电视制导导弹末制导段的弹道仿真研究  

Research on the Last-Stage Guidance Trajectory Simulation of the TV-guided Missile

作　　者：国海峰[1] 刘泽乾[1] 

机构地区：[1]空军航空大学,吉林长春130022

出　　处：《科技情报开发与经济》2009年第26期136-138,共3页Sci-Tech Information Development & Economy

摘　　要：根据电视制导导弹末制导现有的几种制导规律介绍了其基本原理,对比例导引法和组合制导法进行了弹道仿真,分析了比例系数和初始目标线角对弹道和击中目标时间的影响。Based on several existing guidance laws of the terminal guidance of TV -guided missile, this paper introduces its basic principles, and using Matlab to make the guidance trajectory simulation of the proportional guidance and the combined guidance, and analyzes the influences of the of the proportional coefficient and the original target line-angle on the guidance trajectory and the time of hitting the target.

关 键 词：末制导 制导规律 弹道仿真 比例导引法 组合制导法 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]