适应性固定时间滑动模式控制,用于航天器重定向,并具有态度指向约束和干扰排斥
Tao Guan1, Kai Zhang1, Bin Li1
1School of Aeronautics and Astronautics, Sichuan University, Chengdu, China.
ISA transactions
|October 8, 2023
概括
这项研究引入了一种用于太空船态度控制的新型控制器,确保固定的时间收和坚持指向约束,尽管存在不确定性. 它保证了稳定性和干扰拒绝,可靠的航天器机动.
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.
- 现有的方法在固定时间趋同和在不确定性下指向约束方面扎.
研究的目的:
- 开发一个强大的航天器重定向控制器.
- 为了实现固定时间的趋同与预先确定的时间.
- 满足态度指向约束和拒绝干扰.
主要方法:
- 一个非单一的固定时间滑动模式表面的设计,具有潜在的功能.
- 引入一个自适应的滑动模式控制方案.
- 莱普诺夫稳定性分析用于理论上的保证.
主要成果:
- 实现了与预先确定的时间的态度错误的固定时间收.
- 确保了对态度的满意度,指出了约束.
- 证明了有效的干扰排斥和无线性能.
- 通过数值模拟验证控制器的有效性.
结论:
- 拟议的控制器同时实现固定时间稳定性,约束满足和干扰拒绝.
- 该方法在不确定性下为航天器态度控制提供了卓越的性能.
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