弹道模型精确校模方法研究  

Research on accurate correction method of ballistic model

作　　者：贾波[1] 张平[1] 王德伟 王壹 JIA Bo;ZHANG Ping;WANG Dewei;WANG Yi(Chinese People’s Liberation Army 63863, Baicheng 137001, China)

机构地区：[1]中国人民解放军63863部队,吉林白城137001

出　　处：《兵器装备工程学报》2022年第S01期119-123,共5页Journal of Ordnance Equipment Engineering

基　　金：陆军重点项目(1600010230)。

摘　　要：建立一种弹道模型精确校模方法。采用刚体弹道方程,确定射程、横偏、最大弹道高和转速为符合对象,选取阻力符合系数、翻转力矩符合系数、极阻尼力矩符合系数和跳角符合系数作为符合系数,形成多参数、多特征点的全弹道综合校模体系。某型榴弹试验结果表明,在非射击角度,新方法相对传统方法在射程计算上精度大大提高,其他参数也有较大提高。A precise calibration method of ballistic model is established.Using the rigid body trajectory equation,the range,lateral deviation,maximum trajectory height and speed are determined as the coincidence objects,and the resistance coincidence coefficient,overturning torque coincidence coefficient,pole damping torque coincidence coefficient and jump angle coincidence coefficient are selected as the coincidence coefficients to form a multi parameter and multi feature point comprehensive model calibration system for the whole missile track.The test results of a grenade show that the accuracy of range calculation of the new method is greatly improved compared with the traditional method at non firing angle,and other parameters are also greatly improved.

关 键 词：弹道 校模 符合 射表编拟 

分 类 号：TJ012.3[兵器科学与技术—兵器发射理论与技术]