Remaining Useful Life Estimation of Aircraft Engines Using Differentiable Architecture Search

Prognostics and health management (PHM) applications can prevent engines from potential serious accidents by predicting the remaining useful life (RUL). Recently, data-driven methods have been widely used to solve RUL problems. The network architecture has a crucial impact on the experiential perfor...

Full description

Bibliographic Details
Main Authors: Pengli Mao, Yan Lin, Song Xue, Baochang Zhang
Format: Article
Language:English
Published: MDPI AG 2022-01-01
Series:Mathematics
Subjects:
Online Access:https://www.mdpi.com/2227-7390/10/3/352
_version_ 1797486353324179456
author Pengli Mao
Yan Lin
Song Xue
Baochang Zhang
author_facet Pengli Mao
Yan Lin
Song Xue
Baochang Zhang
author_sort Pengli Mao
collection DOAJ
description Prognostics and health management (PHM) applications can prevent engines from potential serious accidents by predicting the remaining useful life (RUL). Recently, data-driven methods have been widely used to solve RUL problems. The network architecture has a crucial impact on the experiential performance. However, most of the network architectures are designed manually based on human experience with a large cost of time. To address these challenges, we propose a neural architecture search (NAS) method based on gradient descent. In this study, we construct the search space with a directed acyclic graph (DAG), where a subgraph represents a network architecture. By using softmax relaxation, the search space becomes continuous and differentiable, then the gradient descent can be used for optimization. Moreover, a partial channel connection method is introduced to accelerate the searching efficiency. The experiment is conducted on C-MAPSS dataset. In the data processing step, a fault detection method is proposed based on the k-means algorithm, which drops large valueless data and promotes the estimation performance. The experimental result shows that our method achieves superior performance with the highest estimation accuracy compared with other popular studies.
first_indexed 2024-03-09T23:32:57Z
format Article
id doaj.art-3ed53c4f61894ab7969d86b809624ab0
institution Directory Open Access Journal
issn 2227-7390
language English
last_indexed 2024-03-09T23:32:57Z
publishDate 2022-01-01
publisher MDPI AG
record_format Article
series Mathematics
spelling doaj.art-3ed53c4f61894ab7969d86b809624ab02023-11-23T17:06:08ZengMDPI AGMathematics2227-73902022-01-0110335210.3390/math10030352Remaining Useful Life Estimation of Aircraft Engines Using Differentiable Architecture SearchPengli Mao0Yan Lin1Song Xue2Baochang Zhang3School of Energy and Power Engineering, Beihang University, Beijing 100191, ChinaCollege of Electrical Engineering and Automation, Shandong University of Science and Technology, Qingdao 266590, ChinaSchool of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, ChinaInstitute of Artificial Intelligence, Beihang University, Beijing 100191, ChinaPrognostics and health management (PHM) applications can prevent engines from potential serious accidents by predicting the remaining useful life (RUL). Recently, data-driven methods have been widely used to solve RUL problems. The network architecture has a crucial impact on the experiential performance. However, most of the network architectures are designed manually based on human experience with a large cost of time. To address these challenges, we propose a neural architecture search (NAS) method based on gradient descent. In this study, we construct the search space with a directed acyclic graph (DAG), where a subgraph represents a network architecture. By using softmax relaxation, the search space becomes continuous and differentiable, then the gradient descent can be used for optimization. Moreover, a partial channel connection method is introduced to accelerate the searching efficiency. The experiment is conducted on C-MAPSS dataset. In the data processing step, a fault detection method is proposed based on the k-means algorithm, which drops large valueless data and promotes the estimation performance. The experimental result shows that our method achieves superior performance with the highest estimation accuracy compared with other popular studies.https://www.mdpi.com/2227-7390/10/3/352prognostics and health managementremaining useful life estimationdifferentiable architecture searchneural architecture searchaircraft engines
spellingShingle Pengli Mao
Yan Lin
Song Xue
Baochang Zhang
Remaining Useful Life Estimation of Aircraft Engines Using Differentiable Architecture Search
Mathematics
prognostics and health management
remaining useful life estimation
differentiable architecture search
neural architecture search
aircraft engines
title Remaining Useful Life Estimation of Aircraft Engines Using Differentiable Architecture Search
title_full Remaining Useful Life Estimation of Aircraft Engines Using Differentiable Architecture Search
title_fullStr Remaining Useful Life Estimation of Aircraft Engines Using Differentiable Architecture Search
title_full_unstemmed Remaining Useful Life Estimation of Aircraft Engines Using Differentiable Architecture Search
title_short Remaining Useful Life Estimation of Aircraft Engines Using Differentiable Architecture Search
title_sort remaining useful life estimation of aircraft engines using differentiable architecture search
topic prognostics and health management
remaining useful life estimation
differentiable architecture search
neural architecture search
aircraft engines
url https://www.mdpi.com/2227-7390/10/3/352
work_keys_str_mv AT penglimao remainingusefullifeestimationofaircraftenginesusingdifferentiablearchitecturesearch
AT yanlin remainingusefullifeestimationofaircraftenginesusingdifferentiablearchitecturesearch
AT songxue remainingusefullifeestimationofaircraftenginesusingdifferentiablearchitecturesearch
AT baochangzhang remainingusefullifeestimationofaircraftenginesusingdifferentiablearchitecturesearch