Online Optimal Attitude Stabilization via Reinforcement Learning for Rigid Spacecraft With Dynamic Uncertainty

In this paper, we discuss an online reinforcement learning (RL) algorithm to solve the optimal control problem for rigid spacecraft attitude control systems with dynamic uncertainty. The RL algorithm adapts in real time, finding the optimal control policy estimation while guaranteeing the stability of the closed-loop system and the algorithm convergence. To address dynamic uncertainty, we introduce a two-phase learning structure implementing recursive computations based on the measurable system state, rather than relying on prior knowledge of the system's dynamic model. A sufficient condition for the algorithm convergence is presented, ensuring that the control policy converges to the optimal controller within finite iterations of the learning process. Comparative simulations are conducted to illustrate the validity and advantages of the proposed algorithm.

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Publication Details

Journal
IEEE Transactions on Aerospace and Electronic Systems
Published
2025-04-25
DOI
https://doi.org/10.1109/taes.2025.3564579
Citations
2
Primary Topic
Adaptive Control of Nonlinear Systems
Type
article
Field-Weighted Citation Impact
2.43
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article

Online Optimal Attitude Stabilization via Reinforcement Learning for Rigid Spacecraft With Dynamic Uncertainty

Rugang Tang, Chengfeng Luo, Xin Ning
2 citations
IEEE Transactions on Aerospace and Electronic Systems
Adaptive Control of Nonlinear Systems
2.43
article

Online Optimal Attitude Stabilization via Reinforcement Learning for Rigid Spacecraft With Dynamic Uncertainty

Rugang Tang, Chengfeng Luo, Xin Ning
article en
2 citations

Abstract

In this paper, we discuss an online reinforcement learning (RL) algorithm to solve the optimal control problem for rigid spacecraft attitude control systems with dynamic uncertainty. The RL algorithm adapts in real time, finding the optimal control policy estimation while guaranteeing the stability of the closed-loop system and the algorithm convergence. To address dynamic uncertainty, we introduce a two-phase learning structure implementing recursive computations based on the measurable system state, rather than relying on prior knowledge of the system's dynamic model. A sufficient condition for the algorithm convergence is presented, ensuring that the control policy converges to the optimal controller within finite iterations of the learning process. Comparative simulations are conducted to illustrate the validity and advantages of the proposed algorithm.

IEEE Transactions on Aerospace and Electronic SystemsVol. 61(4)
Northwestern Polytechnical University (CN)
Affordable and clean energy
Openalex Percentile: Top 12%
Adaptive Control of Nonlinear Systems
2.43
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Online Optimal Attitude Stabilization via Reinforcement Learning for Rigid Spacecraft With Dynamic Uncertainty — Rugang Tang, Chengfeng Luo, et al. · IEEE Transactions on Aerospace and Electronic Systems (2025) | TGRS Research Map | TGRS