控制理论(社会学)
趋同(经济学)
强化学习
航天器
计算机科学
理论(学习稳定性)
控制器(灌溉)
观察员(物理)
滤波器(信号处理)
能源消耗
自适应控制
能量(信号处理)
控制工程
最优控制
国家观察员
约束(计算机辅助设计)
弹道
控制系统
最优化问题
控制(管理)
能量最小化
跟踪(教育)
约束优化
姿态控制
自适应系统
工程类
数学优化
作者
Shuangsi Xue,Z.Q. Ding,Junkai Tan,Kai Qu,H. Cao,Dongyu Li
标识
DOI:10.1109/taes.2025.3650566
摘要
This paper presents a fixed-time synchronized reinforcement learning-based control (pFxT-SRLC) framework for spacecraft attitude systems that simultaneously addresses four critical challenges: predetermined convergence time guarantees, synchronized multi-axis coordination, energy optimization, and practical constraint handling. Our integrated framework combines a fixed-time super-twisting observer with adaptive switching strategy, a practical fixed-time synchronized controller with singularity avoidance, and an actor-critic reinforcement learning structure for near-optimal energy performance. The proposed method ensures all state variables converge to desired neighborhoods simultaneously within predetermined time bounds independent of initial conditions, while the constrained learning algorithm maintains stability throughout the optimization process. A second-order command filter handles input saturation constraints and reduces control chattering for practical implementation. Theoretical analysis proves fixed-time synchronized stability with explicit convergence time bounds, and establishes energy optimality through Hamilton-Jacobi-Bellman approximation. Simulation results demonstrate that the proposed pFxT-SRLC achieves comparable tracking accuracy to conventional fixed-time methods while reducing energy consumption and generating significantly smoother control signals.
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