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再入飞行器攻击慢速活动目标的制导方案研究

Study for the Guidance Scheme of Reentry Vehicles Attacking slowly Moving Targets

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【作者】 陈海东余梦伦辛万青李军辉曾庆湘

【Author】 Chen Haidong Yu Menglun Xin Wanqing Li Junhui(Beijing Institute of Astronautical Systems Engineering, Beijing, 100076) Zeng Qingxiang(Beijing Institute of Special Mechanical and Electronic Devices, Beijing,100076)

【机构】 北京宇航系统工程设计部!北京100076北京特种机电研究所!北京

【摘要】 研究了再入飞行器攻击海上慢速活动目标的制导方案。首先介绍了目标的初始侦察定位系统 ;然后对再入飞行器攻击活动目标可以采用的导引头以及高空探测系统进行了分析 ;最后对再入飞行器降弧段的制导规律进行了研究。针对目标的最大逃逸范围 ,提出了高低空复合制导方案 ,仿真结果表明方案是可行的

【Abstract】 In this paper, the guidance scheme of reentry vehicles attacking slowly moving targets on the sea is studied. First, initial reconnaissance and location systems for targets are introduced; then, the target seeker and high altitude detector which can be used on reentry vehicles to attack the moving target are analyzed; finally, a guidance law in downward phase of reentry vehicles is studied. By considering the largest escape range of the target, a compound guidance scheme in high low altitude is presented. The trajectory simulation shows the feasibility of this scheme.

  • 【文献出处】 导弹与航天运载技术 ,Missiles and Space Vehicles , 编辑部邮箱 ,2000年06期
  • 【分类号】V448
  • 【被引频次】1
  • 【下载频次】386
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