintain the stability of the DC voltage. The control strategy of SMES is shown in Figure5.


## 3.1.1. VSC Control

As shown in Figure2, through the park transformation, the mathematical model of VSC in the dq reference frame is expressed as follows:(7)Ldiddt=-Rid+ωLiq+usd-uDCsdLdiqdt=-Riq-ωLid+usq-uDCsqCduDCdt=32iqsq+idsd-ichopper.The current inner loop control of VSC adopts the internal model control strategy [14]; the control block diagram is shown in Figure 4. The closed-loop transfer function of the current inner loop is(8)Wcis=1Tf2s2+2ξTfs+1.Figure 4
The current inner loop control stratagem.Figure 5
The control stratagem for SMES.For achieving the purpose of rapid response of the current inner loop, letTf be equal to 0.0002 s.


## 3.1.2. DC-DC Chopper Control

Chopper has two basic modes of operation: (1) magnetizing mode; (2) releasing magnetic mode. The mathematical model of chopper is(9)Lscdimagdt=-Rscimag+D1+D2-1uDCCduDCdt=-D1+D2-1imag+iDC,where imag is the current of magnet and D is the switch state of each switch; if switch 1 is on, D1 is equal to 1.In normal operation, the control of chopper is to limit the magnet current in a setting scale. When low voltage fault happens, the control of chopper is to maintain the stability of the DC voltage. The control strategy of SMES is shown in Figure5.


## 3.2. RSC Control

In normal operation, the control ofd/q component of rotor current is to control the active and reactive power of DFIG. Generally, the purpose of control system is to obtain the max wind power.The essence of the maximum wind energy tracking is to control the DFIG output active power and control electromagnetic torque to achieve the best speed control. When the mechanical output of the wind turbine achieves maximum output power, the reference active power of DFIGPs∗ is equal to stator power Ps, as shown as follows:(10)Ps∗=11-sPmax-Pms-Pcus,where Pms is the mechanical loss of wind turbine and Pcus is the copper loss of stator, which is related to Is and Rs. After doing identity transformation, (9) can be expressed as follows:(11)APs∗2+BPs∗+C=0A=Rs3Us2,B=1,C=1s-1kwωw3-Pms+Rs3Us2Qs.The reactive reference power valueQs∗ can be calculated by achieving the lowest loss of DFIG or improving the system’s ability to regulate power. In this paper, Qs∗ is calculated to achieve the lowest loss of DFIG. Thus the expression of Qs∗ is shown as follows:(12)Qs∗=-3XsRrUs2RsXm2+RrRs2+RrXs2.The reference power calculation model of DFIG is shown in Figure6.Figure 6
Reference power calculation model of DFIG.When a fault occurs, the control strategy of rotor converter is irrelevant. Considering SMES will absorb the wind energy,i∗dr and i∗qr can be set to zero to prevent the energy through the converter. Thus, the capacitor in DC side will not absorb a lot of energy and its voltage will not increase sharply. The control stratagem of RSC, in normal situation and when voltage drop happens, is shown in Figure 7.Figure 7
Control block diagram of the RSC.


## 3.3. GSC Control

The purpose of GSC control is to maintain DC capacitor voltage stability and control the factor of input power. The GSC control system is divided into two parts: the outer voltage loop and the inner current loop, which is shown in Figure8. Compensation of load disturbances is achieved by feedforward of the load current iload. System is decoupled by introduced current state feedback w1Lgigd, w1Lgigq.Figure 8
Control block diagram of the GSC.


