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航天测试发射C4I系统设计
引用本文:毛永军,蒋志文.航天测试发射C4I系统设计[J].航天控制,2004,22(6):41-45.
作者姓名:毛永军  蒋志文
作者单位:1. 国防科技大学计算机学院,长沙,410073;国防科技大学计算机学院,长沙,410073
2. 国防科技大学计算机学院,长沙,410073
摘    要:通过分析航天测试发射活动的独特性质和组织指挥模式,提出了航天测试发射C4I系统的一般体系结构,研究了进行系统设计的关键技术及解决方案,并以载人航天工程C4I系统为例介绍了一个具体的航天测试发射C4I系统框架,最后对未来航天测试发射C4I系统的发展方向进行了探索.

关 键 词:航天测试发射  C4I系统  指挥决策
文章编号:1006-3242(2004)06-0041-05
修稿时间:2004年4月16日

Aerospace Test and Launch C4I System Design
Mao Yongjun , Jiang Zhiwen .Computer College of National University of Defense Technology,Changsha .Jiuquan Satellite Launch Center of China,Lanzhou.Aerospace Test and Launch C4I System Design[J].Aerospace Control,2004,22(6):41-45.
Authors:Mao Yongjun  Jiang Zhiwen Computer College of National University of Defense Technology  Changsha Jiuquan Satellite Launch Center of China  Lanzhou
Institution:Mao Yongjun 1,2 Jiang Zhiwen 11.Computer College of National University of Defense Technology,Changsha 410073 2.Jiuquan Satellite Launch Center of China,Lanzhou 732750
Abstract:In this paper, based on the analysis of the unique features and the commanding mode of aerospace test and launch, the systematic architecture of aerospace test and launch C 4I system is presented, and the key technology and solution for architecture design are studied. Then taking manned aerospace project as an example, an outline of aerospace test and launch C 4I system is presented.The development of future research for aerospace test and launch C 4I system is discussed in the end.
Keywords:Aerospace test and launch C  4I system Command and decision-making  
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