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.
Authors
- Rugang Tang (ORCID: https://orcid.org/0000-0003-1572-1794)
- Chengfeng Luo (ORCID: https://orcid.org/0000-0002-9426-1716)
- Xin Ning (ORCID: https://orcid.org/0009-0006-3488-4336)
Institutions
- Northwestern Polytechnical University (CN)
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