Arc Fault Detection in DC Microgrid Using Deep Neural Network

Author(s):  
Dipti D. Patil ◽  
S Bindu ◽  
SushilThale
2021 ◽  
pp. 1-1
Author(s):  
Jun Jiang ◽  
Wei Li ◽  
Zhe Wen ◽  
Yifan Bie ◽  
Harald Schwarz ◽  
...  

2016 ◽  
Vol 103 ◽  
pp. 129-134 ◽  
Author(s):  
Qingqing Yang ◽  
Jianwei Li ◽  
Simon Le Blond ◽  
Cheng Wang

2020 ◽  
Vol 12 (9) ◽  
pp. 1503
Author(s):  
Yuan Sun

With the continuous popularization of Global Navigation Satellite System (GNSS) in various applications, the performance requirement for integrity is also increasing, especially in the field of safety-of-life. Although the existing Receiver Autonomous Integrity Monitoring (RAIM) algorithm has been embedded in the GNSS receiver as a standard method, it might still suffer from small fault detection and delay alarm problem for time series fault models. In an effort to solve this problem, a Deep Neural Network (DNN) for RAIM, named RAIM-NET, is investigated in this paper. The main idea of RAIM-NET is to propose a combination of feature vector extraction and DNN model to improve the performance of integrity monitoring, with a problem specifically designed for loss function, obtaining the model parameters. Inspired by the powerful advantages of Recurrent Neural Network (RNN) in time series data processing, a multilayer RNN is applied to build the DNN model structure and improve the detection rate for small faults and reduce the alarm delay for the time series fault event. Finally, real GNSS data experiments are designed to verify the performance of RAIM-NET in fault detection and time delay for integrity monitoring.


2021 ◽  
Vol 2021 ◽  
pp. 1-13
Author(s):  
Yiming Zhang ◽  
Hang Zhao ◽  
Jinyi Ma ◽  
Yunmei Zhao ◽  
Yiqun Dong ◽  
...  

A new fault detection scheme for aircraft Inertial Measurement Unit (IMU) sensors is developed in this paper. This scheme adopts a deep neural network with a CNN-LSTM-fusion architecture (CNN: convolution neural network; LSTM: long short-term memory). The fault detection network (FDN) developed in this paper is irrelative to aircraft model or flight condition. Flight data is reformed into a 2D format for FDN input and is mapped via the net to fault cases directly. We simulate different aircrafts with various flight conditions and separate them into training and testing sets. Part of the aircrafts and flight conditions appears only in the testing set to validate robustness and scalability of the FDN. Different architectures of FDN are studied, and an optimized architecture is obtained via ablation studies. An average detecting accuracy of 94.5% on 20 different cases is achieved.


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