| 制导兵器飞行力学研究方向综述 |
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| 引用本文： | 袁子怀,钱杏芳.制导兵器飞行力学研究方向综述[J].飞行力学,1996,14(4):89-95. |
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| 作者姓名： | 袁子怀 钱杏芳 |
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| 作者单位： | 北京理工大学 |
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| 摘 要： | 介绍了国外制导兵器的发展概况，主要针对反坦克导弹，制导炮弹，末敏弹药，远程简易制导火箭和制导炸弹。并根据制导兵器发展的需要，提出了制导兵器飞行力学研究领域的一些主要研究方向。
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| 关 键 词： | 飞行力学 制导兵器 反坦克导弹 制导炮弹 火箭 |
A Comprehensive Review of Study Direction for Flight Dynamics of Guidance Weapons |
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| Yuan Zihuai,Qian Xingfang.A Comprehensive Review of Study Direction for Flight Dynamics of Guidance Weapons[J].Flight Dynamics,1996,14(4):89-95. |
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| Authors: | Yuan Zihuai Qian Xingfang |
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| Institution: | Beijing Institute of Technology |
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| Abstract: | This paper introduces the developing state of guidance weapons of abroad. It is including the antitank missile, cannon launched guidance projectile,terminally sensitivity munition, distant simple guidance rocket and guidance bomb. We according to the requirement of development for guidance weapon put forward some research directions. |
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| Keywords: | Flight dynamics Guidance weapon Antitank missile Guidance munition Guidance bomb Rocket |
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