Computer Science ›› 2015, Vol. 42 ›› Issue (5): 10-13.doi: 10.11896/j.issn.1002-137X.2015.05.002

Previous Articles     Next Articles

Aerospace Embedded Computer Architecture Evaluation Model

HAN Wei, BAI Xiao-ying and XIE Jian-chun   

  • Online:2018-11-14 Published:2018-11-14

Abstract: Typical aerospace embedded computers have many characters in common,especially in the aspect of the design of computer architecture.Three typical aerospace embedded computers were sampled and their characters of architecture and common technology were analyzed.These samples are flight control computer,guidance control computer and satellite borne computer.Seven characters of architecture were concluded.They are modular,network centric,integration,intensivism,longevity,application of commercial off the shelf(COTS) and system openness.As a result,3 eva-luation dimensions were proposed:common architecture,cost control and development oriented,which contribute to the final score of the system under test directly.All the architecture characters and evaluation dimensionalities mentioned above form the evaluation model for aerospace embedded computers.Each architecture character has a basic guideline and a practical reference value or design.Based on the relationship of the classification of the final evaluation result,the evaluation dimensions and the architecture characters,any aerospace embedded computer can be scored according to the evaluation model for various estimate requirements.The evaluating method and progress were illustrated through two kinds of advanced aerospace embedded computers’ evaluation case.The cases indicate that the evaluation model is clear,effective and practical.

Key words: Evaluation model,Avionic architecture,Aerospace,Embedded computer,Modularization

[1] 张凤鸣,褚文奎,樊晓光,等.综合模块化航空电子体系结构研究[J].电光与控制,2009,16(9):47-51
[2] 崔西宁,胡林平,叶宏,等.综合化航空电子系统软件接口研究[J].计算机科学,2011,38(2):122-126
[3] 蒋彭龙.片上系统技术在航天领域的发展和应用[J].导弹与航天运载技术,2010,5:17-19
[4] Jakovijevic M.Modular Open System Approach(Mosa) and Ttp-Based Platforms for Aerospace Control Systems[C]∥Procee-ding of 25th Digital Avionics Systems Conference.2006:1-6
[5] 黄永葵,吴建民,谷涛,等.SAE AS4893《通用开放式结构(GOA)框架》评析[J].航空计算技术,2007,38(1):40-46
[6] 牛文生.机载计算机技术[M].西安:航空工业出版社,2013
[7] 谢燕武.飞航导弹一体化制导控制系统[J].兵工自动化,2012,1(11):38-40
[8] 冶元菲,吕楠,黄献龙,等.先进电子信息系统在通信卫星平台中的应用[J].空间控制技术与应用,2011,7(1):45-49
[9] 林长苓,周军连,聂国健.COTS元器件在舰载装备中的可靠性风险分析[J].电子产品可靠性与环境试验,2006,24(6):37-41
[10] 崔昆涛,孙文力,孙文强.模块化开放式系统架构设计、原理研究[J].信息系统工程,2013(5):35-37
[11] 刘士全,隽扬,蔡洁明,等.1553B总线应用发展研究[J].电子与封装,2013,3(12):11-15
[12] 孔德岐,李亚辉,郭鹏.高可靠嵌入式计算机系统的发展[J].通信学报,2013,34(Z1):170-175
[13] 邢克飞,何伟,杨俊.COTS 器件的空间应用技术研究[J].计算机测量与控制,2011,19(7):1741-1745
[14] 王猛,宁滨,马连川.基于COTS的安全计算机系统[J].铁道通信信号,2007,3(3):56-58
[15] 罗巧云.美军F-22的先进航空电子系统[J].电讯技术,2006,46(6):7-12
[16] Luo Rui,LI Guo-zhu.Development of the F-35 Avionics System[J].Ship Electronic Engineering,2012,32(8):21-23

No related articles found!
Viewed
Full text


Abstract

Cited

  Shared   
  Discussed   
No Suggested Reading articles found!