4/14/2023 0 Comments Structural loads on aircraftThe effectiveness of the proposed method is validated by an experimental study performed on a composite unmanned aerial vehicle (UAV) wing subject to concentrated and distributed loads, and the results obtained by the proposed method are superior when compared with a method based on Castigliano’s theorem. The neural networks trained for classification and regression are preceded with an autoencoder, through which maximum informative data at a much smaller scale are extracted from the depth features. The localization of the load is treated as a multinomial logistic classification problem and the load magnitude estimation as a logistic regression problem. To this end, a framework that is based on artificial neural networks is developed where features that are extracted from a depth camera are utilized. This paper deals with the development of a realtime structural health monitoring system for airframe structures to localize and estimate the magnitude of the loads causing deflections to the critical components, such as wings.
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