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Machine learning based prediction of ditching loads
Citation Link: https://doi.org/10.15480/882.9240
Publikationstyp
Preprint
Publikationsdatum
2024-02-16
Sprache
English
We present approaches to predict dynamic ditching loads on aircraft fuselages using machine learning. The employed learning procedure is structured into two parts, the reconstruction of the spatial loads using a convolutional autoencoder (CAE) and the transient evolution of these loads in a subsequent part. Different CAE strategies are assessed and combined with either long short-term memory (LSTM) networks or Koopman-operator based methods to predict the transient behaviour. The training data is compiled by an extension of the momentum method of von-Karman and Wagner and the rationale of the training approach is briefly summarised. The application included refers to a full-scale fuselage of a DLR-D150 aircraft for a range of horizontal and vertical approach velocities at 6° incidence. Results indicate a satisfactory level of predictive agreement for all four investigated surrogate models examined, with the combination of an LSTM and a deep decoder CAE showing the best performance.
Schlagworte
Machine Learning
Aircraft Ditching
DDC Class
510: Mathematics
620: Engineering and Applied Operations
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2402.10724.pdf
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main article
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