| 火箭弹引信作用时间自适应修正技术 |
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| 引用本文： | 杨会军,程翔,张河.火箭弹引信作用时间自适应修正技术[J].弹道学报,2006,18(3):51-54. |
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| 作者姓名： | 杨会军 程翔 张河 |
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| 作者单位： | 南京理工大学,机械工程学院,南京,210094 |
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| 摘 要： | 针对非旋转火箭弹初速低、散布较大降低了命中概率的问题,结合影响火箭弹飞行时间的几个特征参数,介绍了非旋转火箭弹引信作用时间自适应修正技术.结合实例计算了不同装定时间在某最大速度条件下所需要的修正时间.运用曲线拟合归纳出了修正用的经验公式.该技术对于提高火箭弹的命中概率具有重要意义.
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| 关 键 词： | 火箭弹 引信 自适应修正 感应装定 |
| 文章编号： | 1004-499X(2006)03-0051-04 |
| 收稿时间： | 2005-12-31 |
| 修稿时间： | 2005年12月31 |
Acting Time Adaptive Correcting Technology of Rocket Ammunition Fuze |
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| YANG Hui-jun,CHENG Xiang,ZHANG He.Acting Time Adaptive Correcting Technology of Rocket Ammunition Fuze[J].Journal of Ballistics,2006,18(3):51-54. |
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| Authors: | YANG Hui-jun CHENG Xiang ZHANG He |
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| Affiliation: | College of Mechanical Engineering, NUST, Nanjing 210094, China |
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| Abstract: | According to non spinning rocket's characteristics of low initial velocity and much dispersion,which result in low target hitting probability,and combined with the key parameters affecting flying time, the acting time adaptive correcting technology of non spinning rocket ammunition fuze of was introduced.Combined with an example,the needed correcting time corresponding to different setting time for a certain maximum velocity was calculated.Through curve fitting,experience formula was summarized.The technology is of great importance to improve hitting probability of rocket ammunition. |
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| Keywords: | rocket ammunition fuze adaptive correction inductive setting |
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