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Analysis and Validation of Wavelet Transform Based
DC Fault Detection in HVDC System
Yew Ming Yeapa, Nagesh Geddadaa, Abhisek Ukila
aSchool of Electrical and Electronic Engineering, Nanyang Technological University,
SINGAPORE
Abstract
Fault detection plays an important role in both conventional AC and upcoming
DC power systems. This paper aims to study the application of discrete wavelet
transform (WT) for detecting the DC fault in the high voltage DC (HVDC)
system. The methods of choosing the mother wavelet suited for DC fault is
presented, based on degree of correlation to the fault pattern and the time delay.
The wavelet analysis is performed on a multi-terminal HVDC system, built in
PSCAD/EMTDC software. Its performance is judged for critical parameter
like the fault location, resistance and distance. The analysis is further extended
to validation using results from experiment, which is obtained from a lab-scale
DC hardware setup. Load change, one of the transient disturbances in power
system, is carried out to understand the effectiveness of the wavelet transform to
differentiate it from the DC fault. The noise in the experimental result gives rise
to non-zero wavelet coefficient during the steady-state. This can be improved
by removing the unwanted noise using right filter while still retaining the fault-
induced transient. The wavelet transform is compared with short-time Fourier
transform to highlight the issue with window size and noise.
Keywords: DC fault, wavelet transform, multi-terminal HVDC, modular
multi-level converter, PSCAD/EMTDC, DC system experiment,
time-frequency analysis, fault detection
1. Introduction
High voltage direct current system (HVDC) is one of the important technolo-
gies that have taken the conventional power system in a new direction. While a
lot of research efforts are put into the design of controller and control strategy of
the HVDC system, it is equally important to address the protection issue in the
system so that the damage caused by the fault is brought down to minimum.
IThe work was supported by the Start-Up Grant (M4081547.040), Nanyang Technological
University, Singapore.
Email addresses: yeap0022@e.ntu.edu.sg (Yew Ming Yeap), ngeddada@ntu.edu.sg
(Nagesh Geddada), aukil@ntu.edu.sg (Abhisek Ukil)
The traditional high voltage AC circuit breaker (CB) takes advantage of current
zero crossing which enables it to be tripped in a safe manner. Such phenomenon,
however, is not seen in the DC current. The absence of current zero means that
the mechanism of the breaker in the DC system should be completely different.
Due to lack of such technology, most of the present HVDC systems are restricted
to point-to-point connection, where the AC CB is adequate for protection. The
interest was renewed when ABB [1] and Alstom [2] proposed the hybrid DC CB.
It is arguably one of the key enabling technologies that will potentially pave the
way for the deployment of HVDC system with increasing connections, towards
a multi-terminal DC (MTDC) grid.
Development in power electronics converter technology has been critical for
the advancement of the HVDC system. In comparison with the current source
converter (CSC), the voltage source converter (VSC) is relatively more vul-
nerable to the fault on the DC side due to low DC-side inductance. Rapidly
increasing DC current can damage the devices if the fault is not treated im-
mediately. ABB’s hybrid DC CB [3] is capable of isolating the fault within 5
ms, this poses a challenge to the design of protection algorithm to meet such a
stringent requirement. In addition, as the HVDC system is moving towards the
scale of multi-terminal, locating the faulted line has become another important
aspect of the protection system.
In recent times, DC fault detection methods have gained a significant re-
search attention in the HVDC system. Traveling wave is well established me-
thid in conventional AC power system for its effectiveness in locating the fault
point. Its application on the HVDC system had been studied extensively [4].
This technique, however, requires high sampling rate for data collection in order
to accurately capture the wave-front arrival time. Fault detection based on the
DC current measurement was proposed in the works [5, 6], whereby the rate
of change of DC current (di/dt) forms the basis of fault criterion. While it is
simple and computationally efficient, it has difficulty determining the faulted
section independently as the system becomes highly meshed. DC fault can be
also detected by pattern recognition, in which the measured voltage is compared
with already known signal and the degree of similarity is measured by Pearson
correlation coefficient [7]. However, such method might lack generality. Zheng
et al. [8] reported that DC fault transient in CSC-HVDC system resulted in
generation of certain harmonics, which could be leveraged to form a fault basis.
Due to different operating conditions between CSC and VSC, its application on
the latter remains to be investigated.
