| 动力滑翔导弹弹道设计 |
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| 引用本文： | 郭飞帅,刘冬,张高瑜.动力滑翔导弹弹道设计[J].四川兵工学报,2011,32(7):36-39. |
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| 作者姓名： | 郭飞帅 刘冬 张高瑜 |
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| 作者单位： | 第二炮兵工程学院,西安,710025 |
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| 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。
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| 关 键 词： | 动力滑翔导弹 弹道设计 水平推力 |
Design and Research on Trajectory of Dynamic-Glider Missile |
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| Authors: | GUO Fei-shuai LIU Dong ZHANG Gao-yu |
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| Affiliation: | (603 Staff Room,Second Artillery Engineering College,Xian 710025,China) |
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| Abstract: | 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 |
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| Keywords: | dynamic-glider missile trajectory design horizontal thrust |
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