| 松耦合分布式技术在飞参系统设计中应用与发展 |
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| 引用本文： | 吕锁宁,桑龙,董进武,李国柱.松耦合分布式技术在飞参系统设计中应用与发展[J].海军航空工程学院学报,2007,22(1):129-132. |
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| 作者姓名： | 吕锁宁 桑龙 董进武 李国柱 |
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| 作者单位： | 海军驻汉中地区航空军事代表室,陕西汉中,723213 |
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| 摘 要： | 分析了计算机系统设计思路与系统结构的发展趋势,进而对如何建立高性能的飞行参数记录系统结构进行了研究,并对采用这一结构模型的飞参系统的未来发展提出了几点看法。
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| 关 键 词： | 计算机系统 多处理机 松耦合 飞参系统 软件可靠性 |
| 修稿时间： | 2006年3月16日 |
Application and development of decoupling,structure distribution in design of FDR system |
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| LV Suoning,SANG Long,DONG Jinwu and LI Guozhu.Application and development of decoupling,structure distribution in design of FDR system[J].Journal of Naval Aeronautical Engineering Institute,2007,22(1):129-132. |
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| Authors: | LV Suoning SANG Long DONG Jinwu and LI Guozhu |
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| Institution: | Aeronautical Military Representatives Office of Navy in Hanzhong,Hanzhong,Shanxi,723213,Aeronautical Military Representatives Office of Navy in Hanzhong,Hanzhong,Shanxi,723213,Aeronautical Military Representatives Office of Navy in Hanzhong,Hanzhong,Shanxi,723213 and Aeronautical Military Representatives Office of Navy in Hanzhong,Hanzhong,Shanxi,723213 |
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| Abstract: | The design method of the computer system and development trend of the system structure is analyzed. Further how to build high performance of flight recording system structure is studied, and some viewpoints on the future development of flight parameter system based on this structure are put forward. |
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| Keywords: | computer system multi-processor decoupling FDR system reliability of software |
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