事件触发的自适应式预定义时间反解姿态跟踪控制器用于航天器
Guogang Wang1, Zichao Feng1, Youyang Qu2
1School of Information and Control Engineering, Jilin University of Chemical Technology, Jilin, China.
PloS one
|October 22, 2025
概括
这项研究引入了一种新的航天器态度控制系统,用于预定义时间的融合,解决干扰和未知的参数. 控制器通过事件触发机制确保稳定性,防止解,并减少通信负载.
科学领域:
- 航空航天工程 航空航天工程
- 控制系统理论 控制系统理论
- 机器人技术 机器人技术 机器人技术
背景情况:
- 太空飞船的态度控制对于任务的成功至关重要.
- 现有的方法面临外部干扰,未知的惯性和四解卷问题等挑战.
- 需要有效的通信策略来减少数据传输负载.
研究的目的:
- 开发一款具有预定义时间收的航天器态度跟踪控制器.
- 为了解决四基航天器建模中的解现象.
- 实施事件触发机制以减少通信负担.
主要方法:
- 设计一个预定义时间的非单一的滑动表面,以便快速收.
- 引入一个潜在的功能,以确保反解行为.
- 开发一个事件触发的控制机制,以避免Zeno行为和减少通信.
主要成果:
- 闭环系统在预定义的时间内实现了趋同.
- 控制器有效地抑制了喋喋不休的声音,并保证了反解性能.
- 事件触发机制可以降低通信负载,而不会影响系统稳定性.
- 态度跟踪错误汇聚到一个预定义的剩余集.
结论:
- 拟议的控制方法为刚性航天器提供了强大的预定义时间态度跟踪.
- 综合方法有效地处理干扰,未知参数和解问题.
- 事件触发机制为航天器控制系统提供了高效的通信解决方案.
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