一个修改的预先分配的有限时间控制方案,用于航天器的大角度态度机动和跟踪
Xudong Ma1, Yuan Liu1, Yi Cheng2
1School of Aeronautics and Astronautics, Sun Yat-sen University, Shenzhen 518107, China.
Sensors (Basel, Switzerland)
|February 13, 2025
概括
这项研究介绍了一种新的航天器态度控制系统,该系统可以处理限制和故障,以实现精确的机动. 控制器确保稳定性和性能,尊重执行器的限制和干扰.
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.
- 现有的方法与大角度机动,执行器约束和故障作斗争.
研究的目的:
- 开发一个强大的控制战略,用于大角度航天器的态度操纵和跟踪.
- 为了解决角速度,扭矩限制,执行器故障和外部干扰.
主要方法:
- 构建了一个类似滑动模式的向量,以满足角速度约束.
- 设计了一个修改的预分配有限时间函数,用于适应性边界调整.
- 利用一个屏障Lyapunov函数用于闭环系统稳定.
- 实施了适应性补偿执行器和和固定时间干扰观察器.
主要成果:
- 证明了闭环系统的实际预分配的有限时间稳定性.
- 实现了保证过渡和稳定状态的性能.
- 防止过度的角度速度,并确保执行器符合要求.
- 通过模拟验证了控制器的有效性.
结论:
- 拟议的控制器为挑战航天器态度控制场景提供了强大的解决方案.
- 它有效地管理约束,故障和干扰,提高任务可靠性.
- 模拟结果证实了控制器的实际适用性和性能.
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