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- W2611384027 abstract "This paper presents a parametric model-based monitoring technique for detection and confirmation of faults in control surface servo-loops related to the Electrical Flight Control System. It is shown that there exists a direction in the parameter space which is sensitive to the occurrence of the faults on interest. On-line system parameter estimation is combined with an appropriate parametric test decision for robust detection and confirmation of faults. The paper reports on a number of identified practical design considerations identified that should accompany the basic design in order to provide a viable technological solution. The method presented in this paper has reached level 5 on Technological Readiness Level scale under flight Validation & Verification investigations at Airbus. The methodology is considered to be a credible unconventional option to support (not rule out) conventional industrial practices." @default.
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- W2611384027 date "2017-07-10" @default.
- W2611384027 modified "2023-10-12" @default.
- W2611384027 title "Turning theory to practice in model-based FDI: Successful application to new generation Airbus aircraft" @default.
- W2611384027 hasPublicationYear "2017" @default.
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