对于没有角速度传感器的灵活航天器而言,固定的时间容错的态度控制
Muhammad Noman Hasan1, Yong Chen2, Jiongjiong Liang1
1Yangtze Delta Region Institute of University of Electronic Science and Technology (UESTC), Huzhou, Zhejiang, 313001, China.
ISA transactions
|December 21, 2023
概括
本研究介绍了一种用于灵活航天器的新型固定时间故障耐受态度控制系统,仅使用态度数据实现精确的控制和振动抑制,即使执行器故障.
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.
- 灵活的航天器动力学引入了像振动这样的复杂性.
- 执行器故障和外部干扰带来了重大挑战.
研究的目的:
- 为灵活的航天器开发一个固定的时间容错的态度控制策略.
- 为了实现态度控制和抑制振动,仅使用态度信息.
- 为了确保对参数变化,干扰和执行器故障的稳定性.
主要方法:
- 设计了一个自适应的固定时间无模型观察器 (AFTMFO) 用于角度速度估计.
- 合成了一种新的自适应连续控制,使用一种反解的快速固定时间非单元滑动表面 (AFFTNSS).
- 采用Lyapunov技术来确保闭环稳定性.
主要成果:
- 实现了无速度传感器的固定时间态度,以高指向精度进行机动.
- 证明了灵活的附属体的有效抑制振动.
- 展示了故障耐受性和无聊控制,并改进了融合速度.
结论:
- 拟议的控制方案为灵活的航天器提供了强大的,固定的时间故障耐受性态度控制.
- 它有效地抑制振动,没有额外的传感器.
- 与现有方法相比,该方法提供了更高的性能和更少的控制力.
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