Modeling and Simulation of Fuze Flight Rotating Speed

Qi Xiao, Zhi-min Yin, Tengfei Gao, Husheng Guo, Haifei Sun, Zhipeng Wang
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Abstract

The ammunition fuze is the control device to control the projectile initiation in the proper position and the best time of during the flight. In view of the poor life-likeness of the current fuze rotation speed model which directly affects the centrifugal test of the fuze, so it cannot judge the quality of the fuze scientifically. In this paper the working mechanism of fuze centrifugal environment is comprehensively Analysed, the mathematical model of rotational velocity attenuation law of two kinds of projectiles constructed, and the actual measurement of projectile rotation velocity is completed based on radio technology, the motion parameters of the model calculated ,and the validity of the model is verified by simulation .
引信飞行转速建模与仿真
弹药引信是控制弹丸在飞行过程中在适当位置和最佳时间起爆的控制装置。目前的引信转速模型逼真度差,直接影响引信的离心试验,不能科学地判断引信的质量。本文全面分析了引信离心环境的工作机理,建立了两种弹体转速衰减规律的数学模型,并基于无线电技术完成了弹体转速的实际测量,计算了模型的运动参数,并通过仿真验证了模型的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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