Cited by 6Structural Health Monitoring TechniquesFatigue and fracture mechanicsAerospace Engineering and Applications

Machine Learning Application on Aircraft Fatigue Stress Predictions

O’Higgins, Eugene, Graham, Kyle, Daverschot, Derk, Baris, Julien·2020·Lecture Notes in Mechanical Engineering

Integrity signals

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Crossref · 10.1007/978-3-030-21503-3_81

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Authors
O’Higgins, E., Graham, K., Daverschot, D., & Baris, J.
Affiliations
  • Airbus (Germany) (DE)
  • Airbus (United Kingdom) (GB)
  • Airbus (France) (FR)
Corresponding author
Daverschot, Derk
Venue
Lecture Notes in Mechanical Engineering
Published
2019-07-03
Pages
1031-1042
ISSN
  • 2195-4356 (ISSN-L)
  • 2195-4364
OpenAlex
W2953427604
Cited by
6
References
0
Citations by year
2025: 1 · 2024: 1 · 2023: 1 · 2022: 1 · 2021: 1 · 2020: 1
FWCI
2.40
Type
conference paper
Language
en
Open access
closed
Locations
Lecture notes in mechanical engineering (publishedVersion)
Topics
  • Physical Sciences › Engineering › Civil and Structural Engineering › Structural Health Monitoring Techniques
  • Physical Sciences › Engineering › Mechanics of Materials › Fatigue and fracture mechanics
  • Physical Sciences › Engineering › Control and Systems Engineering › Aerospace Engineering and Applications
Keywords
aircraft fatigue, machine learning, flight data, aircraft maintenance, civil aviation

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Registry, retraction, Cites and statistics results are computed, not judged, with one exception: a printed reference that no index lists is read once by a model before it counts as a citation error. Claims are extracted by a model and kept only when their quote appears verbatim in the text; each cited source is then checked, with a model’s help, for whether it says what the claim relies on. Those verdicts can be wrong — read the claim’s quote and the cited source before relying on one.

Statistics and arithmetic are recomputed, not judged.

Confidence bands are shown only for fields calibrated on our annotated test set. None is calibrated yet, so no band is shown.

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