The wavelet transform (WT) can be regarded as one of suitable techniques
for processing the non-stationary fault signals [9, 10]. This signal processing
technique is capable of interpreting the signal in time and frequency domain.
WT has also been applied to detect disturbance in conventional AC power sys-
tem [11–16]. One of the benefits of using the WT is that it is able to discrim-
inatingly identify the DC fault against non-concerned disturbances (AC fault
and load change) [17]. Using the WT, the faulted line can be determined in
a meshed network without the need of communication channel, hence substan-
tially reducing the detection time [18]. Abu-Elanien [19] in their work showed
2
that this technique is able to withstand the influence of fault location and fault
resistance to certain extent.
This paper presents a detailed analysis of the wavelet-based method for
detecting and locating fault in DC system, with software and hardware valida-
tions. Protection strategy is not of major focus. Rather, this paper attempts
to thoroughly evaluate the performance of the WT using real fault signals. The
influences of fault location, resistance and distance in the modular multilevel
converter-based (MMC) HVDC system, modeled in PSCAD/EMTDC, are stud-
ied. The inter-terminal communication is opted out, as the wavelet detection
scheme only requires the DC current signal which is locally available in each ter-
minal. The influences of fault resistance and distance are also validated, using
the experimental results obtained from the point-to-point hardware DC system
operating at lab-scale voltage level. This paper also presents how capable is the
wavelet transform when it comes to differentiating DC fault from load change,
which is carried out experimentally. The improvement of the smoothened exper-
imental result using properly designed filter will be discussed. Lastly, the per-
formance comparison between the wavelet transform and the short-time Fourier
transform (STFT) will be presented.
The remainder of the paper is structured in the following manner. In Section
2, the background of DC fault is presented, followed by brief introduction of the
wavelet transform and selection of mother wavelet in Section 3. The simulation
and experimental results are covered in Section 4 and 5, respectively. Finally,
the conclusions are given in Section 5.
2. DC fault in HVDC System
This section briefly explains the DC fault analysis in the MMC-based HVDC
system. The DC fault can be divided into following types: pole capacitor unbal-
ance, pole-to-ground (PG) and pole-to-pole (PP) fault. DC cable is relatively
more vulnerable to the PG fault caused by insulation breakdown than PP fault
[10]. Due to direct exposure to air, the DC overhead line is prone to the oc-
currence of these two faults. PP fault has the potential to result in extremely
destructive damage to the HVDC system. Therefore, it is always considered as
the most representative DC fault in literatures [20], as well as in this paper.
Modeling of MMC and two-level VSC are fundamentally same, in which the
converter station can be represented as DC current source in the DC side. The
combined submodular capacitance Ceis described in (1), under the balanced
condition, and the derivation can be found in [21, 22].
Ce=6C
n.(1)
The DC side equivalent circuit of single MMC is represented in Fig. 1, at the
instant of PP fault occurrence. Icv is the total current injected to the DC side.
The Ldc and Rdc are the π-model equivalent inductance and resistance of the
positive and negative poles. The fault resistance is denoted by Rf. Immediately
3
Figure 1: Equivalent circuit of MMC DC side during DC fault. (a) Stage 1: DC
capacitor discharge stage, (b) Diode freewheeling stage
as the fault current exceeds the threshold, the IGBTs in the submodule will be
blocked. Then, the current flow switches to the freewheeling diodes, which is
shown in Fig. 1(b). By this time, it is important to clear the fault fast enough
before the current reaches beyond the I2tcapacity of diodes.
The fault analysis can be divided into three stages: 1) DC capacitor dis-
charge stage, 2) diode freewheeling stage, 3) AC infeed stage. The discharge of
capacitor (Icap) dominates the fault current in the first few time-instant of fault.
When the DC voltage drops to zero, the AC side will continue supplying current
to the fault point [23, 24]. The fault analysis here only focuses on stage 1 and
2, as these periods are critical for wavelet transform to make fault decision and
dispatch IGBT block signal, preferably within 2 ms.
The circuit in Fig. 1(a) can be represented by (2).
d2Idc
dt2+Re
Le
dIdc
dt+1
LeCe
Idc = 0 (2)
where Re= 2(Rdc/2) + Rfand Le= 2(Ldc /2).
