A Flight Test Anomaly Detection Framework Based on Adaptive Weight Fusion

2026-99-0606

To be published on 11/06/2026

Authors
Abstract
Content
Flight anomaly detection plays a critical role in ensuring aviation safety. However, conventional anomaly detection methods often suffer from limited accuracy due to their reliance on single-sensor observations or fixed-weight multi-sensor fusion strategies. To address these limitations, this paper proposes an adaptive weight fusion framework for flight-test anomaly detection. The proposed framework integrates a signal-to-noise-ratio-based adaptive weighting strategy, an improved Kalman filtering algorithm, and an ensemble anomaly detection model within a hierarchical fusion architecture to achieve robust multi-sensor data fusion and anomaly identification.
Experiments were conducted using the NASA DASHlink Tail_666_9 flight dataset. Compared with conventional methods, the proposed framework achieved improvements in overall accuracy, precision, recall, and F1-score. Specifically, the proposed method achieved an F1-score of 0.486 while reducing the average anomaly detection delay by more than 2 s. These results indicate that the proposed framework can improve the effectiveness and timeliness of flight anomaly detection, demonstrating its potential for real-time flight safety monitoring.
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Citation
Wang, Y., "A Flight Test Anomaly Detection Framework Based on Adaptive Weight Fusion," 2026 International Conference on Artificial Intelligence, Autonomous Systems, and Aerospace, Wuhan, China, January 16, 2026, .
Additional Details
Publisher
Published
To be published on Nov 6, 2026
Product Code
2026-99-0606
Content Type
Technical Paper
Language
English