基于共识的航天器姿态对准控制器:仿真结果

H. Septanto, Bambang Riyanto-Trilaksono, A. Syaichu-Rohman, Ridanto Eko-Poetro
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引用次数: 9

摘要

采用一致性算法的航天器编队飞行控制是指一个小组中的每个航天器或卫星根据其局部邻居的信息状态更新自己的状态,使每个智能体的最终信息状态收敛到一个公共值。本文讨论了航天器在旋转运动即姿态对准范围内的编队问题。提出了两种基于一致性算法的姿态对准控制器。模拟运行作为初步证明的概念提出。仿真结果表明,所提出的控制律能够很好地解决姿态对准问题,即达到一致。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Consensus-based controllers for spacecraft attitude alignment: Simulation results
Spacecraft formation flying control using consensus algorithm means each spacecraft or satellite in a team updates its state based on the information states of its local neighbours in such a way that the final information state of each agent converges to a common value. This paper discusses spacecraft formation within scope of rotational motions i.e. attitude alignment. Two attitude alignment controllers based on consensus algorithm proposed here.Simulations that run as preliminary proof a concept are presented. Simulations run indicate the proposed control laws might solve the attitude alignment problem i.e. consensus is achieved.
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