期刊文献+

航天器动力学试验评价技术 被引量:7

Summarization of Spacecraft Dynamics Test and Evaluation Technologies
下载PDF
导出
摘要 回顾了国内外航天器动力学试验评价技术的研究和应用,分析了国内航天器动力学试验存在的问题,阐述了复杂航天器的发展对于航天器动力学试验评价体系提出的新要求,重点分析了在评价内容、航天器环境、航天器环境模拟方法、航天器环境效应、测量与分析、评价方法及准则方面必须突破和解决的若干关键技术,展望了航天器动力学试验评价技术的发展前景。 The research and applications of spacecraft dynamics test evaluation techniques at home and abroad were reviewed. The problems of spacecraft dynamic test in our country were analyzed, and new requirements for spacecraft dynamics test and evaluation system as the development of complex spacecraft system were introduced. Some key technologies must be broken through and solved in the aspects of evaluation contents, spacecraft environment, environmental simulation and effects of spacecraft, measurement and analysis evaluation methods, and criteria were analyzed. The development of spacecraft dynamics test evaluation techniques was prospected.
出处 《装备环境工程》 CAS 2012年第3期5-10,共6页 Equipment Environmental Engineering
关键词 评价技术 航天器 动力学试验 故障诊断 evaluation techniques spacecraft dynamics test fault diagnosis
  • 相关文献

参考文献5

二级参考文献12

  • 1王梦魁.多维振动环境试验的实践[J].装备环境工程,2005,2(3):22-25. 被引量:22
  • 2夏益霖.多轴振动环境试验的技术、设备和应用[J].导弹与航天运载技术,1996(6):48-55. 被引量:29
  • 3Chang K Y,Frydman A M. Three-dimensional random vibration definition and simulation[C]. Proceeding of IES, 1990:129-139.
  • 4George A Hamma, Richard C Stroud, Marcos A Underwood. A review of multiaxis/ multiexciter Vibration Technology[J]. Sound and Vibration, 1996,4 : 20-27.
  • 5陈颖,朱长春,周德惠,王雄祥.多轴模拟振动试验技术发展现状[C].第七届全国激光科学技术青年学术交流会论文集,2003:221-224.
  • 6陈颖,朱长春,宁佐贵.某隔振平台的多轴随机振动试验研究[C].中国宇航学会结构强度与环境工程专委会学术研讨会论文集,2006:35-40.
  • 7美国ANSYS公司北京办事处.ANSYS动力学分析指南[M].北京:2000.
  • 8M E McNelis,T D Scharton.Benefits of force limited vibration testing. NASA/TM- . 1999
  • 9T D Scharton.Force limited vibration testing monograph[]..1997
  • 10金恂叔.21世纪航天器的环境试验[J].国际太空,1999(5):19-20. 被引量:5

共引文献33

同被引文献76

引证文献7

二级引证文献32

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