卫星
姿态控制
集合(抽象数据类型)
控制理论(社会学)
控制(管理)
计算机科学
航空学
航空航天工程
遥感
工程类
地理
人工智能
程序设计语言
作者
Shijie Zhang,Tingting Zhang,Haibo Guo,Fan Zhang
标识
DOI:10.1016/j.actaastro.2021.10.043
摘要
This paper investigates the problem of general attitude cooperative control for different satellite formation structures from a new perspective of set theory. A virtual single-integral nonlinear node dynamic system is first presented. Then the general satellite attitude cooperative controller can be designed based on the virtual node dynamic system and consensus theory. The stability of the closed-loop system with respect to the goal set is analyzed by integral input to state stable method. Subsequently, two different scenarios, leaderless and leader-following satellite formation structures, are introduced by the general attitude cooperative control scheme. Corresponding simulations of these two scenarios verify the obtained theoretical results.
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