期刊文献+

微型航天器模块化设计及其关键技术研究 被引量:10

Key technologies of modular design of micro-spacecraft facing micro-spacecraft family
下载PDF
导出
摘要 针对微型航天器柔性化设计问题,通过对国外微小卫星研制技术的分析,突破了传统的按分系统进行卫星设计的模式,提出了面向微型航天器族的微型航天器的模块化设计及其关键技术.该技术的提出对促进我国微小卫星的发展以及全面提高我国卫星总体研制技术水平具有一定的指导意义. Aiming at flexible design problem of micro - spacecraft, by analyzing research technologies of micro - satellites, and breaking through traditional design of satellites according to sub - systems, modular design theory of micro - spacecraft and its key technologies facing micro - spacecraft family were put forward. The proposition of modular design theory is meaningful for improving the development and researching level of micro - satellites.
出处 《哈尔滨工业大学学报》 EI CAS CSCD 北大核心 2007年第12期1908-1911,共4页 Journal of Harbin Institute of Technology
基金 国家安全重大基础研究973项目(5131201-2)
关键词 微型航天器族 微型航天器 模块化 功能模块 micro - spacecraft family micro - spacecraft modularity function module
  • 相关文献

参考文献13

  • 1BONNEVILLE R. Geostep: A gravitation experiment in earth - orbiting satellite to test the equivalence principle[ J]. Adv. Space Res, 2003, 32 (7) : 1367 - 1372. 被引量:1
  • 2LAFON T. JASON 1 : Lessons learned from the development and 1 year in orbit[J]. Acta Astronautica, 2005, 56(1 -2) : 45 -49. 被引量:1
  • 3DECHEZELLES J J, Gerard Huttin. Proteus: A Mutlimission platform for low earth orbits [ J ]. Air & Space Europe, 2000,2 (1) : 77 -81. 被引量:1
  • 4JACKSON B, CAMPBELL J. The subsystemless satellite - a new design paradigm for the next generation of small satellites [ C ]//12th AIAA/USU Conference on Small Satellites, SSC98 - V - 5, 1998. 被引量:1
  • 5GALEAZZI C. PRIMA: A New, Competitive Small Satellite Platform[ J]. Acta Astronautica, 2000, 46 (2 -6) : 379-388. 被引量:1
  • 6LIANG Xu -wen, LI L, LI Hua -wang, et al, Silicon solid- state small satellite design based on IC and MEMS[ OL/BL], http://ieeexplore. ieee. org. 1998 : 932 - 935. 被引量:1
  • 7ORII T, ONO T, AOYAMA J I, et al. Development of Versatile Small Satellite[J]. Acta Astronautica, 2002, 50(9) : 557 -567. 被引量:1
  • 8DRIBAULT L, DURTESTE C. The Leostar platform design and validation[J].Air & Space Europe, 2000, 2(1): 82-85. 被引量:1
  • 9BERGER G. A Smallsat approach to large missions [J]. Acta Astronautica, 1996, 39(9 - 12) : 993-999. 被引量:1
  • 10MARC F, MARTIN S. UOSAT-12 Minisatellite for High Performance Earth Observation at Low Cost[ J]. Acta Astronautica, 1997,41(3):173 -182. 被引量:1

同被引文献59

引证文献10

二级引证文献31

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