The under-damped response is met on the condition R2
e<(Le/Ce)1/2. As-
suming that the PP fault happens at t0with the initial conditions of Vdc(t0) = V0
and Idc(t0) = I0, the solution of the second-order RLC differential equation is
given as,
Idc(t) = e−δt "I0cos(ωt) +
V0
Le−δI0
ωsin(ωt)#,(3)
Vdc(t) = e−δt "V0cos(ωt) + δV0−I0
Ce
ωsin(ωt)#.(4)
where δ=Re/2Leand ω= (1/LeCe−(Re/2Le)2)1/2.
The DC voltage (Vdc) reaches zero when the DC capacitor (Ce) gets dis-
charged. Now, the fault current (I0
dc) is freewheeling within the three-phase
diodes as the corresponding IGBTs are already blocked, depicted in Fig. 1(b).
The line inductor (Ldc) disallows sudden change of current, therefore the initial
4
current for this stage is Idc(t1) = I0
dc(t1) = I0
0. The circuit is now reduced to a
RL circuit, so the expression of the fault current is given as:
Ldc
dI0
dc
dt+RdcI0
dc = 0.(5)
The first order differential equation is solved:
I0
dc(t) = I0
0e−Rdc
Ldc t.(6)
The I0
dc is equally distributed in three-phase diodes:
ID1(t) = ID2(t) = ID3(t) = I0
dc(t)/3.(7)
3. Wavelet Transform
3.1. Theory
Wavelet transform (WT) is used for fault detection instead of Short Time
Fourier Transform (STFT). While both signal processing techniques are able to
analyze non-stationary signal in time and frequency domain, the window size
of the STFT is fixed. A longer window yields good frequency resolution at
the expense of time resolution, and vice versa. A convenient solution to this
dilemma is the WT, as it automatically changes the window size in response
to the dynamics of the signal. It is able to capture the high frequency abrupt
change, which is specially needed for detecting the fault.
The WT breaks up a signal into the shifted and the scaled versions of the
original (or mother) wavelet, allowing for simultaneous time and frequency anal-
ysis. The continuous wavelet transform (CWT) is defined as the sum over all
time of the signal multiplied by the scaled and shifted versions of the wavelet
function.
CW T (a, b) = Z+∞
−∞
x(t)ψ∗
a,b(t)dt. (8)
ψ∗
a,b(t) = |a|−1/2ψ(t−b
a).(9)
ψ(t) is the mother wavelet, the asterisk in (8) denotes a complex conjugate, and
a, b ∈R, a 6= 0 (Ris the real continuous number system) are the scaling and
the shifting parameters, respectively. The discrete wavelet transform (DWT)
in (10) is given by choosing a=a−
0m/2, b=na−m/2
0b0,t=kT in (8) and (9),
where T= 1.0, and k, m, n ∈Z, (Zis the set of positive integers).
DW T (m, n) = a−m/2
0(Xx[k]ψ∗[k−na−m/2
0b0
am
0
]).(10)
We apply the multiresolution signal decomposition (MSD) [25, 26] technique
to decompose a given signal into detailed and smoothed versions. Let x[n] be a
5
discrete-time signal, then the MSD technique decomposes the signal in the form
of wavelet coefficient at scale 1 into C1[n], the smoothed (time-domain view)
and D1[n], the detailed (frequency-domain view) coefficients.
The decomposition process can be iterated, with successive approximations
being decomposed in turn, so that the original signal is broken down into many
lower resolution components. This is called the wavelet decomposition tree [25,
26], shown in 2. MSD technique can be realized with the cascaded quadrature
mirror filter (QMF) banks [27, 28].
So, for example, using 4-scale decomposition, the original signal scan be
represented as:
x[n] = C4[n] + D4[n] + D3[n] + D2[n] + D1[n].(11)
x[n] LPF
HPF
LPF LPF
HPF
HPF
C1[n] C2[n] Cj[n]
Dj[n]
D2[n]
D1[n]
2
2
2
2 2
2
QMF-1 QMF-2 QMF-j
Input signal
Figure 2: Multiresolution signal decomposition.
3.2. Wavelet Selection
The wavelet coefficient is the cross-correlation of the signal and the mother
wavelet; the higher the wavelet coefficient, the closer the signal matches with
the chosen mother wavelet. Thus, a suitable wavelet should be selected such
that it presents closest match to the pattern of the fault signal. Ma et al.
[29] presented a method to facilitate the wavelet selection by using the Pearson
product-moment correlation coefficient, as represented in (12).
r=Pn
i=1(Xi−¯
X)(Yi−¯
Y)
qPn
i=1(Xi−¯
X)2(Yi−¯
Y)2
(12)
where Xiand Yiare the data sets of the fault signal and the wavelet respectively,
their corresponding averages being ¯
Xand ¯
Y.
