| 电视制导导弹末制导段的弹道仿真研究 |
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| 引用本文： | 国海峰,刘泽乾. 电视制导导弹末制导段的弹道仿真研究[J]. 科技情报开发与经济, 2009, 19(26): 136-138 |
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| 作者姓名： | 国海峰 刘泽乾 |
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| 作者单位： | 空军航空大学; |
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| 摘 要： | 根据电视制导导弹末制导现有的几种制导规律介绍了其基本原理,对比例导引法和组合制导法进行了弹道仿真,分析了比例系数和初始目标线角对弹道和击中目标时间的影响。
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| 关 键 词： | 末制导 制导规律 弹道仿真 比例导引法 组合制导法 |
Research on the Last-Stage Guidance Trajectory Simulation of the TV-guided Missile |
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| GUO Hai-feng,LIU Ze-qian. Research on the Last-Stage Guidance Trajectory Simulation of the TV-guided Missile[J]. Sci-Tech Information Development & Economy, 2009, 19(26): 136-138 |
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| Authors: | GUO Hai-feng LIU Ze-qian |
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| Abstract: | Based on several existing guidance laws of the terminal guidance of TV -guided missile, this paper introduces its basic principles, and using Matlab to make the guidance trajectory simulation of the proportional guidance and the combined guidance, and analyzes the influences of the of the proportional coefficient and the original target line-angle on the guidance trajectory and the time of hitting the target. |
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| Keywords: | last-stage guidance guidance law trajectory simulation proportional guidance combined guidance |
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