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凝视红外成像末制导系统应用研究
引用本文:费锦东,刘鹏.凝视红外成像末制导系统应用研究[J].红外与激光工程,2006,35(3):253-257.
作者姓名:费锦东  刘鹏
作者单位:中国航天科工集团公司二院二部,北京,100854
摘    要:根据国外新一代防空导弹的发展趋势,进行了高速导弹末制导系统气动热、气动热辐射和高速流场对目标传输效应等工作环境的初步计算,为高速导弹应用红外末制导系统提供了设计依据.结合高速导弹末制导系统要求和所处的工作环境,分析了红外成像末制导在高速导弹上应用的系统技术问题.最后,提出了应用数学仿真、半实物仿真和外场试验等进行红外成像末制导系统性能评估的方法.

关 键 词:精确制导  红外成像  高速导弹  气动光学
文章编号:1007-2276(2006)03-0253-05
收稿时间:2005-08-02
修稿时间:2005-09-20

System application of staring infrared imaging terminal guidance
FEI Jin-dong,LIU Peng.System application of staring infrared imaging terminal guidance[J].Infrared and Laser Engineering,2006,35(3):253-257.
Authors:FEI Jin-dong  LIU Peng
Affiliation:Second System Design Department of the Second Research Academy of CASIC, Beijing 100854, China
Abstract:According to the development trend of new-style antiaircraft missile, preliminary calculation was done for aero heat effect, aero heat radiation and optical transmission effect of high speed flow field, which can be used as a basis in the design and analysis of high velocity missile terminal guidance system. System technology of infrared imaging terminal guidance used in high velocity missile was studied in combination with application requirements and working environment for high velocity missile terminal guidance system. The approach for evaluating performance of infrared imaging terminal guidance system was put forward using mathematical simulation, semi-physical simulation and field investigation.
Keywords:Precise guidance  Infrared imaging  High velocity missile  Aero optics
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