In this case, Xiis the fault signal as depicted in Fig. 3, while Yicorresponds
to the chosen Daubechies mother wavelet.
6
0 100 200 300 400 500
4
2
0
2
4
6
8
Fault signal
0 50 100 150 200 250 300 350 400
1.5
1
0.5
0
0.5
1
1.5
2
0 100 200 300 400 500 600 700
1.5
1
0.5
0
0.5
1
1.5
2
0 200 400 600 800 1000
1
0.5
0
0.5
1
1.5
0 200 400 600 800 1000 1200
1.5
1
0.5
0
0.5
1
1.5
0 500 1000 1500
1.5
1
0.5
0
0.5
1
1.5
0 500 1000 1500 2000
1.5
1
0.5
0
0.5
1
1.5
db2 db3 db4
db5 db6 db7
Figure 3: The cross correlation between the fault signal and Daubechies wavelet
of varying orders.
db2 db3 db4 db5 db6 db7 db8 db9
Daubechies wavelet order
0.2
0.25
0.3
0.35
0.4
0.45
0.5
0.55
Pearson correlation coefficient
Figure 4: Correlation coefficient between fault signal and Daubechies wavelet
of order 2-9.
The correlation coefficients between the fault signal and the Daubechies
mother wavelet of varying order (db2−db9) are computed and depicted in Fig.
4. It is found that db3 provides the best match among these candidates for the
given fault pattern.
3.3. Mother wavelet and time delay
Besides having adequate sensitivity to the transient caused by the DC fault,
it is equally important to choose the right mother wavelet that yields high-speed
fault detection. Fig. 5 shows the performance of Haar, Daubechies and Coiflet
mother wavelets for providing the maximum wavelet coefficient and correspond-
ing time delay.
7
Figure 5: Time delay introduced by different mother wavelets.
sfis the time the DC fault-induced transient begins to appear. It is noticed
that compact wavelets work well to localize high frequency components in the
transient with minimum time delay. In this case, Haar and db2-3 are the ideal
mother wavelets because they produce the maximum wavelet coefficients with
no delay. For the Daubechies wavelet family, db5 begins to show delay by one
sample. Coiflet wavelet is inappropriate for DC fault detection as far as speed
is concerned. The analysis here agrees with the finding in Santoso’s work [30],
which reported that db4 and db6 are suitable for fast transient in conventional
AC system.
4. Performance evaluation of wavelet transform - simulation result
Fig. 6 shows the MMC HVDC model consisting of four terminals (MMCi,
i=1, 2, 3, 4) developed in PSCAD/EMTDC. Four strong AC systems (ACi ) are
connected with ring and monopole DC network. The DC lines (Lij,i, j = 1, 2,
8
Figure 6: 4-terminal MMC HVDC model.
Table 1: System data
Parameters Values
Rated power 600 MVA
AC frequency 50 Hz
AC system short circuit ratio 10
Number of submodules per arm 100
Module capacitor 1000 µF
Arm inductor 50 mH
Switching frequency 180 Hz
Length L12, L13, L34, L24 100 km
Length L23 200 km
3, 4), consisting of positive and negative poles, are represented as single line in
the figure. The MMC adopts the detailed equivalent modeling (DEM) [31], with
MMC1 working as fixed DC voltage control and the rest as fixed active power
control. Its corresponding functional control structure will not be elaborated
here, the detail can be found in [21, 32]. The full system data is given in Table
1.
The DC currents (Idcij,i, j = 1, 2, 3, 4) are measured at each terminal
(MMCi). The IGBTs will not be blocked in the simulation as the focus is to
identify the signature associated with fault in the DC current signal. The signals
are exported to MATLAB and post-processed with discrete wavelet transform
algorithm to generate the wavelet coefficients.
The fault location (df ) is the distance from the fault to the monitoring termi-
nal. The fault simulated here is the PP fault, with the fault resistance denoted
as Rf. The sampling rate (fs) is selected based on the available frequency range
offered by digital fault recorder [33]. The mother wavelets to be adopted is db3,
since it has been shown in Section 3 that it presents the closest similarity with
9
fault pattern. The application of wavelet transform on the fault identification
in the multi-terminal system is evaluated by considering the three cases below:
•To study the influence of DC fault location: PP fault on Lij (i, j =
1,2,3,4), Rf= 0.01Ω, df = 50km,fs= 15360Hz, using db3.
