期刊文献+

神舟七号微小卫星伴随飞行技术试验 被引量:5

Companion Microsatellite in SZ-7 Flight Mission
下载PDF
导出
摘要 神舟七号(SZ-7)载人航天任务中释放的一颗微小伴随卫星(BX-1),首次开展了卫星在轨释放、对飞船观测和对轨道舱接近及绕飞等技术试验.该卫星首次进行了GaInP2/GaAs/Ge中国产太阳电池阵、锂离子蓄电池、微型液氨推进模块、小型化姿态跟踪控制模块、双焦距一体化可见光相机及小型化USB测控应答机等技术验证.本文介绍了SZ-7微小卫星的设计方案,讨论了形成稳定伴随飞行的轨道设计等技术,并根据卫星在轨运行情况对试验任务进行了评价. The BX-1 micro-satellite, successfully released from the Shenzhou-7 (SZ-7) module, accomplished the purposes of providing the images of the SZ-7 and demonstrating the ability to inspect the orbital module and conduct proximity operations around the SZ-7 module. The BX-1 was a demonstrator for many new space technologies, including GaInP2/GaAs/Ge solar cells, lithiumion battery, micro-ammonia thruster, micro-attitude tracking controller, camera with double-focusing systems and micro-USB-responsor. The criterion of forming the stable elliptic orbit around the SZ-7 module is discussed in this paper. The evaluation of the BX-1 micro-satellite mission is provided by flight datum.
出处 《空间科学学报》 CAS CSCD 北大核心 2009年第3期319-325,共7页 Chinese Journal of Space Science
关键词 微小卫星 伴随飞行 空间观测 相对轨道 SZ-7载人飞行 Micro-satellite, Companion flying, Space observation, Relative-orbit, SZ-7 spaceflight
  • 相关文献

参考文献7

  • 1朱振才,杨根庆,余金培,张锐.微小卫星组网与编队技术的发展[J].上海航天,2004,21(6):46-49. 被引量:16
  • 2Kerstein L. The X-Mir Inspector Mission. 1995, IAF-95-T.3.02:1-10
  • 3Wilde D. The Inspector Family. 1995, IAF-95:1-8
  • 4Kerstein L. Free-Flyer Services on and Around the International Space Station. ESA SP-433, 1999. 2:149-155
  • 5Clohessy W H, Wiltshire R S. Terminal guidance system for satellite rendezvous. J. Aeros. Sci., 1960, 27(5): 653-674
  • 6Hill G W. Researches in the lunar theory. Amer. J. Math., 1878, 1(1):5-26
  • 7吴汉基,蒋远大,张志远,王鲁峰.微小卫星的在轨推进技术[J].火箭推进,2006,32(3):40-43. 被引量:14

二级参考文献7

  • 1边炳秀.卫星推进系统的历史、现状和未来[J].控制工程(北京),2001(5):28-39. 被引量:5
  • 2吴汉基.脉冲等离子体电火箭在卫星控制方面的应用[J].电工电能新技术,1986,(3):27-33.
  • 3[3]R M Myers,S R Oleson,Melissa Mcguire,et al.Pulsed plasma thruster technology for small satellite missions[C].In:Proc.of the 9th annual AIAA/USU Conf.of small satellite,1995.
  • 4[4]Gregory G,Spanjers,Daron R,Bromaghim,et al.AFRL MicroPPT development for small spacecraft propulsion[R].AIAA 2002-3974.
  • 5RIDER L. Analytic design of satellite constellations for zonal earth coverage using inclined circular orbits [J]. J of the Astronautical Sciences, 1987, 35(4): 155-192.
  • 6ADAMS W S, RIDER L. Rosette constellations of earth satellites [J]. IEEE Trans. Aerosp. Electron.Syst. , 1980, 16(5): 656-673.
  • 7吴汉基,蒋远大,张志远.电推进技术的应用与发展趋势[J].推进技术,2003,24(5):385-392. 被引量:71

共引文献28

同被引文献26

  • 1刘鹏,赵平.氢化处理铸造镁锂系合金[J].铸造,2006,55(5):505-508. 被引量:12
  • 2李红斌,吉海宾,姚广春,刘宜汉,郭志强,刘振刚.新型Mg-Li-Mn合金的显微组织和力学性能[J].过程工程学报,2006,6(3):491-494. 被引量:2
  • 3王素洁,吴国清,李瑞华,罗根香,黄正.5wt%YAl_2p/Mg-Li复合材料的组织与性能的研究[J].航空材料学报,2007,27(1):20-22. 被引量:5
  • 4刘滨,张密林.Ce对Mg-Li-Al合金组织及力学性能的影响[J].特种铸造及有色合金,2007,27(5):329-331. 被引量:23
  • 5Kerstein L. The X-Mir Inspector Mission [C]//46th International Astronautical Congress. Oslo, Norway: IAF, 1995:1-10.
  • 6Hirt C W, Nichols B D. Volume of Fluid (VOF) Method for The Dynamics of Free Boundaries [J]. J. Comput. Phys., 1981, 39:201-225.
  • 7Sussman M, Smereka P, Osher S. A Level Set Approach for Computing Solutions to Incompressible Two-Phase Flow [J]. J. Comput. Phys., 1994, 114:146-154.
  • 8Stark J A, Bradshow R D, Blatt M H. Low-g Fluid Behavior Technology Summaries [R]. NASA-CR-134746, 1974.
  • 9Dodge F T. Fhrther Studies of Propellant Sloshing Under Low Gravity Conditions [R]. NASA-CR-119892, 1971.
  • 10ARMEN T. Redesign of the poly picosatellite orbital de- ployer for the dnepr launch vehicle [ D ]. San Luis Obis- po, California: California Polytechnic State University, 2007.

引证文献5

二级引证文献4

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