| 半主动雷达地空导弹制导律性能分析 |
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| 引用本文： | 张伟明,杨军,展建超.半主动雷达地空导弹制导律性能分析[J].弹箭与制导学报,2008,28(6). |
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| 作者姓名： | 张伟明 杨军 展建超 |
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| 作者单位： | 1. 西北工业大学航天学院,西安,710072
2. 徐州空军学院,江苏徐州,221007 |
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| 摘 要： | 在半主动雷达地空导弹的建模基础上，通过对比例导引律、扩展比例导引律和现代最优导引律三者的理论及仿真对比分析。明确了三种导引律在不同参数条件下制导精度性能的优劣，对半主动雷达地空导弹导引规律的设计具有重要意义。
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| 关 键 词： | 半主动雷达制导 比例导引 扩展比例导引 最优导引 |
Analysis on Guidance Law Performance of Semi active Radar Guided Surface-to-air Missile |
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| ZHANG Weiming,YANG Jun,ZHAN Jianchao.Analysis on Guidance Law Performance of Semi active Radar Guided Surface-to-air Missile[J].Journal of Projectiles Rockets Missiles and Guidance,2008,28(6). |
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| Authors: | ZHANG Weiming YANG Jun ZHAN Jianchao |
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| Abstract: | Based on modeling of semi-active radar guided surface-to-air missile,a conclusion was given on guided precision of proportional navigation,extended proportional navigation and modern optimal guidance law at different parameters based on both theory and simulation analysis.It is meaningful to the guidance law design of semi-active radar guided surface-to-air missile. |
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| Keywords: | semi-active radar guidance proportional navigation extended proportional navigation optimal guidance |
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