| 飞航导弹BTT制导规律研究 |
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| 引用本文： | 栾泽威,李风雷.飞航导弹BTT制导规律研究[J].战术导弹技术,1991(4):26-31,25. |
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| 作者姓名： | 栾泽威 李风雷 |
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| 作者单位： | 哈尔滨工业大学
(栾泽威)，航空航天部三院三部(李风雷) |
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| 摘 要： | 论述了将BTT导引控制技术应用到某型飞导弹的方法。根据常规弹道的特点，选用自主控制加比例导引的制导方法地制导律及制导逻辑，并以此型飞航导弹为原准弹进行了全弹道数字仿真。最后对仿真结果进行了分析。
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| 关 键 词： | 飞航导弹 BTT制导规律 导引规律 倾斜转弯技术 |
STUDY OF BTT GUIDANCE LAW FOR CRUISE MISSILE |
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| Luan Zewei Harbin Institute of Technology Li Fenglei The Third Research Academy of MAS.STUDY OF BTT GUIDANCE LAW FOR CRUISE MISSILE[J].Tactical Missile Technology,1991(4):26-31,25. |
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| Authors: | Luan Zewei Harbin Institute of Technology Li Fenglei The Third Research Academy of MAS |
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| Affiliation: | Luan Zewei Harbin Institute of Technology Li Fenglei The Third Research Academy of MAS |
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| Abstract: | A method of applying BTF control technique to a cruise missile is discussed. On the basis of conventional trajectory, the guidance method of autonomous and proportional navigation has been chosen, the guidance law and its logic have been designed. All trajectory digital simulation for the cruise missile has been made. Finally, the simulation results are analysed- |
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| Keywords: | Missile Missile guidance Guidance law ~*Bank-to-Turn |
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