arXiv · 2212.06688
PCA Methods and Evidence Based Filtering for Robust Aircraft Sensor Fault Diagnosis
Abstract
In this paper PCA and D-PCA techniques are applied for the design of a Data Driven diagnostic Fault Isolation (FI) and Fault Estimation (FE) scheme for 18 primary sensors of a semi-autonomous aircraft. Specifically, Contributions-based, and Reconstruction-based Contributions approaches have been considered. To improve FI performance an inference mechanism derived from evidence-based decision making theory has been proposed. A detailed FI and FE study is presented for the True Airspeed sensor based on experimental data. Evidence Based Filtering (EBF) showed to be very effective particularly in reducing false alarms.
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N. Cartocci, G. Costante, M. R. Napolitano, P. Valigi, F. Crocetti, M. L. Fravolini. 2022-12-13. PCA Methods and Evidence Based Filtering for Robust Aircraft Sensor Fault Diagnosis. https://doi.org/10.1109/med48518.2020.9182973
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