弹丸飞行非线性参数逼近精度的评定

Volodymyr Мaidaniuk Volodymyr, Semen Bondarenko, Andrii Onofriichuk
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引用次数: 0

摘要

本文对弹丸气动力系数(力矩)和大气参数的近似精度进行了评价,其中大气参数具有明显的非线性。以南非Denel Naschem公司155毫米阿塞格M2000弹的气动力系数(力矩)和国际标准ISO 2533:1975/ add . 1:20 85(en)标准大气定义的大气参数为基础。通过给定的表格数据与气动力系数(矩)的近似函数值之间的相对误差(偏差)来估计表格值近似值的精度。采用解析函数作为逼近函数,如一个支持函数(误差函数)和一组基本函数(高斯函数)的和,可以得到一个在弹丸飞行参数变化段上连续微分的逼近函数,可以用单一表达式表示。在Maple软件环境下,将解析函数(误差函数和高斯函数)近似为155-mm阿塞盖M2000弹的气动力(力矩)系数的表值。得到的力系数(力矩)和大气参数的单解析函数值可用于解决计算发射表、使用弹道积分算法(弹道计算器)准备发射现有、新型和正在现代化的火炮系统的数据等问题。结果表明,通过对气动力系数(力矩)和大气参数的表格数据进行迭代逼近,可以在整个变化范围内以连续函数的形式构造弹丸飞行参数的解析函数,从而保证其对表格数据的逼近的给定精度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Assessment of the accuracy of the approximation of the nonlinear parameters of the projectile flight
The article evaluates the accuracy of the approximation of the aerodynamic force coefficients (moments) of the projectile and atmospheric parameters, which are significantly nonlinear. The aerodynamic force coefficients (moments) of the 155-mm Assegai M2000 projectile of the South African company Denel Naschem and atmospheric parameters defined by the international standard ISO 2533:1975/Add.1:1985(en) Standard Atmosphere are taken as basis. The estimation of the accuracy of the approximation of the tabular values is presented through the relative error (misalignment) between the given tabular data and the values of the approximated function of the aerodynamic force coefficients (moments). Analytical functions are used as approximating functions, such as the sum of a support function (error function) and a set of basic functions (Gaussian functions), which makes it possible to obtain an approximating function continuously differentiated on the segment of the change in the projectile flight parameter, which can be represented by a single expression. In the Maple software environment, analytical functions (error functions and Gaussian functions) were approximated to the tabulated values of the aerodynamic coefficients of forces (moments) of the 155-mm Assegai M2000 projectile. The obtained values of the single analytical functions of force coefficients (moments) and atmospheric parameters can be used to solve the problems of calculating firing tables, preparing data using ballistic integrating algorithms (ballistic calculators) for firing existing, new artillery systems and those systems being modernized. It is shown that by iterative procedures of approximation of tabular data of aerodynamic force coefficients (moments) and parameters of the atmosphere, it is possible to construct analytical functions in the form of a continuous function of the projectile flight parameter within the entire range of its change, ensuring the given accuracy of its approximation to the tabular data.
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