•To study the influence of DC fault resistance: PP fault on L12, 0.01 <
Rf<500Ω, df= 50km,fs= 15360Hz, using db3.
•To study the influence of DC fault distance: PP fault on L12, Rf= 0.01Ω,
15 < df<85km,fs= 15360Hz, using db3.
230 235 240 245 250 255 260
Sample number
(a)
-0.5
0
0.5
Wavelet coefficient
230 235 240 245 250 255 260
Sample number
(b)
-0.5
0
0.5
Wavelet coefficient
230 235 240 245 250 255 260
Sample number
(c)
-0.5
0
0.5
Wavelet coefficient
230 235 240 245 250 255 260
Sample number
(d)
-0.5
0
0.5
Wavelet coefficient
230 235 240 245 250 255 260
Sample number
(e)
-0.5
0
0.5
Wavelet coefficient
Idc12
Idc21
Idc13
Idc31
Idc34
Idc43
Idc24
Idc42
Idc23
Idc32
Figure 7: Detailed wavelet coefficient for each DC line current in different PP
fault location. a) L12, b) L13, c) L34, d) L24, e) L23.
4.1. Influence of DC fault location
Fig. 7 shows the wavelet coefficient obtained from the PP fault simulated
on the DC lines in the multi-terminal HVDC system. The PP fault is initiated
by shorting the positive and the negative DC lines through a fault resistance.
Therefore, only the wavelet coefficient for positive pole DC current is presented
here.
The wavelet coefficient remains low during the steady-state, approximating
to zero. The occurrence of fault on a DC line is detected when the DC current of
10
the faulted line generates a high wavelet coefficient abruptly. To illustrate, PP
fault on L13 (see Fig. 7(b)) generates large overcurrent in fault current between
MMC1 and MMC3, resulting in high wavelet coefficients for Idc13 and Idc31.
Similar pattern is observed in other cases. With the high wavelet coefficient
obtained at 243th sample, the fault is detected with a time delay of 1.09 ms.
Additionally, the wavelet transform allows the healthy terminals to recognize
that the fault is outside their protection zone, since the wavelet coefficients of
their currents remain consistently low.
The discriminative nature of wavelet transform has been validated. It is a
reliable method for each terminal to independently identify the fault by just
monitoring the DC current.
10-2 10-1 10 010110210 3
Fault resistance (Ω)
0
0.1
0.2
0.3
0.4
0.5
0.6
Maximum wavelet coefficient
Idc12
Idc21
Idc13
Idc31
Idc34
Idc43
Idc24
Idc42
Idc23
Idc32
Figure 8: Effect of PP fault resistance on detailed wavelet coefficient for each
DC line current.
4.2. Influence of DC fault resistance
This subsection studies the robustness of the WT to detect the high resis-
tance fault in a multi-terminal HVDC system. Fig. 8 shows the trend of the
wavelet coefficients of DC currents as the fault resistance on L12 is increased
from 0.01 Ω to 500 Ω.
The wavelet coefficient appears to be constantly high for the PP fault re-
sistance ranging from 0.01 Ω to 5 Ω. Beyond that, however, the value begins
to show downward trend. This can be explained by the fact that fault induced
transient has been dampened by large fault resistor. As a consequence, the
wavelet coefficient decreases with increasing fault resistance. Nevertheless, the
wavelet coefficient of fault current remains vastly above that of healthy DC
current by large margin.
4.3. Influence of DC fault distance
The fault-induced transient is the function of fault location. If a DC fault
happens in close proximity to a terminal, the DC current of that terminal will
experience bigger frequency change and higher magnitude. Fig. 9 shows the
11
Idc12
df=85 km
Idc21
df=15 km
Figure 9: Line current (a) Idc12 , (b) Idc21 and their corresponding detailed
wavelet coefficient (c), (d) under the influence of fault distance. df =15km and
df =85km are represented by black line and red dashed line, respectively.
wavelet coefficients of Idc12 and Idc21 as the location of PP fault (df ) is adjusted
from 15 km to 85 km away from MMC1 along L12.
