В. Майданюк, С. Бондаренко, В. Грабчак
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引用次数: 0

摘要

在计算弹丸飞行轨迹时,一个迫切需要解决的问题是在弹丸空间运动微分方程数学模型系统中具有明显非线性性质的气动力(力矩)和大气参数的定义和表示。气动系数表格值的数值微分运算是确定气动力误差的一个重要组成部分,气动系数表格值作为微分方程系统中的分量。在这个方向上,一种基于解析函数逼近大气气动系数和参数数据的科学方法是很有前途的,其要求是能够在弹丸飞行参数的整个变化范围内获得一个单一的连续函数,并保证它们与表格数据的最佳逼近。进一步发展了统一的方法来定性地逼近不同空气动力系数和大气参数的可能性;作为逼近函数,提出用一个解析函数作为参考函数(误差函数)和一组基本函数(高斯函数)的和,从而得到弹丸飞行参数变化段的连续微分逼近函数,该函数可以用单一解析表达式表示。得到的弹丸飞行参数变化段上的单次连续微分近似于气动系数和大气参数的函数,用单一解析表达式给出,可用于解决火炮发射系统弹道积分算法的射击表计算和数据准备问题。关键词:气动力(力矩),大气参数,弹丸,近似,微分,解析表达式,误差函数,高斯函数。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
АНАЛІТИЧНІ ФУНКЦІЇ НЕЛІНІЙНИХ ПАРАМЕТРІВ ПОЛЬОТУ СНАРЯДА
When calculating projectile flight trajectories, an urgent issue is the definition and representation of aerodynamic forces (moments) and parameters of the atmosphere, which are significantly non-linear in nature, in the system of mathematical models - differential equations of spatial motion of projectiles. A significant component of the error in determining the aerodynamic force is introduced by the operation of numerical differentiation of tabular values of aerodynamic coefficients, which are included as components in systems of differential equations. In this direction, a scientific approach based on the approximation of the data of aerodynamic coefficients and parameters of the atmosphere by analytical functions is promising, the requirement for which is the possibility of obtaining a single and continuous function within the entire range of changes in the flight parameters of the projectile and ensuring their best approximation to tabular data. A unified approach to the possibility of approximating qualitatively different aerodynamic coefficients and parameters of the atmosphere found further development; as approximating functions, it is proposed to use an analytical function as the sum of a reference function (error function) and a set of basic functions (Gaussian functions), which allows to obtain a continuous-differentiated approximating function on the segment of the change of the projectile flight parameter, which can be represented by a single analytical expression. The obtained values of the single continuous-differentiated on the segment of the change of the projectile flight parameter approximating the function of the aerodynamic coefficients and the parameters of the atmosphere, which are given by a single analytical expression, can be used to solve the problems of calculating Firing tables and preparing data using ballistic integrating algorithms for firing artillery systems. Keywords: aerodynamic forces (moments), parameters of the atmosphere, projectile, approximation, differentiation, analytical expression, error function, Gaussian function.
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