A guide method of end segment self-adapt proportion-amending

摘要：

When the end segment of a whole proportion-guided ground-to-air missile is approaching an object, the guide head has entered its dizzy distance. The missile has set itself a near linear end segment collide course according to proportion guide rule. The method is based on two relationships. Through analysing the relationship between front direction excursion moving and meet gesture, the relationship between attack angle and front place angle can be acquired. Then the end segment self-adapt proportion-amending guide can be formed, which means that the ideal meet scattering center is the real part of the object and that the missile can attack the object effectively.

关键词： front direct excursion proportion guide amendment guide

作者: YAO Zhimin

作者单位: Department of Missile Engineering, Ordnance Engineering College, Shijiazhuang, Hebei 050003, China

会议类型: 国际会议

会议名称: 第七届国际测试技术研讨会

会议地点: 北京

会议语种:英文

在线出版日期: 2007-08-05（万方平台首次上网日期，不代表论文的发表时间）