期刊文献+

基于三种模型的航空电子设备结构设计分析

Structural Design Analysis of Avionics Equipment Based on Three Models
下载PDF
导出
摘要 通过分析总结航空电子设备结构设计面临的技术需求、结构设计技术发展各阶段的特点,提出下一阶段电子设备结构设计应在实体模型基础上做数据积累,进而提升有限元结构仿真准确度,综合运用理论模型、仿真模型和实物模型,提升结构设计水平。 Through analyzing and summarizing the technical requirements faced by the structural design of avionics equipment and the characteristics of each stage of structural technology development.It is proposed that in the next stage of structural design of avionics equipment,data should be accumulated on the accuracy of solid models,thus improving the accuracy of finite element structural simulation,comprehensively applying theoretical models and solid modes to improve the level of structural design.
作者 张丰华 田沣 刘治虎 李雪龙 ZHANG Feng-hua;TIAN Feng;LIU Zhi-hu;LI Xue-long(Xi′an Aeronautics Computing Technique Research Institute,AVIC,Xi′an 710068,China)
出处 《航空计算技术》 2020年第2期79-81,共3页 Aeronautical Computing Technique
基金 国家科技重大专项基金项目资助(2017-V-0014-0066)。
关键词 模型 电子设备 结构设计 model avionics equipment structural design
  • 相关文献

参考文献7

二级参考文献44

  • 1何志强.综合化航空电子系统发展历程及重要支撑技术[J].电讯技术,2004,44(4):1-5. 被引量:46
  • 2周代忠,张安,史志富.微电子技术在航空电子系统中的应用[J].电光与控制,2005,12(4):40-43. 被引量:8
  • 3柳超.高可靠军用电子产品可靠性评估方法[J].四川兵工学报,2006,27(6):64-66. 被引量:2
  • 4LIN Qiang XIONG Hua-gang ZHANG Qi-shan.Credit Determination of Fibre Channel in Avionics Environment[J].Chinese Journal of Aeronautics,2007,20(3):247-252. 被引量:4
  • 5Prisaznuk P J. Integrated modular avionics[C]//Aerospace and Electronics Conference, 1992: 39-45.
  • 6Watkins C B, Walter R. Transitioning from federated avi- onics architectures to integrated modular avionics [C]// Proceedings of IEEE the 26th Digital Avionics Systems Conference, 2007: 2. A. 1-1-2. A. 1-10.
  • 7Di N M, Sangiovanni-Vincentelli A L. Moving from feder- ated to integrated architectures in automotive: the role of standards, methods and tools automotive electronics sys- tems need to support an increasing number of features and functions. A new integrated architecture paradigm is nee- ded to overcome the proliferation of electronic control units (ECUs) and allow integration of software components on distributed platforms [J]. Proceedings of the IEEE, 2010,98(4) : 603-620.
  • 8Li X Y, Xiong H G. Modelling and simulation of integrat- ed modular avionics systems[C]//IEEE/AIAA 28th Digit- al Avionics Systems Conference, 2009: 7B3-1-7B3-8.
  • 9Wang G Q. Integration technology for avionics system[C]// IEEE/AIAA 31st Digital Avionics Systems Conference, 2012 : 7C6-1-7C6-9.
  • 10Nesrine B, Katia J, Jean L S, et al. End-to-end delay analysis in an integrated modular avionics architecture[C]// IEEE 18th Conference on Emerging Technologies & Fac- tory Automation (ETFA), 2013 : 1-4.

共引文献96

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