仿形轻诱饵空间定姿初探  

Profile Modeling Light Decoy Spatial Attitude Control Design

作　　者：陈方予[1] 赵蕾[1] 张其刚[1] 李明[1] 

机构地区：[1]中国航天科工集团公司南京8511所,江苏南京210007

出　　处：《现代防御技术》2010年第4期83-87,共5页Modern Defence Technology

摘　　要：注意到目前反导武器逐渐使用图像区分真假目标的发展状况,阐述了对于远程BM使用仿形轻诱饵进行突防是一个很好的方法。探讨了研制仿形轻诱饵可能涉及的几项关键技术,借鉴卫星姿态稳控技术,初步探讨了南北飞行的轻诱饵使用磁强计和磁力矩器利用地磁场定姿的可行性,并分析了其局限性。最后说明了这种方法对于南北飞行的诱饵,在BM弹头可调姿的情况下,是可以与弹头姿态保持一致的。The development trend that current anti tactical ballistic missile （ATBM） distinguishes warhead from decoys by means of image characters is observed. Long distance ballistic missile （BM） penetration by using profile modeling light decoy is a useful method. Several key techniques of designing profile modeling is analyzed. Consulting spacecraft attitude control technology, a decoy flying along south and north direction is studied to control attitude itself by means of using magnetometers and magnetic roads as well as geomagnetic field and then the feasibility and weakness of this method are analyzed. Lastly, the author points out that this method is available for the decoy flying along south and north direction to keep the same attitude as the warhead in the condition that warhead can adjusts its attitude.

关 键 词：仿形轻诱饵 空间 定姿 

分 类 号：TN972.4[电子电信—信号与信息处理] TJ761.3[电子电信—信息与通信工程]