期刊文献+

空天飞行器大气传感技术研究 被引量:2

原文传递
导出
摘要 根据空天飞行器的特点和大气传感系统的技术类型,调研了国外典型空天飞行器的大气传感系统技术,明确了嵌入式大气数据传感技术适合空天飞行器,在此基础上分析了嵌入式大气数据传感系统的组成方案,并针对空天飞行器的特殊需求,梳理了嵌入式大气数据传感系统关键技术。
出处 《飞航导弹》 北大核心 2014年第6期3-9,共7页 AERODYNAMIC MISSILE JOURNAL
  • 相关文献

参考文献17

  • 1Judy L Shin.Comparison of predicted and experimental real-gas pressure distributions on space shuttle orbiter nose for shuttle entry air data system.NASA-TP-1627,1980.
  • 2Terry J Larson,Paul M.Use of nose cap and fuselage pressure orifices for determination of air data for space shuttle orbiter below supersonic speeds.NASA-TP-1643,1980.
  • 3Stephen A Whitmore,Brent R Cobleigh,Edward A Haering.Design and calibration of the X-33 flush airdata sensing (FADS) system.AIAA 98-0201.
  • 4Joel C Ellsworth,Stephen A Whitmore.Reentry air data system for a sub-orbital spacecraft based on X-34 design.AIAA 2007-1200.
  • 5Joel C Ellsworth,Stephen A Whitmore.Simulation of a flush air-data system for transatmospheric vehicles.Journal of spacecraft and rocket,2008,45(4):716-732.
  • 6Carlos Henrique Westhelle.X-38 backup air data system (AeroDAD).AIAA 2002-0007.
  • 7Arthur C Grantz.X-37B orbital test vehicle and derivatives.AIAA 2011-7315.
  • 8Christopher D Karlgaard,Roger E Beck,Stephen A O' Keefe,etc.Mars entry atmospheric data system modeling and algorithm development.AIAA 2009-3916.
  • 9Soumyo Dutta,Robert D Braun,Christopher D Karlgaard.Atmospheric data system sensor placement optimization for mars entry,descent,and landing.AIAA 2012-4507.
  • 10Mark C Davis,Joseph W Pahle,John Terry White,etc.Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at mach 3 to 8.AIAA 2000-0504.

同被引文献23

引证文献2

二级引证文献6

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