非線形モデルに基づくロバストフィルタを用いたジェットエンジンのヘルスモニタリング

We develop a novel jet engine health monitoring method using a high-fidelity, physics-based simulation model. In jet engine health monitoring, fault detection with a state estimation is frequently carried out. However, a challenge for a filtering-based health monitoring method with a high-fidelity m...

Full description

Saved in:
Bibliographic Details
Published inShisutemu Seigyo Jouhou Gakkai rombunshi Vol. 29; no. 8; pp. 337 - 345
Main Authors 垣内, 大紀, 中村, 恵子, 木村, 麻衣, 足立, 修一, 小野, 雅裕, 若林, 優一, 木下, 萌, 佐藤, 諒
Format Journal Article
LanguageJapanese
Published Kyoto 一般社団法人 システム制御情報学会 2016
Japan Science and Technology Agency
Subjects
Online AccessGet full text
ISSN1342-5668
2185-811X
DOI10.5687/iscie.29.337

Cover

More Information
Summary:We develop a novel jet engine health monitoring method using a high-fidelity, physics-based simulation model. In jet engine health monitoring, fault detection with a state estimation is frequently carried out. However, a challenge for a filtering-based health monitoring method with a high-fidelity model is the difficulty to analytically obtain the Jacobians, which is required for the extended Kalman filter. Our approach is to derive a linearized model a priori at a fixed operation point, and use a robust filter method to guarantee a reliable health monitoring over a wide range of operation points despite the linearization errors. We validate the proposed method by extensive simulations.
Bibliography:ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 14
ISSN:1342-5668
2185-811X
DOI:10.5687/iscie.29.337