| 空对地导弹的变结构三维导引律(英文) |
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| 引用本文： | 陈胜琪.空对地导弹的变结构三维导引律(英文)[J].火力与指挥控制,2009,34(5). |
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| 作者姓名： | 陈胜琪 |
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| 作者单位： | 西北工业大学航天学院,陕西,西安,710072 |
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| 摘 要： | 推导了空对地导弹的三维导引律模型,并设计了针对机动目标的变结构导引律,分析了其制导特性.设计的导引律由于需要的目标信息少,可以便利地应用于实际工程中,数字仿真结果证实了设计的导引律的可行性.
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| 关 键 词： | 空对地导弹 变结构 导引律 |
A 3-D Guidance Law for Air to Surface Missile |
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| CHEN Shengqi.A 3-D Guidance Law for Air to Surface Missile[J].Fire Control & Command Control,2009,34(5). |
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| Authors: | CHEN Shengqi |
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| Institution: | College of Astronautics;Northwestern Polytechnical University;Xi'an 710072;China |
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| Abstract: | Three dimension kinematic model for air to surface missile is given, then a variable structure guidance law is designed considering the characteristics of surface maneuver target.Performance of the guidance system is analyzed theoretically.Guidance law proposed in the paper can be implemented conveniently in engineering as it needs little target information.Numerical simulation result sustains the effectiveness of the guidance law. |
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| Keywords: | air to surface missile variable structure guidance law |
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