期刊文献+

基于改进故障模型的CAN总线调度分析 被引量:2

A Scheduling Analysis of CAN Based on an Improved Fault Model and Its Application in Missile Control System
在线阅读 下载PDF
导出
摘要 鉴于数据传输总线的诸多优点,建立总线式体制是现代导弹控制系统互联方式发展的必然趋势。CAN总线是一种设计优良的总线,但缺点在于其事件驱动型的协议导致无法建立CAN总线的可靠调度策略。Tindell给出的基于最小间隔故障模型的WCRT调度分析方法在强干扰环境中会导致乐观偏差,因此需要建立一种CAN总线在复杂环境中的更加准确的调度分析方法以指导可靠的系统设计。基于此目的,给出了一种基于广义泊松过程的改进故障模型,并在此基础上建立了CAN总线消息的调度分析。最后将该调度分析应用于导弹控制系统,并分析了对总线调度能力构成影响的因素。 Due to the advantages of data transmission bus, the bus-based framework is the trend of the interconnecting method of modern missile control system. CAN is a well-designed bus, whose defect lies in its event-driven communication protocol that brings great difficulties in finding a reliable scheduling scheme for CAN. The previous scheduling analysis of CAN presented by Tindell based on minimal-interval fault model, will lead to optimistic error especially in case of strong interference. So it is essential to establish a more accurate scheduling analysis of CAN under complex environment to guide the reliable design of control system. Based on this aim, an improved fault model based on generalized Poisson process is presented, and a new scheduling analysis of CAN based on it is established. In the end, this analysis is applied to a CAN based missile control system, and the factors relative to the bus scheduling are analyzed.
出处 《电光与控制》 北大核心 2010年第3期93-97,共5页 Electronics Optics & Control
关键词 导弹控制系统 CAN总线 调度分析 泊松过程 故障模型 失败概率 missile control system CAN bus scheduling analysis Poisson process fault model failure probability
  • 相关文献

参考文献10

二级参考文献22

共引文献23

同被引文献18

  • 1邹方,薛汉杰,周万勇,许国康.飞机数字化柔性装配关键技术及其发展[J].航空制造技术,2006,49(9):30-35. 被引量:60
  • 2佟为明,陈培友,高洪伟,钱英军.CAN总线位定时与同步机制的研究[J].电子器件,2007,30(4):1499-1502. 被引量:10
  • 3Atmel Corporation. Rad-hard 32ibt SPARC embedded processor TSC695F[ Z]. DATA Sheet,2003.
  • 4Philips Semiconductors. PCA82C250 CAN controller in- terface [ Z ]. PHILIPS DATA Sheet,2000.
  • 5JOHNK E, DIETMAYER K. Application note determina- tion of bit timing parameters for SJA1000 CAN controller [ Z ]. AN97046, Philips Semiconductors, 1997.
  • 6HARTMANN J, MEEKER C, WEIIER M, et al. Determinate asssembly of tooling allows concurrent design of airbus wings and major as-sembly fixtures [ R ]. SAE Paper 2004-01- 2832,2004.
  • 7CORBE~ J, NAING S . Feature based design for jiglessassembly [ D ]. Bedfordshire, UK: Cranfield University, 2004.
  • 8倍福电气有限公司.TwinCAT PLC编程手册[M].2005.
  • 9Beckhoff G. EtherCAT : The Ethemet fieldhus [ Z ]. Ether- CAT Technology Group, 2006.
  • 10冯仪,黄树槐.基于S7-200可能量预选的摩擦压力机数控系统[J].华中科技大学学报(自然科学版),2008,36(9):79-82. 被引量:8

引证文献2

二级引证文献3

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