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基于并行层次方案的集成轨道 - 态度 - 振动合动力学和大型航天器的控制
Bailiang Lyu1, Xiaokui Yue1, Chuang Liu1
1National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China; Research & Development Institute of Northwestern Polytechnical University in Shenzhen, Shenzhen 518057, China.
ISA transactions
|January 8, 2025
概括
本研究介绍了大型航天器的综合模型控制方案,同时管理轨道,态度和振动. 这种新的方法提高了太空任务中复杂,合动态的控制精度.
科学领域:
- 航空航天工程 航空航天工程
- 控制系统工程 控制系统工程
- 应用数学 应用数学 应用数学
背景情况:
- 大型航天器在轨道,态度和振动上表现出复杂,时间变化的合动力学.
- 现有的方法经常简化模型,可能会丢失关键的动态信息.
- 同时控制多个动态方面对于任务的成功至关重要.
研究的目的:
- 开发大型航天器的综合模型控制方案.
- 为了解决轨道-态度-振动动态的强时间变化的合特性.
- 为了实现同时维护轨道,稳定气态和抑制振动.
主要方法:
- 使用绝对节点坐标配方和拉格朗日力学建立了一个集成的动态模型,保持时间变化的合.
- 提出了一个平行分层方案,用于联合集成建模控制设计,避免复杂的计算.
- 通过同等动态转换进行独立的振动控制,并采用基于干扰观察器的终端滑动模式控制器.
主要成果:
- 拟议的方案有效地处理了非简化的变时合动态模型.
- 实现了轨道和态度的同时稳定,并自动抑制振动.
- 数字模拟验证了大型航天器系统的有效性和性能.
结论:
- 综合模型控制方案为复杂的航天器动态提供了精确有效的解决方案.
- 平行分层方法简化了控制设计,同时保持了高精度.
- 这种方法增强了大型太空任务的合作控制能力.
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