2023
DOI: 10.1109/jsen.2022.3228551
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A Series Arc Fault Diagnosis Method in DC Distribution Systems Based on Multiscale Features and Random Forests

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Cited by 9 publications
(10 citation statements)
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“…DLA refers to the residual angle of the phase angle between the current vector and the voltage vector flowing through the dielectric under an alternating electric field [26], that is, š›æ = 90 ā€¢ āˆ’ arg(I āˆ•U ). From Figure 3, the zero-sequence current flowing through the non-faulty line i can be expressed as shown in Equation (12).…”
Section: Analysis Of the Impact Of Neutral Grounding Methods On Diele...mentioning
confidence: 99%
See 2 more Smart Citations
“…DLA refers to the residual angle of the phase angle between the current vector and the voltage vector flowing through the dielectric under an alternating electric field [26], that is, š›æ = 90 ā€¢ āˆ’ arg(I āˆ•U ). From Figure 3, the zero-sequence current flowing through the non-faulty line i can be expressed as shown in Equation (12).…”
Section: Analysis Of the Impact Of Neutral Grounding Methods On Diele...mentioning
confidence: 99%
“…In Equation (12), Ļ‰ represents the angular frequency of the voltage and current, and the DLA of the non-faulty line i is given by Equation (13).…”
Section: Analysis Of the Impact Of Neutral Grounding Methods On Diele...mentioning
confidence: 99%
See 1 more Smart Citation
“…Many efforts have been done to measure the current variation with time in the range from DC to kHz to detect the slow decrease of the arc current by means of a current shunt [20], a tunneling effect magnetic sensor [22], a lowfrequency current transformer [24], Hall effect probes [25] or commercial current transformers that can reach the range of MHz, [21], [26]. However, these devices do not comply with the constraints of sensitivity, or weight and size imposed by the aeronautic sector.…”
Section: Introductionmentioning
confidence: 99%
“…However, these devices do not comply with the constraints of sensitivity, or weight and size imposed by the aeronautic sector. Other types of sensors require a power supply [22], [24], [25], [27], [28] which could be a problem for this industrial application and should be avoided even when they have good sensitivity. Other authors, [29], use a Rogowski coil but their solution is hardly valid for aircraft systems because requires a shunt capacitor with the load on each monitored circuit and the sensitivity is well below than the proposed sensor in this paper.…”
Section: Introductionmentioning
confidence: 99%