Detonating control method based on missile-target relative attitude for accurate hit of oriented damage elements

摘要：

　　According to the characteristics of the missile and target rendezvous while the warhead scatters narrowly, the rendezvous model including three relative attitude angles is proposed.In some case,the model can be simplified.Taking it as the background that cruising missiles attack ground armor targets, the relative attitude is introduced into the analysis of the missile and target rendezvous.The impact factors of the hit precision is decoupled and discussed.Based on the analysis mentioned above, optimization algorithms of detonating time and guide point are proposed, and the results of Monte Carlo simulation show that the hit precisions significantly increase.Finally, the objective function of optimal damage is built.

关键词： Accurate hit Relative attitude Detonating control Optimal damage

作者: Yu-hang HE Yan-xuan WU Zheng-jie WANG Jing-ru HAN

作者单位: College of mechanical and electrical engineering, Beijing Institute of Technology, Beijing, 100081,China

会议类型: 国际会议

会议名称: 2018 International Conference on Defence Technology (2018国际防务技术会议)

会议地点: 北京

会议语种:英文

页码: 990-994

在线出版日期: 2018-10-21（万方平台首次上网日期，不代表论文的发表时间）