Learning robust satellite attitude dynamics with physics-informed normalising flow

Attitude control is a fundamental aspect of spacecraft operations. Model Predictive Control (MPC) has emerged as a powerful strategy for these tasks, relying on accurate models of the system dynamics to optimize control actions over a prediction horizon. In scenarios where physics models are incomplete, difficult to derive, or computationally expensive, machine learning offers a flexible alternative by learning the system behavior directly from data. However, purely data-driven models often struggle with generalization and stability, especially when applied to inputs outside their training domain. To address these limitations, we investigate the benefits of incorporating Physics-Informed Neural Networks (PINNs) into the learning of spacecraft attitude dynamics, comparing their performance with that of purely data-driven approaches. Using a Real-valued Non-Volume Preserving (Real NVP) neural network architecture with a self-attention mechanism, we trained several models on simulated data generated with the Basilisk simulator. Two training strategies were considered: a purely data-driven baseline and a physics-informed variant to improve robustness and stability. Our results demonstrate that the inclusion of physics-based information significantly enhances the performance in terms of the mean relative error with the best architectures found by 27.08%. These advantages are particularly evident when the learned models are integrated into an MPC framework, where PINN-based models consistently outperform their purely data-driven counterparts in terms of control accuracy and robustness, and achieve improved settling times when compared to traditional MPC approaches, yielding improvements of up to 62%, when subject to observation noise and RWs friction. • Spacecraft attitude dynamics with normalising flow models and self-attention. • Compared physics-informed and data-driven neural networks. • Compared neural networks approaches with traditional controllers. • Improved closed-loop control robustness under noisy state observations. • Enhanced MPC performance under parameter and observation uncertainties.

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Publication Details

Journal
Acta Astronautica
Published
2026-03-01
DOI
https://doi.org/10.1016/j.actaastro.2026.03.047
Primary Topic
Spacecraft Dynamics and Control
Type
article
Field-Weighted Citation Impact
0.00
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article

Learning robust satellite attitude dynamics with physics-informed normalising flow

Marcello Chiaberge, Carlo Cena, Mauro Martini
Acta Astronautica
Spacecraft Dynamics and Control
article

Learning robust satellite attitude dynamics with physics-informed normalising flow

Marcello Chiaberge, Carlo Cena, Mauro Martini
article en

Abstract

Attitude control is a fundamental aspect of spacecraft operations. Model Predictive Control (MPC) has emerged as a powerful strategy for these tasks, relying on accurate models of the system dynamics to optimize control actions over a prediction horizon. In scenarios where physics models are incomplete, difficult to derive, or computationally expensive, machine learning offers a flexible alternative by learning the system behavior directly from data. However, purely data-driven models often struggle with generalization and stability, especially when applied to inputs outside their training domain. To address these limitations, we investigate the benefits of incorporating Physics-Informed Neural Networks (PINNs) into the learning of spacecraft attitude dynamics, comparing their performance with that of purely data-driven approaches. Using a Real-valued Non-Volume Preserving (Real NVP) neural network architecture with a self-attention mechanism, we trained several models on simulated data generated with the Basilisk simulator. Two training strategies were considered: a purely data-driven baseline and a physics-informed variant to improve robustness and stability. Our results demonstrate that the inclusion of physics-based information significantly enhances the performance in terms of the mean relative error with the best architectures found by 27.08%. These advantages are particularly evident when the learned models are integrated into an MPC framework, where PINN-based models consistently outperform their purely data-driven counterparts in terms of control accuracy and robustness, and achieve improved settling times when compared to traditional MPC approaches, yielding improvements of up to 62%, when subject to observation noise and RWs friction. • Spacecraft attitude dynamics with normalising flow models and self-attention. • Compared physics-informed and data-driven neural networks. • Compared neural networks approaches with traditional controllers. • Improved closed-loop control robustness under noisy state observations. • Enhanced MPC performance under parameter and observation uncertainties.

Acta Astronautica
Politecnico di Torino (IT)
Climate action
Openalex Percentile: Top 3%
Spacecraft Dynamics and Control
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