TY - GEN
T1 - Embeddings for the Identification of Aircraft Faults (MERIT)
AU - Elshrif, Mohamed
AU - Rizzo, Stefano Giovanni
AU - Betz, Franz D.
AU - Margineantu, Dragos D.
AU - Zaki, Mohammed J.
AU - Chawla, Saniav
N1 - Publisher Copyright:
© 2018 IEEE.
PY - 2018/8/27
Y1 - 2018/8/27
N2 - Vector representation concept proves its success in solving many real-world problems from a variety of applications. In this paper, we built a novel vector representation model for avionics system for two types of fault messages called MERIT. This new model aims to identify the relationship between the flight deck effects (FDEs) and the maintenance messages (MMSGs) through calculating the embedding co-occurrence matrix between them within a predefined flight leg window. The a vector space embeddings representation of MERIT is able to differentiate between the strong and weak relationship between messages. Moreover, we benefit from the negative sampling method to incorporate the weak relationship between the FDEs and MMSGs from different subsystems (chapters) in assessing this relationship precisely. We called the developed MERIT with specialized negative sampling approach subsystem-wise MERIT. Both developed models can be used as descriptive and predictive tasks based on the flight leg window used (one and three, respectively). The main advantage of the proposed latent aircraft system model (MERIT) is that it needs to be trained only once and can be easily queried using any similarity measurements between the embedding vectors, which means it is more feasible and computationally efficient than traditional machine learning algorithm, where it necessitates building a different model each time for every target FDE. We tested both models on a real Boeing dataset and the experimental results demonstrate the effectiveness of the proposed model in exhibiting the embedded relationships between fault messages and extracting the most relevant predictors.1.1Mohamed Elshrif et al. This is an open-access article distributed under the terms of the Creative Commons Attribution 3.0 United States License which permits unrestricted use, distribution, and reproduction in any medium, provided the original author and source are credited.
AB - Vector representation concept proves its success in solving many real-world problems from a variety of applications. In this paper, we built a novel vector representation model for avionics system for two types of fault messages called MERIT. This new model aims to identify the relationship between the flight deck effects (FDEs) and the maintenance messages (MMSGs) through calculating the embedding co-occurrence matrix between them within a predefined flight leg window. The a vector space embeddings representation of MERIT is able to differentiate between the strong and weak relationship between messages. Moreover, we benefit from the negative sampling method to incorporate the weak relationship between the FDEs and MMSGs from different subsystems (chapters) in assessing this relationship precisely. We called the developed MERIT with specialized negative sampling approach subsystem-wise MERIT. Both developed models can be used as descriptive and predictive tasks based on the flight leg window used (one and three, respectively). The main advantage of the proposed latent aircraft system model (MERIT) is that it needs to be trained only once and can be easily queried using any similarity measurements between the embedding vectors, which means it is more feasible and computationally efficient than traditional machine learning algorithm, where it necessitates building a different model each time for every target FDE. We tested both models on a real Boeing dataset and the experimental results demonstrate the effectiveness of the proposed model in exhibiting the embedded relationships between fault messages and extracting the most relevant predictors.1.1Mohamed Elshrif et al. This is an open-access article distributed under the terms of the Creative Commons Attribution 3.0 United States License which permits unrestricted use, distribution, and reproduction in any medium, provided the original author and source are credited.
UR - http://www.scopus.com/inward/record.url?scp=85062831251&partnerID=8YFLogxK
U2 - 10.1109/ICPHM.2018.8448927
DO - 10.1109/ICPHM.2018.8448927
M3 - Conference contribution
AN - SCOPUS:85062831251
T3 - 2018 IEEE International Conference on Prognostics and Health Management, ICPHM 2018
BT - 2018 IEEE International Conference on Prognostics and Health Management, ICPHM 2018
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2018 IEEE International Conference on Prognostics and Health Management, ICPHM 2018
Y2 - 11 June 2018 through 13 June 2018
ER -