Online Trajectory Optimization of an ASV Based on an Improved RBFNN

Optimization based on conventional neural networks can only guarantee calculation speed. However, the accuracy of network prediction is also a key index in online trajectory optimization. This paper proposes a novel online trajectory optimization approach based on an Improved Radial Basis Function Neural Network (IRBFNN). First, multiple optimal trajectories for different variations of Air-Breathing Supersonic Vehicles (ASVs) are generated, considering attitude, and collected as the dataset. Then, an IRBFNN is trained to predict trajectories online with the above dataset, in which an enhanced loss function is introduced to improve prediction accuracy. Finally, numerical simulations are presented to demonstrate the feasibility and superiority of the proposed online trajectory optimization method. The open-source code of the proposed method is shared in the form of a link to showcase its implementation.

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Publication Details

Journal
Symmetry
Published
2024-12-18
DOI
https://doi.org/10.3390/sym16121679
Citations
1
Primary Topic
Aerospace and Aviation Technology
Type
article
Field-Weighted Citation Impact
1.30

Funders

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article

Online Trajectory Optimization of an ASV Based on an Improved RBFNN

Chao Ming, Suyu Yan
1 citations
Symmetry
Aerospace and Aviation Technology
1.30
article

Online Trajectory Optimization of an ASV Based on an Improved RBFNN

Chao Ming, Suyu Yan
article en
1 citations

Abstract

Optimization based on conventional neural networks can only guarantee calculation speed. However, the accuracy of network prediction is also a key index in online trajectory optimization. This paper proposes a novel online trajectory optimization approach based on an Improved Radial Basis Function Neural Network (IRBFNN). First, multiple optimal trajectories for different variations of Air-Breathing Supersonic Vehicles (ASVs) are generated, considering attitude, and collected as the dataset. Then, an IRBFNN is trained to predict trajectories online with the above dataset, in which an enhanced loss function is introduced to improve prediction accuracy. Finally, numerical simulations are presented to demonstrate the feasibility and superiority of the proposed online trajectory optimization method. The open-source code of the proposed method is shared in the form of a link to showcase its implementation.

SymmetryVol. 16(12)
Nanjing University of Science and Technology (CN)
National Natural Science Foundation of China
Openalex Percentile: Top 11%
Aerospace and Aviation Technology
1.30
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