TY - JOUR
T1 - A point cloud reconstruction method based on uncertainty feature enhancement for aerodynamic shape optimization
AU - LI, Junlin
AU - ZHANG, Yang
AU - PANG, Bo
AU - BAI, Junqiang
AU - XU, Jiakuan
N1 - Publisher Copyright:
© 2025 The Author(s)
PY - 2026/6
Y1 - 2026/6
N2 - The precision of shape representation and the dimensionality of the design space significantly influence the cost and outcomes of aerodynamic optimization. The design space can be represented more compactly by maintaining geometric precision while reducing dimensions, hence enhancing the cost-effectiveness of the optimization process. This research presents a new point cloud Autoencoder Based on Uncertainty Feature Enhancement (AE-BUFE) architecture, designed to attain efficient and precise generalized representations of 3D aircraft through uncertainty analysis of the deformation relationships among surface grid points. The deep learning architecture consists of two components: the uncertainty index-based feature enhancement module and the point cloud autoencoder module. It learns the shape features of the point cloud geometric representation to establish a low-dimensional latent space. To assess and evaluate the efficiency of the method, a comparison was conducted with the prevailing point cloud autoencoder architecture and the proper orthogonal decomposition linear dimensionality reduction method under conditions of complex shape deformation. The results show that the new architecture significantly improves the extraction effect of the low-dimensional latent space. Then, this paper developed the surrogate-based optimization framework based on the AE-BUFE parameterization method and completed a multi-objective aerodynamic optimization design for a wide-speed-range vehicle considering volume and moment constraints. While ensuring the take-off and landing performance, the aerodynamic performance is improved under transonic and hypersonic conditions, which verifies the efficiency and engineering practicability of this method.
AB - The precision of shape representation and the dimensionality of the design space significantly influence the cost and outcomes of aerodynamic optimization. The design space can be represented more compactly by maintaining geometric precision while reducing dimensions, hence enhancing the cost-effectiveness of the optimization process. This research presents a new point cloud Autoencoder Based on Uncertainty Feature Enhancement (AE-BUFE) architecture, designed to attain efficient and precise generalized representations of 3D aircraft through uncertainty analysis of the deformation relationships among surface grid points. The deep learning architecture consists of two components: the uncertainty index-based feature enhancement module and the point cloud autoencoder module. It learns the shape features of the point cloud geometric representation to establish a low-dimensional latent space. To assess and evaluate the efficiency of the method, a comparison was conducted with the prevailing point cloud autoencoder architecture and the proper orthogonal decomposition linear dimensionality reduction method under conditions of complex shape deformation. The results show that the new architecture significantly improves the extraction effect of the low-dimensional latent space. Then, this paper developed the surrogate-based optimization framework based on the AE-BUFE parameterization method and completed a multi-objective aerodynamic optimization design for a wide-speed-range vehicle considering volume and moment constraints. While ensuring the take-off and landing performance, the aerodynamic performance is improved under transonic and hypersonic conditions, which verifies the efficiency and engineering practicability of this method.
KW - Deep learning
KW - Design space dimensionality reduction
KW - Flight vehicle design
KW - Point cloud autoencoder
KW - Sensitivity analysis
KW - Wide speed range
UR - https://www.scopus.com/pages/publications/105037679858
U2 - 10.1016/j.cja.2025.103847
DO - 10.1016/j.cja.2025.103847
M3 - 文章
AN - SCOPUS:105037679858
SN - 1000-9361
VL - 39
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 6
M1 - 103847
ER -