Fig. 9(a)&(b) illustrates the relationship between the change of DC current
and fault location. The current magnitude decreases and the transient becomes
dampened as the fault point increases. This phenomenon is reflected in their
wavelet coefficients. For example, the fault at df =85km yields the wavelet coeffi-
cient about -0.2342 for Idc12 and -1.389 for Idc21. Despite diminished sensitivity,
the fault can be successfully detected for all distances evaluated.
5. Performance evaluation of wavelet transform - experimental result
Laboratory DC system experiment setup is developed to study DC fault
with variation of fault parameters. The schematic block diagram of the setup
is shown in Fig. 10 and various parameters, ratings are given in Table 2.
Experimental studies are performed at input voltage of 85 V (line rms).
Three phase, 30 kVA, (0-450) V, variable transformer was used to set the desired
input voltage of 85 V. Converters (VSC1,VSC2 ) at the DC side are rated at
30 kVA, 415 V.
The voltage and current quantities at power level are converted to signal
level using hall effect voltage (±500 V to ±15 V) and current (±10 A to ±4
V) transducers. These signals are fed to the dSPACE 1103 controller through
12
VSC1 VSC2
DC MCBDC MCB
DC MCB
DC MCB
Pole1
Pole2
2dc
v
ic2
ib2
ia2
2abc
i
1dc
v
idc1
Voltage andCurr ent
TransducerSensor
Board
R
la
R
lb
R
lc
Lf2
2abc
v
idc2
VariablePower
Resistor
R
f2
SwitchingPulses V SC1 SwitchingPulses V SC2
BKR2
Voltage andCurr ent
TransducerSensor
Board
Filter
Inductor
Variable
Transformer
1abc
v
1abc
i
Lf1
R
f1
Three
PhaseAC
Protection
BoardL
MCCB
Upstream
laboratory
MCB1
vsb
ThreePhase
415V50Hz
vsa
vsc
isa
isb
isc
Laboratory
Threephase
Supply Side
Dspace11v3Controller
interfaceto PC
BKR1
Filter
Inductor
T1 T2
1a
i
1b
i
1c
i
2abc
v
f
i
R
1L1L2
R
2
R
3L3
R
f=2
R
4L4
Fdc12
DC Regulated
Supply
VSC2
VSC1
Filter
Inductor
PC for Dspace
Interface
DC line
Resistive Load
Filter
Inductor
Autotr ansformer
Figure 10: Schematic diagram of two-terminal DC system and photograph of
laboratory setup.
Table 2: Experiment Setup Parameters
Parameters Values
Supply voltage 3φ, 85 Vrms , 50 Hz
3φAC Protection Board 40 A, B Type, TP MCB with Shunt trip
3φVariable Transformer 30 kV A, (0-415) V
Converters (VSC1, VSC2) 30 kV A, 400 V
DC Capacitor Cdc = 2350 µF ,
DC Line Paramters Ld= 1.5 mH,Rd= 0.03 Ω
DC MCB C60H-DC, C 4 A
Interface Filter Parameters Rf= 0.1 Ω, Lf= 10 mH
Linear Load Rl= 20 Ω
Variable Power Resistor 5000 W, (1-16) Ω
DC Solid State Relay D2D40, 200 V, 40 A
analog to digital channels (ADCH) ports. The control algorithm is developed
in MATLAB/Similink and converted for the dSPACE hardware interface by
13
the means of Real Time Interface (RTI) toolbox. The pulse-width modulation
(PWM) gating pulses generated by the controller are fetched to the VSCs for
switching.
Figure 11: (a)Experimental result for 2 Ω DC fault; (b)Wavelet coefficients for
Idc12 and Idc21.
Direct short-circuit across the DC line is not viable as the large fault current
could trigger the tripping of main circuit breaker in the laboratory. In order to
limit the magnitude of the fault current, a power resistor is inserted between
upper and bottom DC line and the connection is controlled by a DC solid-state
relay. During the startup of experiment, the relay remains open. When the sys-
tem has achieved steady-state, the relay will be closed to electrically establish
a connection across DC line via power resistor. The value of the resistance is
adjustable from 1 Ω to 16 Ω.
Fig. 11 shows the measurements of Iac1,Vdc1,Idc12 and Idc21, in that or-
14
der on LeCroy Wavesurfer 3024 oscilloscope, for 2 Ω DC fault. The sampling
frequency used in the measurement is 10 kHz. The signals of interest here are
Idc12 and Idc21. The segment in dashed box is zoomed in to better visualize
the fault-induced transient. The corresponding wavelet analysis using db3 is
presented in the same figure.
