结构设计,准确性分析和机械校准一个小型的两组合对接机制,用于太空中的大型负载
Jule Zhang1,2, Junjie Li1,2, Chong Zhao1
1Key Laboratory of Space Utilization, Technology and Engineering Center for Space Utilization, Chinese Academy of Sciences, Beijing, 100094, China.
Scientific reports
|February 7, 2025
概括
一个新的紧的,高精度的双组件对接机制被设计用于组装大型空间有效载荷. 该系统使用渐进定位来准确地对接连接器的对接,这对于轨道建设至关重要.
科学领域:
- 航空航天工程 航空航天工程
- 机器人和自动化机器人与自动化
背景情况:
- 被动对接组件的最终完成需要先进的机制,以在太空中组装大型有效载荷.
- 使用现场资源在轨道上组装需要强大而精确的对接解决方案.
研究的目的:
- 为大型空间负载设计一个紧的,高精度的双组件对接机制.
- 为了能够准确地在轨道上组装空间站组件.
主要方法:
- 积极和被动对接元件的参数设计与约束方程.
- 实施渐进定位方法 (粗到细的校正).
- 分析双组件校准,定位性能和静态负载能力.
主要成果:
- 原型测试显示最大位置偏差为0.12 mm (X),0.5 mm (Y) 和0.07 mm (Z).
- 在双组件操作过程中,最大角偏差在0.04°时被测量.
- 静态分析证实了负载能力和直径之间的正相关性.
结论:
- 开发的对接机制满足了轨道上的轴向和辐射对接条件的负载要求.
- 渐进定位策略有效捕捉大偏差,并实现高精度对接.
- 这项研究为未来的太空对接机制开发提供了宝贵的理论和技术见解.
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