J4 ›› 2011, Vol. 38 ›› Issue (6): 140-145.doi: 10.3969/j.issn.1001-2400.2011.06.023

• 研究论文 • 上一篇    下一篇

ARINC 659容错数据总线测试验证系统研制


  1. (1. 中国航空工业计算技术研究所,陕西 西安  710068;
    2. 西安电子科技大学 多媒体技术研究所,陕西 西安  710071)
  • 收稿日期:2010-08-22 出版日期:2011-12-20 发布日期:2011-11-29
  • 通讯作者: 张喜民
  • 作者简介:张喜民(1973-),男,副教授,博士,E-mail: zczya@sohu.com
  • 基金资助:


Research on the test and verification system of the ARINC 659 fault-tolerant backplane data bus

ZHANG Ximin1,2;WEI Ting1

  1. (1. Aeronautics Computing Technique Research Institute, Xi'an  710068, China;
    2. Research Inst. of Multimedia Technology, Xidian Univ., Xi'an  710071, China)
  • Received:2010-08-22 Online:2011-12-20 Published:2011-11-29
  • Contact: ZHANG Ximin


研制了具有自主知识产权的自带微处理器的ARINC 659总线接口芯片,开发了接口芯片内微处理器的帧描述语言编译器;设计开发了总线接口板、通信试验台等,构建了总线通信测试验证系统.按ARINC 659总线规范要求对各实现功能进行了软、硬件联合调试和测试,测试结果验证了接口芯片、通信测试验证系统功能的正确性和完整性.研究成果已用于某些航空安全关键系统,提高了系统的可靠性,降低了全寿命周期费用.

关键词: ARINC 659, 容错, 背板数据总线, 接口芯片设计, 测试环境, 功能验证


The ARINC 659 data bus is a high reliability and high-integrity avionic standard backplane bus designed to provide fault tolerance and robustness partition in time and memory space. It is a key component of the integrated modular avionics system. The ARINC 659 data bus is the property key technique of the Honeywell Company, and it places a stick embargo on the correlative productions for other companies especially for our country. In this paper, the independent innovative ARINC 659 data bus interface ASIC, which has a special microprocessor, and its Frame Description Language compiler are developed. The design and realization of the communication test platform are presented, which consists of the three complements: the ARINC 659 data bus interface card, the communication node controller and the communication test-bed of the data bus. The debug and test configurations of the hardware and software are explored. The methods are given to test and verify the function under the test environment according to the ARINC 659 Specification, and the result shows the correctness and integrity of the design. The research has been applied in the avionic safe critical systems, and the systems benefit from it with higher reliability and lower LLC.

Key words: ARINC 659, fault-tolerance, backplane data bus, interface chip design, test environment, function verification