One can immediately notice that the steady state DC currents essentially
do not yield zero wavelet coefficient as seen in the simulation results. The value
falls between [w1,w2 ], marked by the dashed line. For now we take [w1,w2 ] as
threshold, it will be discussed in subsection later how removing the noise in the
signal can reduce the steady state wavelet coefficient.
As expected, abrupt increase of current caused by the DC fault registers high
wavelet coefficients for both currents. The fault inception time (3s) is translated
to 1877th sample at 4th level of decomposition. The highest wavelet coefficient
is obtained by one sample delay. Even with the delay introduced by filtering,
the detection time would still be reasonably short.
5.1. Influence of DC fault resistance
Figure 12: Wavelet coefficient for DC fault of varying fault resistance (a) 4 Ω;
(b) 6 Ω; (c) 8 Ω; (d) 10 Ω; (e) 12 Ω; (f) 14 Ω.
Similar to the Section 4.2, repeated experiments are carried out to evaluate
the performance of wavelet transform for different fault resistance, ranging from
4 Ω to 14 Ω. Fig. 12 depicts the result of wavelet analysis on the DC currents
(Idc12 &Idc21).
15
The faults are detected for all fault resistances evaluated. The highest
wavelet coefficient is observed around sample number 1878 (equivalent to 3.0016
s). Despite the presence of noise in the signal, the wavelet coefficients are kept
within the presumed threshold, marked by the dashed line in the figures, during
steady-state. The wavelet coefficient shows downward trend when increasing the
fault resistance. Nevertheless, a reasonably big margin between the threshold
and the wavelet coefficient still justifies the effectiveness of the WT in detecting
the DC fault.
5.2. Influence of DC line length
Figure 13: DC line represented by RL circuit in experiment and different line
length to be investigated.
Similar to the Section 4.3, our interest is to study the effect of fault distance
on the WT at experimental level. Besides the fault location, the frequency
content of the transient is also a function of the DC line length. Three tests
with different combination of inductance representing different fault location
and DC line length are carried out, as shown in Fig. 13. The DC currents are
analyzed with the WT and the result is shown in Fig. 14.
The WT successfully detects the DC fault with the wavelet coefficient ex-
ceeding the threshold by large margin. One can observe that the terminal closer
to the fault has current yielding the higher wavelet coefficient than its counter-
part. For example, in Test 3, smaller L2and L4implicates the fault to be closer
to the VSC2, and the fault at this location results in higher wavelet coefficient
for Idc21 compared to Idc12. Nevertheless, the two terminals are able to rec-
ognize the occurrence of DC fault as their maximum wavelet coefficients are
consistently higher than threshold for all fault locations evaluated.
16
Figure 14: Wavelet coefficient for DC fault of varying fault location (a) Test 1;
(b) Test 2; (c) Test 3.
5.3. Influence of other type of power system disturbance
Figure 15: Experimental result and wavelet analysis for (a) DC fault; (b) Load
change.
17
Load change in power system results in current increase that could be mis-
taken for DC fault. This subsection aims to study the feasibility of the WT
in differentiating between DC fault and load change. To reproduce this phe-
nomenon at experimental level, the resistive load at receiving end is reduced
abruptly such that it generates a transient that reaches the same peak as fault-
induced transient. The results from the experiment and the corresponding
wavelet coefficients are shown in Fig. 15.
As expected, the Idc12 in DC fault produces high wavelet coefficient. Al-
though the load change causes transient in the DC current, its wavelet coeffi-
cient appears to increase not very much, barely crossing the presumed threshold.
Thus, it is now clear that the DC fault can be differentiated from the load change
using the WT.
5.4. Influence of signal noise
Figure 16: (a) Raw and denoised signal for DC fault at 14 Ω; (b) Wavelet
coefficient for denoised signal.
The signal measured directly from the experiment contains the noise amount-
ing to 11.421 dB signal-to-noise ratio (SNR). The noise gives rise to non-zero
wavelet coefficient during steady state. However, the wavelet coefficient appears
to stay within the presumed threshold in all the studies so far. This subsection
investigates on filtering the noise.
The Idc12 for DC fault at 14 Ω is smoothened with bandstop filter so as to re-
tain the fault-induced transient which is of high frequency and critically needed
18
for detection. The denoised signal now has 27.658 dB SNR during steady-state.
