| 末制导中的全向攻击原理 |
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| 引用本文： | 姜玉宪.末制导中的全向攻击原理[J].北京航空航天大学学报,1989(3):87-95. |
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| 作者姓名： | 姜玉宪 |
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| 作者单位： | 北京航空航天大学自动控制系 |
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| 摘 要： | 本文提出一种能够实现导弹对活动目标全方位攻击的基本原理,并讨论了工程上实现的途径。通过平面及空间导引弹道仿真,初步证明了它的正确性及可实现性。
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| 关 键 词： | 末制导 全向攻击 导弹 制导 |
PRINCIPLE OF ALL AZIMUTHS ATTACK IN TERMINAL GUIDANCE |
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| Jiang Yuxian.PRINCIPLE OF ALL AZIMUTHS ATTACK IN TERMINAL GUIDANCE[J].Journal of Beijing University of Aeronautics and Astronautics,1989(3):87-95. |
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| Authors: | Jiang Yuxian |
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| Institution: | Department of Automatic Control |
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| Abstract: | This paper presents a thcory which can make missiles attack moving targets in all azimuths and discusses the way of putting it in engineering prentice.The validity and reality of this theory arc primtryly demonstrate 1 by the simulation of guidance trajectories of missiles. |
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| Keywords: | terminal guidance all aspects attack guidance system optimal guidance law trajectory simulation |
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