Distributed adaptive attitude consensus of networked spacecraft on directed graphs

Lijiao Wang
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引用次数: 2

Abstract

In this paper, we address attitude consensus problem of multiple spacecraft in the presence of dynamic uncertainties and bounded constant time delays. The agents are assumed to interact on strongly connected graphs. The consensus objective is achieved via the construction of the reference systems, where the quaternion-based nonlinear inner coupling of the attitudes is utilized as the reference control input such that the attitudes of the reference systems are driven to synchronize asymptotically. Then, based on the reference systems, we perform the quaternion-based adaptive controller design to achieve consensus of the networked spacecraft. The convergence of consensus errors is proved with energy-based analysis structure and Lyapunov stability tool. Finally, simulation with networked spacecraft is included to validate the effectiveness of the proposed strategy.
网络航天器在有向图上的分布式自适应姿态一致性
研究了存在动态不确定性和有界常数时滞的多航天器姿态一致性问题。假设代理在强连接图上交互。共识目标是通过构建参照系来实现的,其中利用基于四元数的姿态非线性内部耦合作为参照系控制输入,从而驱动参照系的姿态渐近同步。然后,在参考系统的基础上,进行了基于四元数的自适应控制器设计,实现了网络化航天器的一致性。利用基于能量的分析结构和Lyapunov稳定性工具证明了一致性误差的收敛性。最后,通过网络化航天器的仿真验证了所提策略的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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