Structural design and experimental verification of the composite flexible thin rod

doi:10.19936/j.cnki.2096-8000.20230628.016

Abstract

Abstract: The flexible deceleration brush de-rotation method is an existing contact active de-rotation technique for free tumbling targets in space. According to the technical requirements of the flexible brush tool for a certain type of deceleration brush de-rotation device, a kind of flexible thin rod of carbon fiber composites was designed. By carrying out finite element simulation analysis, the rationality of the structural design scheme was verified. Thin rod samples were prepared by rubbing-winding process. Randomly selected samples were tested for validation. The test results show that, both the bundling stiffness of 24 composite flexible thin rods and the maximum bending deflection of a single composite flexible thin rod meet the basic design requirements. The results of the simulation analysis are in accordance with the experimental results. This research work has laid the foundation for subsequent research into the application of the component on the deceleration brush de-rotation device.

Key words: composite, flexible thin rod, deceleration brush, simulation analysis, stiffness test

CLC Number:

TB332

LIANG Xuhao, ZHANG Juanjuan, SHEN Feng, CHEN Yongxiao, WANG Xiaolei, BAI Ruixiang. Structural design and experimental verification of the composite flexible thin rod[J]. COMPOSITES SCIENCE AND ENGINEERING, 2023, 0(6): 115-119.

References

[1] 林来兴. 空间碎片现状与清理[J]. 航天器工程, 2012, 21(3): 1-10.
[2] ABAD A F, MA O, PHAM K, et al. A review of space robotics technologies for on-orbit servicing[J]. Progress in Aerospace Sciences, 2014, 68: 1-26.
[3] 崔乃刚, 王平, 郭继峰, 等. 空间在轨服务技术发展综述[J]. 宇航学报, 2007, 28(4): 805-811.
[4] 翟光, 仇越, 梁斌, 等. 在轨捕获技术发展综述[J]. 机器人, 2008, 30(5): 467-480.
[5] 路勇, 刘晓光, 周宇, 等. 空间翻滚非合作目标消旋技术发展综述[J]. 航空学报, 2018, 39(1): 021302.
[6] NISHIDA S I, KAWAMOTO S. Strategy for capturing of a tumbling space debris[J]. Acta Astronautica, 2011, 68(1): 113-120.
[7] DANESHJOU K, ALIBAKHSHI R. Multibody dynamical modeling for spacecraft docking process with spring-damper buffering device: A new validation approach[J]. Advances in Space Research, 2018, 61(1): 497-512.
[8] KAWAMOTO S, KOHTARO M, SACHIKO W. Ground experiment of mechanical impulse method for uncontrollable satellite capturing[C]//Proceeding of the 6th International Symposium on Artificial Intelligence and Robotics & Automation in Space (i-SAIRAS). Montreal: Canadian Space Agency, 2001.
[9] WANG D, HUANG P, MENG Z. Coordinated stabilization of tumbling targets using tethered space manipulators[J]. IEEE Transactions on Aerospace and Electronic Systems, 2015, 51(3): 2420-2432.
[10] MATUNAGA S, KANZAWA T, OHKAMI Y. Rotational motion-damper for the capture of an uncontrolled floating satellite[J]. Control Engineering Practice, 2001, 9(2):199-205.
[11] GOMEZ N O, WALKER S J I. Guidance, navigation, and control for the eddy brake method[J]. Journal of Guidance, Control, and Dynamics, 2017, 40(1): 52-68.
[12] PETERS T V, OLMOS E D. COBRA contactless de-tumbling[J]. CEAS Space Journal, 2016, 8(3): 143-165.
[13] 赵一鸣. 基于库仑力的非接触式目标消旋研究[D]. 哈尔滨: 哈尔滨工业大学, 2016.
[14] 马广富, 郭延宁, 邱爽, 等. 空间非合作目标消旋技术研究现状总结与展望[J]. 飞控与探测, 2018, 1(1): 026-033.
[15] 孙晟昕, 吴昊, 魏承, 等. 基于柔性毛刷的自旋卫星的消旋动力学分析[J]. 中国科学:物理学力学天文学, 2019, 49: 024515.
[16] 王耀先. 复合材料力学与结构设计[M]. 上海: 华东理工大学出版社, 2012.
[17] 王勖成. 有限单元法[M]. 北京: 清华大学出版社, 2003.
[18] 徐芝纶. 弹性力学[M]. 北京: 高等教育出版社, 2016.
[19] 袁家军. 卫星结构设计与分析[M]. 北京: 中国宇航出版社, 2004.
[20] 关鑫, 王洪雨, 徐挺, 等. 某型无人机碳纤维复合材料尾撑杆研制[J]. 复合材料科学与工程, 2020(11): 61-65.