期刊文献+

小卫星AIT流程简化探讨 被引量:11

Discussion on AIT Flow Minimization for Small Satellites
下载PDF
导出
摘要 调研了国外航天器总装、测试与试验(AIT)流程的发展,总结了快速AIT研制经验,包括简化或删除大型环境试验、采用自动化测试等。介绍了国内小卫星的传统AIT流程,指出由于体系构架、软件落焊等原因导致AIT流程过于繁琐。结合调研结果,从首发卫星、继承卫星和快速响应卫星三个方面给出了简化的国内小卫星AIT测试流程,优化方法包括删减环境试验、简化综合测试、提高总装效率等,并提出了卫星设计模块化,测试设备通用化和小型化,测试自动化,以及总装工作自动化等小卫星设计优化及测试方法的改进建议。 This paper provides an investigation of traditional spacecraft AIT (assembly, integra- tion, and test) flow in foreign countries, and summarizes the rapid AIT learning lessons: reduc- ing or removing environment tests, automatic testing, etc. Then the traditional satellite AIT flow in China is given and analyzed. Due to the system configuration, software solidifying and other factors, the traditional f AIT flow for first satellite, fo tively, which includes the met low is time-consuming. Based on the research, the minimization of llow-on satellite and rapid responsive satellite is presented respec- hods as reducing environment tests, simplifying integration tests, and making assembly procedure more efficiency. Satellite modularization, test equipment generali- zation and miniaturization, automatic testing, automatic assembly as well as other suggestions for small satellite design and test methods are given at the end of the paper.
出处 《航天器工程》 北大核心 2015年第1期120-125,共6页 Spacecraft Engineering
关键词 小卫星 总装 测试与试验 测试流程 small satellite AIT test flow
  • 相关文献

参考文献7

  • 1Wertz J,Larson W.Spacecraft mission analysis and design(SMAD)III[M].Holland Amsterdam:Kluwer Academic Publisher,1999.
  • 2Lisa A Baghal.Assembly,integration,and test methods for operationally responsive space satellites[D].Maxwell:Department of the Air Force,Air University,2010.
  • 3Casola A,Castelmani F,Di Serio M.New objectives of vibration testing during intensive rate satellite productions[C]//Proceedings of the 4th International Symposium on Environmental Testing for Space Programmes.Paris:ESA,2001:341-346.
  • 4Wendler B.Establishing minimum environmental test standards for space vehicles[C]//Proceedings of the21st Aerospace Testing Seminar.Washington D.C.:NASA,2003.
  • 5黄志澄.美国“太空快速响应”计划[J].国际太空,2006(10):14-17. 被引量:9
  • 6戴居峰,袁利,王跃.基于开放式结构的航天器控制系统测试技术研究[J].空间控制技术与应用,2012,38(5):34-37. 被引量:5
  • 7James Canoy.Improving electrical ground support equipment development for satellite testing[C]//Proceedings of 2011IEEE Systems Readiness Technology Conference(AUTOTESTCON 2011).New York:IEEE,2011:92-101.

二级参考文献5

共引文献12

同被引文献84

引证文献11

二级引证文献22

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