Similarity-based information fusion grey model for remaining useful life prediction of aircraft engines. Issue 3 (16th October 2020)

• Record Type: Journal Article
• Authors: Yang, Xiaoyu; Fang, Zhigeng; Li, Xiaochuan; Yang, Yingjie; Mba, David
• Is Part Of: Grey systems. Volume 11:Issue 3(2021)
• Page Start: 463
• Page End: 483
• Publication Date: 2020-10-16
• Subjects: GM(1, 1) -- Remaining useful life -- Similarity-based -- Information fusion -- Aircraft engine; Cybernetics -- Periodicals; Systems engineering -- Periodicals; 003.5
• DOI: 10.1108/GS-05-2020-0066
• Languages: English
• ISSNs: 2043-9377

Abstract

Abstract : Purpose: Online health monitoring of large complex equipment has become a trend in the field of equipment diagnostics and prognostics due to the rapid development of sensing and computing technologies. The purpose of this paper is to construct a more accurate and stable grey model based on similar information fusion to predict the real-time remaining useful life (RUL) of aircraft engines. Design/methodology/approach: First, a referential database is created by applying multiple linear regressions on historical samples. Then similarity matching is conducted between the monitored engine and historical samples. After that, an information fusion grey model is applied to predict the future degradation trajectory of the monitored engine considering the latest trend of monitored sensory data and long-term trends of several similar referential samples, and the real-time RUL is obtained correspondingly. Findings: The results of comparative analysis reveal that the proposed model, which is called similarity-based information fusion grey model (SIFGM), could provide better RUL prediction from the early degradation stage. Furthermore, SIFGM is still able to predict system failures relatively accurately when only partial information of the referential samples is available, making the method a viable choice when the historical whole life cycle data are scarce. Research limitations/implications: The prediction of SIFGM method is based on a single monotonically changing health indicator (HI) synthesized from monitoring sensory signals, which is assumed to be highly relevant to the degradation processes of the engine. Practical implications: The SIFGM can be used to predict the degradation trajectories and RULs of those online condition monitoring systems with similar irreversible degradation behaviors before failure occurs, such as aircraft engines and centrifugal pumps. Originality/value: This paper introduces the similarity information into traditional GM(1, 1) model to make it more suitable for long-term RUL prediction and also provide a solution of similarity-based RUL prediction with limited historical whole life cycle data.