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Aerodynamic parameter identification method based on physics-informed radial basis function-deep neural networks.

Jungu Chen1, Junhui Liu1, Jiayuan Shan1

  • 1Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China.

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|August 27, 2025
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Summary
This summary is machine-generated.

This study introduces a new method for estimating aerodynamic parameter changes using a physics-informed deep neural network. The approach accurately identifies aerodynamic perturbations, improving aircraft model predictions.

Keywords:
Aerodynamic parameters perturbationDeep learningParameter estimationPhysics-informed neural networks

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Area of Science:

  • Aerospace Engineering
  • Computational Fluid Dynamics
  • Machine Learning

Background:

  • Accurate estimation of aerodynamic parameters is crucial for flight dynamics and control.
  • Real-world aerodynamic parameters often deviate from nominal values due to various factors, necessitating robust identification methods.

Purpose of the Study:

  • To develop and validate a novel aerodynamic parameter identification method for precise estimation of perturbations.
  • To enhance the fitting capability and accuracy of aerodynamic parameter identification using advanced neural network architectures.

Main Methods:

  • Proposing a physics-informed radial basis function-deep neural network (PIRBF-DNN) for aerodynamic parameter identification.
  • Utilizing an integration-based loss function within the PIRBF-DNN to precisely estimate parameter perturbations.
  • Employing a radial basis function-deep neural network (RBF-DNN) structure to improve the network's fitting capabilities.

Main Results:

  • The PIRBF-DNN method demonstrated precise estimation of aerodynamic parameter perturbations in simulation.
  • Validation across different scenarios confirmed the effectiveness of the proposed identification technique.
  • Comparative analysis showed superior performance against existing physics-informed neural network (PINN) based methods.

Conclusions:

  • The PIRBF-DNN offers a powerful and accurate approach for identifying aerodynamic parameter perturbations.
  • This method enhances the reliability of aerodynamic models by accounting for real-world parameter variations.
  • The study highlights the potential of integrating physics-informed neural networks with RBF-DNNs for complex system identification.