| 飞航导弹导引头系统与控制系统抗干扰通讯设计 |
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| 引用本文： | 裴虎城.飞航导弹导引头系统与控制系统抗干扰通讯设计[J].战术导弹技术,2004(1):59-63. |
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| 作者姓名： | 裴虎城 |
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| 作者单位： | 中国航天科工集团公司第三研究院,北京100074 |
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| 摘 要： | 抗干扰通讯设计是数字通讯中一个重要的问题, 也是较容易忽视的问题.介绍了数据通讯中基本抗干扰编码和差错控制原理, 并对飞航导弹导引头系统与控制系统数据通讯中的特有情况进行了分析, 然后对其抗干扰通讯进行了设计.
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| 关 键 词： | 导引系统 抗干扰 通讯 |
| 文章编号： | 1009-1300(2004)01-0059-05 |
| 修稿时间： | 2003年6月10日 |
Anti-jamming Communication Design of Guidance System and Control System in Winged Missile |
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| Pei Hucheng.Anti-jamming Communication Design of Guidance System and Control System in Winged Missile[J].Tactical Missile Technology,2004(1):59-63. |
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| Authors: | Pei Hucheng |
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| Abstract: | Since most of the winged missile work under a complicated hostile environment,its communication parts are apt to be interfered and the reliability of communication can't be assured.The theory of mistake control and the basic anti-jamming code in digital communication are introduced.The specific feature of digital communication in the guidance system and control system of winged missile is analysed,and then its anti-jamming communication is designed. |
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| Keywords: | guidance system anti-jamming communication |
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