期刊文献+

激光驱动典型几何形状碎片运动建模研究 被引量:3

Dynamic modeling of laser-driven space debris of typical shapes
下载PDF
导出
摘要 在以往的激光烧蚀驱动移除空间碎片研究中,均假设激光光束覆盖整个所关注的空间碎片。文章提出了焦斑式激光辐照下球体、圆柱体和立方体碎片反喷冲量和运动姿态的计算模型,研究了激光辐照在3种形状碎片不同位置处所产生的反喷冲量和姿态变化规律。结果表明:碎片运动规律与碎片几何形状和激光作用位置有关,当反喷冲量过质心时,碎片获得平动冲量;不过质心时,则会改变碎片的角速度或姿态。研究结果可为激光移除空间碎片研究提供理论参考。 In the active removal of space debris by the laser-driven method,it is assumed that the laserbeams cover the whole debris assemble.This paper proposes to focus the laser beams into a small focal spot onthe debris surface.A simple motion model is built to calculate the impulse and the attitude of the space debris oftypical shape under a small laser spot irradiation.Fragments in shapes of sphere,cylinder and cube are selected.It is indicated that the momentum transfer by the laser ablation is related with the shape of the debris and theirradiated position.If the impulse direction is along the normal direction of the irradiated surface,the angularvelocity of the debris will not change,on the other hand,if the impulse direction is not through the center ofmass,the angular velocity and the attitude of the debris will change.The results of this paper may provide atheoretical basis for the active debris removal by the laser-driven method.
作者 张品亮 龚自正 汤秀章 陈川 杨武霖 ZHANG Pinliang;GONG Zizheng;TANG Xiuzhang;CHEN Chuan;YANG Wulin(Science and Technology on Reliability and Environmental Engineering Laboratory, Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;China Institute of Atomic Energy, Beijing 102413, China)
出处 《航天器环境工程》 2017年第2期138-142,共5页 Spacecraft Environment Engineering
基金 国家自然科学基金项目(批准号:11505299) 可靠性与环境工程技术重点实验室开放基金项目
关键词 空间碎片 焦斑式辐照 运动建模 典型几何形状 space debris laser spot irradiation dynamic modeling typical shapes
  • 相关文献

参考文献3

二级参考文献13

  • 1Kaplan M H. Survey of space debris reduction methods[R]. AIAA-2009-6619, 2009.
  • 2Phipps C, Birkan M, Eckel H A, et al. Review: laser-ablation propulsion[J]. Journal of Propulsion and Pozver,2010,26(4): 609-637.
  • 3Campbell J W. Project Orion: orbital debris removal using ground-based sensors and lasers[C]//The Second European Conference on Space Debris. 1997:699-701.
  • 4Phipps C, Albrecht G, Friedman H, et al. Orion: clearing near-earth space debris using a 20-kW, 530-nm, earth-based, repetitively pulse laser[J]. Laser and Particle Beams, 1996,14(1) : 1-44.
  • 5Cho M. Removal of orbital debris ~rom low earth orbit by laser-generated drag[J]. J Spacecraft, 1994,31(5) : 920-922.
  • 6Barty C P J, Caird J A, Erlandson A E, et al. High energy laser for space debris removal[R]. LLNL-TR-419114, 2009.
  • 7Schall W O. Laser radiation for cleaning space debris from lower earth orbits[J]. Journal of Spacecr@ and Rockets, 2002,39(1):81-91.
  • 8Liedahl D A, Libby S B, Rubenchik A. Momentum transfer by laser ablation of irregularly shaped space debris. High-power laser ablation [R]. LLNL-PROC-423224, 2010 : 7-16.
  • 9Claude R. Phipps,Kevin L. Baker,Stephen B. Libby,Duane A. Liedahl,Scot S. Olivier,Lyn D. Pleasance,Alexander Rubenchik,James E. Trebes,E. Victor George,Bogdan Marcovici,James P. Reilly,Michael T. Valley.Removing orbital debris with lasers[J].Advances in Space Research.2012(9)
  • 10J.-C. Liou.An active debris removal parametric study for LEO environment remediation[J].Advances in Space Research.2011(11)

共引文献88

同被引文献67

引证文献3

二级引证文献9

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部