| 寻的制导控制系统设计方法探讨 |
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| 引用本文： | 魏明英.寻的制导控制系统设计方法探讨[J].现代防御技术,2001,29(5):42-45. |
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| 作者姓名： | 魏明英 |
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| 作者单位： | 中国航天机电集团公司二院二部, |
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| 摘 要： | 对使用寻的体制探测目标的防空导弹制导控制系统设计方法进行了分析、探讨.设计中主要考虑了天线罩折射误差及去耦系数、有效导航比、稳定回路时间常数、气动力时间常数和遮挡效应的影响;对于低空制导控制系统主要考虑了多路径(镜像干扰)的影响,对布鲁斯特角效应抑制多路径(镜像干扰)的影响进行了分析.
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| 关 键 词： | 制导控制系统 多路径效应+ 天线罩折射误差 遮挡效应+ |
| 文章编号： | 1009-086(2001)05-0042-04 |
| 修稿时间： | 2000年12月25 |
Design Technique Discussion of Seeking Guidance System |
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| WEI Ming,ying.Design Technique Discussion of Seeking Guidance System[J].Modern Defence Technology,2001,29(5):42-45. |
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| Authors: | WEI Ming ying |
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| Abstract: | This paper analyzes and discusses the design technique for guidance and control system of air defense missile using seeking guidance system. Influence of radome refraction error and decoupling parameters, effective navigation ratio, stabilization loop time constant, pneumatic time constant and eclipsing effect are considered during the design process. For low altitude guidance and control system, effects of multipath (mirror interference) are mainly pondered on and using Brewster angle effect to restrain effects of multipath is analyzed. |
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| Keywords: | Guidance and control system Multipath effect Radome refraction error Eclipsing effect |
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