## 4. Economic Analysis

Compared to other energy storage devices, SEMS has the advantage of high response speed, high efficiency, high-power density, and high cycle life characteristics. But the application of SMES in DFIG will increase the cost of the system. Therefore, the capital cost of SMES applied in DFIG is an indispensable part of DFIG’s technical performance. In terms of energy storage devices, the capital costs contain energy cost $/kWh, power cost $/kW, and cycle cost. As the energy storage device is used in DFIG, high-power characteristic is necessary. The power costs of SMES are less than their energy costs, and this is an indication that they are suitable for high-power applications. Table1 shows the cost comparison for the storage technologies [16]. As can be seen from the table, SMES has a lower power cost compared to pumped-hydro storage, lithium-ion batteries and other energy storage devices. In addition, the long life of SMES makes it possible to participate in the protection of the entire life of the DFIG. In general, considering the economic and other technical performances, SMES is a good choice for ESD in DFIG.Table 1
Cost comparison for the storage technologies.
ESD
Capacity
Life
Power cost ($/kW)
Energy cost ($/kWh)
Pumped-hydro storage
100–2000 MW
>20 years
2000–4300
10–100
Compressed-air energy storage
100–300 MW
>20 years
400–1000
2–50
Flywheel energy storage
5 kW–1.5 MW
>15 years
250–350
1000–10000
Lithium-ion batteries
1–1000 kW
3000 cycles
1000–3000
1000–3800
Supercapacitors
1–100 kW
>50000 cycles
100–300
300–2000
Superconducting magnetic energy storage
10–500 kW
>20 years
200–400
500–1000
Vanadium redox battery
<10 MW
10–30 years
600–1500
150–1000


## 5. Simulation Analysis and Conclusion

The simulations are carried out in MATLAB/Simulink. The simulation parameters are shown in Table2. The simulation parameters of SMES are shown in Table 3. The purpose of the simulation is to observe the performance of the back-to-back converter when the grid fault occurs.Table 2
DFIG parameters.
Symbol
Name
Quantity
S
N
Capacity
1.5 MW
f
N
System frequency
60 Hz
R
s
Stator resistance
0.016 p.u.
L
l
s
Stator leakage inductance
0.16 p.u.
R
r
Rotor resistance
0.016 p.u.
L
l
r
Rotor leakage inductance
0.16 p.u.
L
m
Magnetizing inductance
2.9 p.u
S
b
Base capacity
1.5/0.9 MVA
f
b
Base frequency
60 Hz
V
s
_
n
o
m
Base stator voltage (Vrms)
575 V
V
r
_
n
o
m
Base rotor voltage (Vrms)
1975 VTable 3
SMES parameters.
Parameter
Value
HTS material
Bi 2223
Capacity
40 kJ/600 kW
Magnet inductance (L)
0.5 H
Magnet resistance
2 × 10−5 Ω
Filter capacitance (C)
0.02 F
Series transformer ratio
1
Transformer resistance
1 × 10−4 ΩThe transient grid voltage fault occurs at 0.7 s and lasts for 300 ms. The grid voltage during fault drops to 0. The grid voltage is shown in Figure9. Figures 10 and 11 compare the currents of stator converter and rotor converter with and without SMES. When there is no SMES, in the moment of low voltage faults, the overcurrent of the stator and rotor side converters is almost five times larger than the normal operating range. With the proposed method, the currents of back-to-back converters are always in the affordable range. Moreover, as shown in Figure 13, the DC capacitor voltage is well suppressed during the fault. The output voltage of SMES in d/q frame is shown in Figure 12. The base voltage is the same as base rotor voltage. Figure 14 shows the transient SMES current response.Figure 9
The grid voltage.
(a)
(b)Figure 10
(a)
The current of stator converter with SMES
(b)
The current of stator converter without SMESFigure 11
(a)
The current of rotor converter with SMES
(b)
The current of rotor converter without SMESFigure 12
The SMES output voltage.
(a)
(b)Figure 13
The DC voltage.Figure 14
The magnet current of SMES.Compared to traditional control stratagems, the new control strategy with SMES can suppress the overcurrent in stator and rotor within the affordable range even when grid voltage drops to 0. The DC bus voltage can also be limited effectively.This paper presents a new control stratagem to enhance the LVRT capability of DFIG with series SMES. By controlling the SMES output voltage with the proposed controller, the converter currents and capacitor voltage in fault are suppressed effectively. The method has been validated by simulations in MATLAB/Simulink.



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