Asynchronously fault detection for flight vehicles with unstable modes via MDLF and MDADT method

This research focuses on detecting faults in flight vehicles with unstable subsystems operating asynchronously. By accounting for asynchronous switching, a switched model is established, and filters for fault detection (FD) in unstable subsystems are developed. The FD challenge is then transformed into an H∞ filtering issue. Utilizing the multiple discontinuous Lyapunov function (MDLF) approach and the mode-dependent average dwell time (MDADT) method, sufficient conditions are derived to ensure stability during both fast and slow switching. Furthermore, the existence and solutions for FD filters are provided through linear matrix inequalities (LMIs). The simulation outcomes demonstrated the excellent performance of the developed method in studied cases.

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Publication Details

Journal
Defence Technology
Published
2025-03-23
DOI
https://doi.org/10.1016/j.dt.2025.03.016
Primary Topic
Fault Detection and Control Systems
Type
article
Field-Weighted Citation Impact
0.00

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article

Asynchronously fault detection for flight vehicles with unstable modes via MDLF and MDADT method

Sheng Luo, Xin Liu, Yuh-Jiuh Cheng
Defence Technology
Fault Detection and Control Systems
article

Asynchronously fault detection for flight vehicles with unstable modes via MDLF and MDADT method

Sheng Luo, Xin Liu, Yuh-Jiuh Cheng
article en

Abstract

This research focuses on detecting faults in flight vehicles with unstable subsystems operating asynchronously. By accounting for asynchronous switching, a switched model is established, and filters for fault detection (FD) in unstable subsystems are developed. The FD challenge is then transformed into an H∞ filtering issue. Utilizing the multiple discontinuous Lyapunov function (MDLF) approach and the mode-dependent average dwell time (MDADT) method, sufficient conditions are derived to ensure stability during both fast and slow switching. Furthermore, the existence and solutions for FD filters are provided through linear matrix inequalities (LMIs). The simulation outcomes demonstrated the excellent performance of the developed method in studied cases.

Defence TechnologyVol. 49
National Natural Science Foundation of China, Aeronautical Science Foundation of China
Climate action
Openalex Percentile: Top 94%
Fault Detection and Control Systems
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