| BTT导弹的新型三维非线性寻的制导律 |
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| 引用本文： | 李君龙,江涌.BTT导弹的新型三维非线性寻的制导律[J].现代防御技术,2000,28(1):42-46. |
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| 作者姓名： | 李君龙 江涌 |
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| 作者单位： | 中国航天机电集团二院二部,北京,100854 |
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| 摘 要： | 建立了导弹与目标的三维相对运动模型，分析了目前寻的制导律的一些局限性，提出了新型非线性寻的制导律。在更复杂的交战环境中，将此制导律用于高性能的ＢＴＴ导弹，可望提高制导精度
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| 关 键 词： | 寻的制导 相对阶 碰撞线 拦截 末制导 |
| 修稿时间： | 1999-04-08 |
New Three-Dimensional Nonlinear Homing Guidance Law for BTT Missile |
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| LI Jun-long,JIANG Yong.New Three-Dimensional Nonlinear Homing Guidance Law for BTT Missile[J].Modern Defence Technology,2000,28(1):42-46. |
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| Authors: | LI Jun-long JIANG Yong |
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| Abstract: | Three dimensional relative motion model of missile and target is established in the paper Some limitation in today's most homing guidance laws are analyzed In order to overcome the drawback of the linearization near collision course,nonlinear homing guidance law is derived It is suited to high performance BTT missile in more complex combat enviroment and the guidance precision is greatly enhanced |
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| Keywords: | Homing guidance Relative degree\ Collision course\ Interception Terminal guidance |
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