Singularity-Free Analytic Solution of Ballistic Trajectory with Quadratic Drag

Dong-Yeon Lee, M. Tahk, Chang-hun Lee, Young-Won Kim
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Abstract

In this study, an approximate analytic solution that represents the ballistic trajectory under the quadratic drag is studied. The analytic solution has the following assumptions: gravity is constant and drag is proportional to the square of velocity. The previous studies under these assumptions provide a closed-form solution of velocity as a function of flight path angle, but it is prone to a singularity problem that the denominator is zero under certain conditions. In this study, the derivation process of the previous solution is investigated to analyze the physical meaning of the singularity condition. The analysis shows that analytic derivation using altitude as the independent variable produces singularity conditions and affects the time and downrange calculations. New substitution variables are introduced to avoid these singularity conditions. Numerical simulations are conducted to find the new solution singularity free and accurate.
二次阻力弹道的无奇异解析解
本文研究了在二次阻力作用下弹道轨迹的近似解析解。解析解有如下假设:重力恒定,阻力与速度的平方成正比。以往在这些假设下的研究都给出了速度随航迹角函数的封闭解,但在某些条件下容易出现分母为零的奇点问题。本文研究了前一种解的推导过程,分析了奇异条件的物理意义。分析表明,以高度为自变量的解析推导会产生奇异条件,影响时间和下程计算。为了避免这些奇异条件,引入了新的替代变量。数值模拟表明,新解无奇点且精度高。
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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