Physics-Informed Neural Networks for Unmanned Aerial Vehicle System Estimation

被引:2
|
作者
Bianchi, Domenico [1 ,2 ]
Epicoco, Nicola [2 ,3 ]
Di Ferdinando, Mario [1 ,2 ]
Di Gennaro, Stefano [1 ,2 ]
Pepe, Pierdomenico [1 ,2 ]
机构
[1] Univ Aquila, Dipartimento Ingn & Sci Informaz & Matemat, Via Vetoio, I-67100 Laquila, Italy
[2] Univ Aquila, Ctr Ric Eccellenza DEWS, Via Vetotio, I-67100 Laquila, Italy
[3] LUM Libera Univ Mediterranea Giuseppe Degennaro, Dept Engn, Str Statale 100 Km 18, I-70010 Casamassima Bari, Italy
关键词
quadrotor control; system identification; Physics-Informed Neural Networks; IDENTIFICATION;
D O I
10.3390/drones8120716
中图分类号
TP7 [遥感技术];
学科分类号
081102 ; 0816 ; 081602 ; 083002 ; 1404 ;
摘要
The dynamic nature of quadrotor flight introduces significant uncertainty in system parameters, such as thrust and drag factors. Consequently, operators grapple with escalating challenges in implementing real-time control actions. This study presents an approach for estimating the dynamic model of Unmanned Aerial Vehicles based on Physics-Informed Neural Networks (PINNs), which is of paramount importance due to the presence of uncertain data and since control actions are required in very short computation times. In this regard, by including physical laws into neural networks, PINNs offer the potential to tackle several issues, such as heightened non-linearities in low-inertia systems, elevated measurement noise, and constraints on data availability or uncertainties, while ensuring the robustness of the solution, thus ensuring effective results in short time, once the network training has been performed and without the need to be retrained. The effectiveness of the proposed method is showcased in a simulation environment with real data and juxtaposed with a state-of-the-art technique, such as the Extended Kalman Filter (EKF). The results show that the proposed estimator outperforms the EKF both in terms of the efficacy of the solution and computation time.
引用
收藏
页数:17
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