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导弹武器全制导技术发展分析
引用本文:赵晶,来庆福,戴幻尧,冯德军,王雪松. 导弹武器全制导技术发展分析[J]. 中国电子科学研究院学报, 2012, 7(1): 34-41
作者姓名:赵晶  来庆福  戴幻尧  冯德军  王雪松
作者单位:国防科技大学电子科学与工程学院,长沙湖南,410073
基金项目:国家自然科学基金,总装预研项目,国防科技大学研究生创新资助
摘    要:面向反舰、对地攻击和反辐射等典型精确制导武器作战的现实需求,探讨了以高精度惯导信息获取与利用为核心的导弹武器全制导技术的新概念、方法和应用,构建出导弹武器全制导技术仿真验证半实物仿真系统,进行了反舰巡航导弹全弹道飞行等仿真评估实验,充分地验证了该方案的可行性与有效性。全制导技术方案着眼于制导方式、信息融合和信号处理上的完善与改进,可为提高我军精确制导武器在复杂环境下的作战能力提供可行的技术实现途径,同时可为新一代精确制导武器的研制提供必要的技术储备。

关 键 词:惯性导航系统  导引头  信息融合  导弹制导控制  复合制导

Technology Development of Full Guidance Technique in Missile Weapon
ZHAO Jing,LAI Qing-fu,DAI Huan-yao,FENG De-jun,WANG Xue-song. Technology Development of Full Guidance Technique in Missile Weapon[J]. Journal of China Academy of Electronics and Information Technology, 2012, 7(1): 34-41
Authors:ZHAO Jing  LAI Qing-fu  DAI Huan-yao  FENG De-jun  WANG Xue-song
Affiliation:(School of Electronic Science and Engineering,National University of Defense Technology,Changsha Hunan 410073,China)
Abstract:Full guidance technique(FGT) in missile weapon,based on the acquisition and application of high precision inertial navigation information,is introduced for the exigent demands of precision striking warfare in anti-ship,land-attacking and anti-radiation.The novel concepts,methods and applications are elaborated to construct a hardware-in-the-loop simulation and visualization system in adding of inertial ap-paratus.A representative scenario simulation,whole trace flying of an anti-ship cruise missile,is carried out to fully demonstrate the feasibility and validity of FGT.The exploitation and advancement of current missile guidance,sensor fusion and signal processing techniques,as the core of FGT,would provide a vi-able approach to enhance the performance of missile weapons under complicated environment,as well as offer some useful suggestions for future precision striking development.
Keywords:inertial navigation system  seeker  information fusion  missile guidance and control  com- posite guidance
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