A hybrid framework for real-time satellite fault diagnosis using Markov jump-adjusted models and 1D sliding window Residual Networks

IF 3.1 2区 物理与天体物理 Q1 ENGINEERING, AEROSPACE Acta Astronautica Pub Date : 2025-01-02 DOI:10.1016/j.actaastro.2024.12.057
MohammadSaleh Hedayati, Afshin Rahimi
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Abstract

Data-driven methods, including Artificial Intelligence (AI) and Machine Learning (ML) techniques, have been becoming more prominent in the field of satellite Fault Diagnosis and Prognosis (FDP) owing to their exceptional pattern recognition capabilities. On the other hand, they have some glaring accompanying issues other than their data dependency that have not been explored in the literature on satellite fault diagnosis. These issues include their inability to accommodate real-time fault diagnosis requirements, failure to account for the fault diagnosis and fault-tolerant modules’ interactions, and being prone to getting overfit due to manually injected faults. Therefore, this work proposes a hybrid framework for real-time fault diagnosis of a single Reaction Wheel (RW) onboard a satellite that capitalizes on both data-driven and model-based methods’ strong suits. The proposed methodology can also be applied to other satellite sub-systems. The presented hybrid framework comprises a Morkov jump-adjusted RW model, a Markov Jump-Adjusted Particle Filter (MJAPF), and a One Dimensional (1D) sliding window Residual Network (ResNet). The Morkov jump-adjusted RW model addresses the under-represented issues of data-driven methods, the MJAPF provides a means of estimating the non-linear RW’s hidden states under non-Gaussian noise conditions while accounting for malfunction dynamics, and the 1D sliding window ResNet model ensures online diagnosis performance. Experiments showed that the hybrid framework can achieve accurate and timely results, even reaching accuracy rates as high as 99% in low-noise conditions. The proposed MJAPF algorithm proved to be a capable estimation technique. However, the proposed MJAPF and ResNet frameworks were incompatible due to the gap in their perceptions of fault dynamics but proved effective on their own merits. Future remarks for making the proposed hybrid framework more robust to noise are also discussed.
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来源期刊
Acta Astronautica
Acta Astronautica 工程技术-工程:宇航
CiteScore
7.20
自引率
22.90%
发文量
599
审稿时长
53 days
期刊介绍: Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to: The peaceful scientific exploration of space, Its exploitation for human welfare and progress, Conception, design, development and operation of space-borne and Earth-based systems, In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.
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