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空间柔性绳网纠缠组合体拖曳动力学仿真分析

张瑞雄 王东辉 刘志 赵丹 王治易

上海航天(中英文)2026,Vol.43Issue(3):44-53,10.
上海航天(中英文)2026,Vol.43Issue(3):44-53,10.DOI:10.19328/j.cnki.2096-8655.2026.03.005

空间柔性绳网纠缠组合体拖曳动力学仿真分析

Simulation Analysis on Towing Dynamics of Space Flexible Tether-net Entanglement Combination

张瑞雄 1王东辉 1刘志 1赵丹 2王治易1

作者信息

  • 1. 宇航空间机构全国重点实验室,上海 201109||上海宇航系统工程研究所,上海 201109
  • 2. 上海宇航系统工程研究所,上海 201109
  • 折叠

摘要

Abstract

Space flexible tether-net is an effective way to capture and remove failed spacecraft and space debris in orbit.In this paper,a towing dynamics model of flexible tether-net entanglement combination is established based on the continuum mechanics,concentrated mass method,and Hertz contact theory,and a simulation analysis is conducted on the towing process.The results show that when an active spacecraft tows a non-spinning target or a spinning target at a 15(°)/s spin speed,the target spin will intensify the entanglement of the tether-net entanglement combination,which may generate new space debris.Adding buffer components between the active spacecraft and target can reduce the peak tension of the towing tether-net,shorten the time of the tether-net combination for forming a stable towing state,reduce the interference with the active spacecraft,and improve the reliability of towing missions.The dynamic simulation analysis can provide reference for the formulation of in-orbit target removal strategies.

关键词

空间柔性绳网/空间碎片/拖曳动力学/接触碰撞/系统仿真

Key words

space flexible tether-net/space debris/towing dynamics/contact collision/system simulation

分类

航空航天

引用本文复制引用

张瑞雄,王东辉,刘志,赵丹,王治易..空间柔性绳网纠缠组合体拖曳动力学仿真分析[J].上海航天(中英文),2026,43(3):44-53,10.

基金项目

国家重点基础研究发展计划资助项目(2013CB733004) (2013CB733004)

上海航天(中英文)

2096-8655

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