| 有翼式战术地地导弹导引规律研究 |
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| 引用本文： | 郭宇春,戴宗礼,江涌.有翼式战术地地导弹导引规律研究[J].航天控制,1998,16(4):1-8. |
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| 作者姓名： | 郭宇春 戴宗礼 江涌 |
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| 作者单位： | 北京电子系统工程研究所,100854 |
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| 摘 要： | 导引规律的研究在导弹武器系统的设计中占有十分重要的地位。我国自行研制的某型有翼式近程战术地地导弹在使用现有导引规律时存在弹道确定性差的缺点。针对这一问题， 提出一种基于模糊逻辑系统的全程变导航比比例导引规律， 以平飞段模拟目标方法为辅助， 仿真计算表明取得了明显的改进效果， 具有较好的应用前景。
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| 关 键 词： | 模糊控制系统 地地导弹 导引规律 |
| 修稿时间： | 1998年7月7日 |
Study of Guidance Laws of Tactical Surface to Surface Missiles |
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| Guo Yunchun,Dai Zongli,Jiang Youg.Study of Guidance Laws of Tactical Surface to Surface Missiles[J].Aerospace Control,1998,16(4):1-8. |
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| Authors: | Guo Yunchun Dai Zongli Jiang Youg |
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| Institution: | Guo Yunchun Dai Zongli Jiang Youg Beijing Institute of Electronic System Engineering 100854 |
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| Abstract: | The study of guidance laws is very important in missile design. A kind of modified proportional streering guidance with variant navigation ratio in whole range based on fuzzy logic system is proposed in this article. Simulation computing results prove the guidance law is efficient and easy to be employed in future. |
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| Keywords: | Fuzzy control system Surface to surface missile Guidance law |
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