TY - JOUR
T1 - SPARSE RECONSTRUCTION OF SURFACE LOADS ON AIRCRAFT USING POD AND RBFNN
AU - Jia, Xuyi
AU - Gong, Chunlin
AU - Li, Chunna
N1 - Publisher Copyright:
© 2024, International Council of the Aeronautical Sciences. All rights reserved.
PY - 2024
Y1 - 2024
N2 - loads based on the measurements from sensors in wind tunnel test or during flight are crucial for aerodynamic design, health monitoring and flight control. However, obtaining the complete surface loads in real-time is challenging due to the limitations of available measurements. To handle this problem, we propose a sparse reconstruction modeling method based on proper orthogonal decomposition (POD) and radial basis function neural network (RBFNN). This method leverages the dimensionality reduction capabilities of POD to extract the dominant modes of surface loads, and then use RBFNN to accurately predict the mode coefficients based on sparse measurements. Furthermore, to improve the accuracy of sparse reconstruction, we have developed an objective function that integrates the surface loads in optimizing the sensor locations. The case study of the DLR-F6 aircraft shows that a weight of 0.25 for the objective function provides the best reconstruction performance. Additionally, a minimum of 240 modeling samples is required to ensure the accuracy of the sparse reconstruction model. Specifically, with just 37 sensors, we can achieve real-time sparse reconstruction of surface pressure coefficients.
AB - loads based on the measurements from sensors in wind tunnel test or during flight are crucial for aerodynamic design, health monitoring and flight control. However, obtaining the complete surface loads in real-time is challenging due to the limitations of available measurements. To handle this problem, we propose a sparse reconstruction modeling method based on proper orthogonal decomposition (POD) and radial basis function neural network (RBFNN). This method leverages the dimensionality reduction capabilities of POD to extract the dominant modes of surface loads, and then use RBFNN to accurately predict the mode coefficients based on sparse measurements. Furthermore, to improve the accuracy of sparse reconstruction, we have developed an objective function that integrates the surface loads in optimizing the sensor locations. The case study of the DLR-F6 aircraft shows that a weight of 0.25 for the objective function provides the best reconstruction performance. Additionally, a minimum of 240 modeling samples is required to ensure the accuracy of the sparse reconstruction model. Specifically, with just 37 sensors, we can achieve real-time sparse reconstruction of surface pressure coefficients.
KW - Aircraft
KW - Proper orthogonal decomposition
KW - Sensor locations optimization
KW - Sparse reconstruction
KW - Surface loads
UR - http://www.scopus.com/inward/record.url?scp=85208811995&partnerID=8YFLogxK
M3 - 会议文章
AN - SCOPUS:85208811995
SN - 1025-9090
JO - ICAS Proceedings
JF - ICAS Proceedings
T2 - 34th Congress of the International Council of the Aeronautical Sciences, ICAS 2024
Y2 - 9 September 2024 through 13 September 2024
ER -