Fig. 16 depicts the difference between raw and denoised signal. When ana-
lyzed with the WT, it is noticed that the steady-state wavelet coefficient has
decreased substantially (see Fig. 16(b)), compared to that in Fig. 12(f). Fur-
thermore, the maximum wavelet coefficient does not deviate much as a result of
filtering, proving that the fault transient in the denoised signal is still preserved.
Hence, an appropriate filtering is highly recommended if one wants to keep the
steady-state wavelet coefficient as low as possible.
5.5. Comparison with short-time Fourier transform method
Figure 17: Frequency spectrum of experimental fault current for window length
(a) 16, (b) 32 and (c) 64. Zero-crossing frequency bin is marked by dash line.
The problem with choosing the window size for STFT has been discussed in
Section 3. For the purpose of fast fault detection, small window is preferable
at the expense of frequency resolution. The STFT analysis of high frequency
components in transient signals was reported in [34]. During steady-state, the
frequency spectrum of constant DC current should resemble a sinc function,
with the main-lobe concentrated at 0 Hz, with side-lobes uniformly distributed.
A key feature in the frequency spectrum is the zero-crossing frequency bin. Con-
sidering nas window size in term of sample number, the zero-crossing frequency
bin appears at 2fs/n, 3fs/n, 4fs/n and so on. When the DC fault happens, the
high-frequency transient will have its signal energy leak into other frequencies,
causing visible distortion across the side-lobes. Based on this phenomenon, the
fault can be detected by tracking the magnitude of zero-crossing frequency bin,
which will increase under the fault condition.
The frequency spectra of experimental fault current (Idc12) for 16, 32 and
64-sample window lengths using Hanning window are shown in Fig. 17.
1. 16-sample: The first zero-crossing frequency bin for this window is 1250
Hz. It can be seen that the side-lobes has already experienced slight
distortion caused by signal noise even before the fault occurrence. The
zero-crossing frequency bin increases above 0 dB (threshold) at 0.8 ms
after the fault inception. At which time, the fault is successfully detected.
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2. 32-sample: The influence of noise is comparatively less significant for this
window size, given that the side-lobes retain equiripple-like pattern dur-
ing pre-fault. The first zero-crossing frequency bin (625 Hz) exceeds the
threshold with a time delay of 1.6 ms.
3. 64-sample: Similar to 16-sample window, the side-lobes are heavily dis-
torted by the noise during pre-fault. The fault is detected when the first
zero-crossing frequency bin (312.5 Hz) increases above threshold after 3.2
ms.
It is observed that the detection time is very much dependent on the window
size. 16-sample window provides the fastest detection. However, the signal
noise can cause significant distortion making the tracking of frequency difficult.
The influence of noise is also observable in 64-sample window while 32-sample
window is minimally affected. The STFT is met with the difficulty of choosing
the window size. The wavelet transform, on the other hand, can adjust the
window size automatically to suit the fault signal. In addition, as part of the
process of cascaded filtering, the wavelet transform is able to preserve the critical
signal while eliminating noise, but this cannot be done by the STFT.
6. Conclusion
The application of the wavelet transform to detect and identify the DC
fault in HVDC system has been analyzed and validated using simulation and
experimental results. db3 is adopted in the wavelet analysis as it presents the
closest match to the fault pattern and is able to detect fault with minimal delay.
The simulation result shows that the wavelet transform is able to indepen-
dently detect the faulted line in a 4-terminal HVDC system, only using the
wavelet coefficient for the DC line current at each terminal as criterion. The
detection time is approximately 1 ms. The value of the wavelet coefficient de-
creases as the fault resistance and the fault distance are increased, however it
is still well above the threshold by large margin.
From the experimental results, it can be inferred that the wavelet transform
also presents reasonable robustness to the influence of fault resistance and dis-
tance. It is not sensitive to the transient caused by load change, allowing to
classify the DC fault from other types of disturbances. The inherent noise in
the experimental result yields a non-zero wavelet coefficient, thus the threshold
needs to be set above that so as to avoid wrong detection. The steady-state
wavelet coefficient can be vastly reduced by smoothening the raw signal. The
filter has to be properly designed so that only the unwanted noise is removed
while the fault-induced transient, which is of high frequency, is still preserved.
Compared to the short-time Fourier transform (STFT), the wavelet transform
provides better flexibility when it comes to selecting window size and tolerance
against noise.
20
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