动力滑翔导弹弹道设计  

Design and Research on Trajectory of Dynamic-Glider Missile

作　　者：郭飞帅[1] 刘冬[1] 张高瑜[1] 

机构地区：[1]第二炮兵工程学院,西安710025

出　　处：《四川兵工学报》2011年第7期36-39,共4页Journal of Sichuan Ordnance

摘　　要：研究了在滑翔弹道的波峰加载水平推力对射程的影响问题。针对动力滑翔导弹建立其弹道运动模型,利用M atlab对其进行仿真。结果表明,加载动力后导弹射程增益明显。Glide missile is now the new missile that all countries are researching on,and loading power in the process of gliding can add even more range and penetration of missiles.This article is to study effects on range of missiles when loading power on the peak of trajectory.Trajectory design plays a very important role overall design of the missile,in this paper it has established its trajectory motion model of dynamic-glider missile and simulated its trajectory using MATLAB software.The results show that the missile has significantly a range gain after loading power.

关 键 词：动力滑翔导弹 弹道设计 水平推力 

分 类 号：TJ76[兵器科学与技术—武器系统与运用工程]