| 多导弹协同制导律综述 |
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| 引用本文： | 王建青,李帆,赵建辉,万聪梅.多导弹协同制导律综述[J].飞行力学,2011,29(4):6-10. |
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| 作者姓名： | 王建青 李帆 赵建辉 万聪梅 |
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| 作者单位： | 北京航空航天大学仪器科学与光电工程学院,北京,100191 |
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| 摘 要： | 根据制导约束条件的不同,将多导弹协同制导律划分为具有弹着时间、终端角度、终端速度分别约束,以及弹着时间与终端角度同时约束四类.系统地论述了各类导引律的方法和特点,总结和分析了其优缺点,并对其发展趋势进行了探讨,可为多导弹协同制导律的优化设计提供参考.
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| 关 键 词： | 多导弹协同 制导律 弹着时间 终端角度 终端速度 |
Summary of guidance law based on cooperative attack of multi-missile method |
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| WANG Jian-qing,LI Fan,ZHAO Jian-hui,WAN Cong-mei.Summary of guidance law based on cooperative attack of multi-missile method[J].Flight Dynamics,2011,29(4):6-10. |
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| Authors: | WANG Jian-qing LI Fan ZHAO Jian-hui WAN Cong-mei |
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| Institution: | WANG Jian-qing,LI Fan,ZHAO Jian-hui,WAN Cong-mei(School of Instrument Science and Opto-electronics Engineering,BUAA,Beijing 100191,China) |
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| Abstract: | According to the constraints in different cases for missile guidance,the multi-missile cooperation guidance law is divided into four typical kinds,which base on the different constraint conditions,such as the impact time,the terminal angle,the terminal speed,and the impact time together with the terminal angle.It is expected to specify the methods and characteristic of each guidance law and summarize their advantage and disadvantage systematically.Then,the development trends are discussed which also provide... |
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| Keywords: | multi-missile cooperation guidance law impact time terminal angle terminal speed |
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