An Interpretable Data-Driven Learning Approach for Nonlinear Aircraft Systems With Noisy Interference

This article discusses a learning algorithm for nonlinear aircraft systems, which targets the weaknesses of data-driven algorithms, mainly poor generalization ability and limited interpretability. It handles these constraints by integrating physical information with data-driven techniques. Referred to as the physics-informed SINDY (PI-SINDY) framework in this article, it improves the standard SINDY algorithm to tackle strongly time-varying nonlinear flight systems. This method incorporates the physical information described by the aircraft's differential kinematic equations into the SINDY algorithm and can also deal with the effects of measurement noise, making it more robust and practical. The proposed method displays higher robustness and generalization ability in comparison with the original SINDY algorithm and the WSINDy method, as confirmed by simulation results. Finally, we use the nonlinear system model learned with the suggested method for tracking control to supplement its efficiency.

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Institutions

Publication Details

Journal
IEEE Transactions on Aerospace and Electronic Systems
Published
2024-08-13
DOI
https://doi.org/10.1109/taes.2024.3442164
Citations
4
Primary Topic
Control Systems and Identification
Type
article
Field-Weighted Citation Impact
1.31
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article

An Interpretable Data-Driven Learning Approach for Nonlinear Aircraft Systems With Noisy Interference

Rui Cao, Kelin Lu, Yanbin Liu
4 citations
IEEE Transactions on Aerospace and Electronic Systems
Control Systems and Identification
1.31
article

An Interpretable Data-Driven Learning Approach for Nonlinear Aircraft Systems With Noisy Interference

Rui Cao, Kelin Lu, Yanbin Liu
article en
4 citations

Abstract

This article discusses a learning algorithm for nonlinear aircraft systems, which targets the weaknesses of data-driven algorithms, mainly poor generalization ability and limited interpretability. It handles these constraints by integrating physical information with data-driven techniques. Referred to as the physics-informed SINDY (PI-SINDY) framework in this article, it improves the standard SINDY algorithm to tackle strongly time-varying nonlinear flight systems. This method incorporates the physical information described by the aircraft's differential kinematic equations into the SINDY algorithm and can also deal with the effects of measurement noise, making it more robust and practical. The proposed method displays higher robustness and generalization ability in comparison with the original SINDY algorithm and the WSINDy method, as confirmed by simulation results. Finally, we use the nonlinear system model learned with the suggested method for tracking control to supplement its efficiency.

IEEE Transactions on Aerospace and Electronic SystemsVol. 61(1)
Southeast University (CN), Yangzhou University (CN), Nanjing University of Aeronautics and Astronautics (CN)
Openalex Percentile: Top 20%
Control Systems and Identification
1.31
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