| 弹载中制导计算机设计方法研究 |
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| 引用本文： | 张伟,周莹.弹载中制导计算机设计方法研究[J].航空计算技术,2009,39(1):123-127. |
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| 作者姓名： | 张伟 周莹 |
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| 作者单位： | 空军工程大学,导弹学院,陕西,三原,713800 |
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| 摘 要： | 弹载中制导计算机是弹载中制导系统的核心部件，从弹载计算机体系结构和主要技术两个方面对弹载中制导计算机的设计方法进行了初步研究。结合导弹制导体制和制导系统配置模式对弹载中制导计算机体系结构进行了总结、归类，并从处理器、存储器选型、总线技术、电源设计等几个方面讨论了弹载计算机的主要设计方法。最后给出了一个弹载制导一体化计算机设计的工程实例。
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| 关 键 词： | 弹载中制导计算机 体系结构 |
Research on Design Method of Missile-borne Guidance Computer |
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| ZHANG Wei,ZHOU Ying.Research on Design Method of Missile-borne Guidance Computer[J].Aeronautical Computer Technique,2009,39(1):123-127. |
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| Authors: | ZHANG Wei ZHOU Ying |
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| Institution: | Missile Institute;Air Force Engineering University;Sanyuan 713800;China |
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| Abstract: | Missile-borne guidance computer is the core component of missile-borne guidance system.Design method of missile-borne guidance computer has been researched in two aspects-system structure and main technology in this paper.induction and summarization of missile-borne guidance computer system structure has been proposed by combined with missile guidance system and allocation model of guidance system.Main design method of missile-borne guidance computer has been explained from aspects of CPU and memory selecti... |
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| Keywords: | missile-borne guidance computer system structure |
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