摘要
采用一种INS/GPS组合导航系统与引信导引头的信息融合技术 ,来控制导弹的飞行与起爆。从信息融合角度出发 ,利用引信导引头信息与导航信息的融合、分散化滤波技术 ,提供一种准确、及时。
In this paper, an information mixed-technology of the INS/GPS united guide navigation system and the fuse guide head is adopted to control the fly and detonation of the missile. On the basis of the information mixed-technology, an accurate, timely and effective design plan is put forward by means of the mixture and scatter filter technology of the fuse guide head information and the guide navigation information.
出处
《陕西工学院学报》
2002年第1期15-18,共4页
Journal of Shaanxi Institute of Technology
关键词
信息融合
引制一体化
设计
组合导航技术
航空
航天
mixture of information
the united guided navigation technology
the integration of fuse and control
