Predefined-Time Actor-Critic Learning for Constrained Spacecraft Attitude Consensus

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초록

This article focuses on the problem of predefined-time suboptimal attitude consensus control for multiple spacecraft with time-varying state constraints. Under the backstepping framework, a predefined-time optimized controller is developed through the actor-critic architecture, where the actor executes control actions and the critic evaluates their effectiveness. The proposed approach derives the updating laws from the negative gradient of a positive function generated by the partial derivative of the Hamilton-Jacobi-Bellman (HJB) equation, thereby avoiding the complexity of traditional Bellman residual-based methods and relaxing the persistence of excitation condition. Based on the barrier Lyapunov function, it is proved that the proposed strategies can steer the spacecrafts to attitude consensus in a predefined time, and the states of multiple spacecraft do not violate the prescribed constraints. The simulation results verify the effectiveness of the proposed approach in a predefined time.

키워드

Timing; Titanium; Tracking; Design methodology; Matrices; Law; Attitude control; Geographic information systems; Bismuth; Business intelligence; Attitude consensus control; fuzzy logic systems (FLS); multiple spacecraft; optimal control; predefined-time control; reinforcement learning (RL); FAULT-TOLERANT CONTROL; COOPERATIVE CONTROL; NONLINEAR-SYSTEMS; STABILIZATION; DESIGN
제목
Predefined-Time Actor-Critic Learning for Constrained Spacecraft Attitude Consensus
저자
Zhou, Ying; Li, Yuan-Xin; Hou, Zhongsheng; Ahn, Choon Ki
DOI
10.1109/TAES.2026.3711617
발행일
2026
유형
Article
저널명
IEEE Transactions on Aerospace and Electronic Systems
권
62
페이지
13698 ~ 13711