期刊文献+

民用飞机飞控计算机的现状与展望 被引量:6

A Present and Future Perspective for Flight Control Computer of Civil Aircraft
下载PDF
导出
摘要 自从1988年空客A320采用电传飞控系统,在新的民用飞机的设计中,电传飞控系统已成为飞行控制系统的唯一选择。作为飞控系统的核心——飞控计算机,必须具备高安全性和高可靠性。本文介绍了空客A3XX和波音777飞控计算机的结构,并陈述了综合化的发展趋势。 Since it entried into commercial airplane service on the Airbus A320 in 1988, the all-electronic fly -by -wire system has gained such popularity that it is becoming the only one control system used on new airlines. So flight control computer, as a core of FBW, must have high safety and high reliability. This paper introduces the architecture of the flight control computers for Airbus A3XX and Boeing777, and presents the future integrated perspectives.
作者 杨菊平 陈益
出处 《航空计算技术》 2007年第5期131-134,共4页 Aeronautical Computing Technique
关键词 电传飞控系统 飞控计算机 综合化模块化航电 FBW flight control computer IMA
  • 相关文献

参考文献8

  • 1Lui Sha.Using Simplicity to Control Complexity[J].IEEE SOFTWARE July/August,2001:20 -28.
  • 2陈宗基,秦旭东,高金源.非相似余度飞控计算机[J].航空学报,2005,26(3):320-327. 被引量:41
  • 3Yeh Y.C.Safety critical avionics for the 777 primary flight control system[A].Digital Avionics Systems,2001 DASC.The 20t h Conference:Volume 1[C].2001.14-18.
  • 4Naidu.Case study:Airbus A340 flight control system[D].University of Virginia,2002:1-12.
  • 5Yeh Y.C.Triple-Triple Redundant 777 Primary Flight Computer[A].IEEE Aerospace Applications Conference[C].1996:27 -35.
  • 6James W.Ramsey.Boeing 787:Integration's Next Step[C].Defense Daily Network,June 2005:168-174.
  • 7AGARD,Integrated Vehicle Management Systems[R].AGAR-DAdvisory Report 343,1996:46 -57.
  • 8Lui Sha.A Software Architecture for Dependable and Evolvable Industrial Computing Systems[R].Technical Report CMU/SEI-95-TR-005 ESC-TR-95 -005,1995:21 -27.

二级参考文献14

  • 1Kienzle J. Software fault tolerance : a tutorial [R]. Ada-Europe 2003.45-67.
  • 2Collinson R P G . Fly-by-wire flight control[J]. Compu-ting and Control Engineering Journal, 1999,10(4):141-152.
  • 3Yeh Y C. Design considerations in Boeing 777 fly-by-wire computers[A]. High-Assurance Systems Engineering Symposium[C]. 1998. 64-72.
  • 4Yeh Y C. Safety critical avionics for the 777 primary flight control system[A]. Digital Avionics Systems, 2001. DASC. The 20th Conference: Volume 1[C] . 2001.14-18.
  • 5Yeh Y C. Triple-triple redundant 777 primary flight computer[A]. Aerospace Applications Conference[C]. 1996.293-307.
  • 6Aplin J D. Primary flight computer for the Boeing 777[J]. Microprocessors and Microsystems, 1997, 20:473-478.
  • 7Jon Rea P E. Boeing 777 high life control system[J]. IEEE AES Systems Magazine,1993, 8(8):15-21.
  • 8张新国.从Boeing 777客机飞行控制系统分析飞控系统容错设计及可靠性技术的发展[R].技术报告[R].飞行自动控制研究所,1993..
  • 9Briere D, Traverse P. Airbus A320/A330/A340 electrical flight control-A family of fault-tolerant systems[C].France: 1993.616-623.
  • 10Burgner N. Airbus A320 family still going strong[Z]. http://www.flug-revue.rotor.com/FRheft/FRH9709/FR9709a.htm.

共引文献40

同被引文献27

引证文献6

二级引证文献15

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