期刊文献+

气球控制安全中的双机冗余设计 被引量:11

Dual-host redundancy design on safe control of balloon
下载PDF
导出
摘要 分析现代战争的特点和气球载雷达的功能,指出气球载雷达具有长时间浮空的特性。为了满足气球控制系统稳定可靠,能够长时间滞空工作的要求,提出了一种采用双计算机并行工作,热备份冗余切换的双机容错系统的设计方案。通过实际项目验证,气球可以数月系留工作,满足气球载雷达球控系统滞空工作的高可靠性要求。 The floating time of aerostat-load-radar is very long in modern warfare.Therefore the high stable and reliable balloon control system is needed.A design scheme of dual-host redundancy system was put forward,which adopted two host computers working together and the two computers could switch in real time.The scheme was verified through actual project.The balloon can work for several months,which meet the reliability requirements of the balloon control system in aerostat-load-radar.
作者 黄翌 陈丽娟
出处 《信息与电子工程》 2010年第3期357-359,共3页 information and electronic engineering
关键词 气球载雷达 球控系统 双机容错 仲裁算法 aerostat-load-radar balloon control system dual-host redundancy arbitrating algorithm
  • 相关文献

参考文献4

二级参考文献18

  • 1帖军,陆际光.同步互斥机制中的读者-写者模型[J].中南民族大学学报(自然科学版),2005,24(3):67-70. 被引量:4
  • 2BOSCH.CAN Specification Version 2.0[EB/OL].[1991-09].http://www.semiconductors.bosch.de/pdf/CAN2spec.pdf.
  • 3Barranco M,Almeida L,Proenza J.ReCANcentrate:A replicated star topology for CAN networks[C]// Proc.10th IEEE conference on 2005 ETFA.2005,2:8,476.
  • 4Barranco M,Proenza J,Rodriuez-Navas G,et al.An active Star Topology for Improving Fault Confinement in CAN Networks[J].IEEE trans.on Industrial informatics,2006,2(2):78-85.
  • 5Sivencrona H,Nilsson G,Bj?rn F.A Novel Distributed Add-on Concept to Detect and Recover from Bus Failures in Controller Area Network using REDCAN[C]// Proc.8th International CAN Conference(ICC-08).2002.
  • 6Lin C E,Yen H M.A Prototype Dual CAN-BUS Avionics System for Small Aircraft Transportation System[C]// 25th Digital Avionics Systems Conference.2006 IEEE/ AIAA,2006:1-10.
  • 7[1]Collinson R P G.Fly-by-wire flight control[J].Computer & Control Englneering Journal,1999,12(12):141-153.
  • 8[2]Ahlstrom K,Torin J.Future architecture for flight control systems[C].IEEE 20th Digital Avionics Systems Conference,2001,1.B.5-1-5-10.
  • 9Suzuki,Hideto,et al.Space demonstration of a fault tolerant computer system using commercial MPU[J].Space Technology,2004,24(1):35-41
  • 10LIU Chung-Yu,A study of flight-critical computer system recovery from space radiation-induced error[J].IEEE Aerospace and Electronic Systems Magazine,2002,17(7):19-25

共引文献46

同被引文献43

引证文献11

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