高超声速精确打击武器制导控制关键技术  

Key Technologies of Guidance and Control for Hypersonic Precise Strike Weapon

作　　者：柳青 朱坤[2] 赵欣 Liu Qing;Zhu Kun;Zhao Xin(Beijing Aerospace.Technology Institute,Beijing 100074,China;HIWING Technology Academy of CASIC,Beijing 100074,China)

机构地区：[1]北京空天技术研究所,北京100074 [2]中国航天科工飞航技术研究院,北京100074

出　　处：《战术导弹技术》2018年第6期63-69,共7页Tactical Missile Technology

摘　　要：首先分析了以超燃冲压发动机为动力的高超声速巡航导弹的主要技术特点,介绍了高超声速巡航导弹的国外发展现状;在此基础上,着重探讨和分析了高超声速巡航导弹动力学建模、飞行控制、制导体制选择及导引律设计、高动态雷达精确制导和高温高速光电制导五个方面的关键技术特点和后续应重点关注的技术发展途径,为高超声速精确打击武器制导控制技术研究提供一定的参考。The main technical features and the recent deployment of hypersonic cruise missile which is powered by scramjet is firstly introduced. And on this basis,the key problems and current difficulties of guidance and control are analyzed from the aspects of dynamic modeling,flight control,guidance structure selection and guidance law design,high dynamic radar guidance,photoelectric guidance at high temperature and high speed. At last,combined with the technical difficulties which is faced by hypersonic precise strike weapon,the guidance and control technology follow-up development directions are given.Some references will be provided for the research of guidance and control technology of hypersonic precise strike weapon.

关 键 词：高超声速 精确打击 制导控制 巡航导弹 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]