首页> 外文会议>International symposium on ballistics >A COMPARISON OF PIECEWISE CUBIC HERMITE INTERPOLATING POLYNOMIALS, CUBIC SPLINES AND PIECEWISE LINEAR FUNCTIONS FOR THE APPROXIMATION OF PROJECTILE AERODYNAMICS
【24h】

A COMPARISON OF PIECEWISE CUBIC HERMITE INTERPOLATING POLYNOMIALS, CUBIC SPLINES AND PIECEWISE LINEAR FUNCTIONS FOR THE APPROXIMATION OF PROJECTILE AERODYNAMICS

机译:近似射影气动的分段立方赫尔姆特插值多项式,立方样条和分段线性函数的比较

获取原文

摘要

Modelling and simulation of projectile flight is at the core of ballistic computer software and is essential to the study of performance of rifles and projectiles in various engagement conditions. An effective and representative numerical model of projectile flight requires a relatively good approximation of the aerodynamics. The aerodynamic coefficients of the projectile model should be described as a series of piecewise polynomial functions of the Mach number that ideally meet the following conditions: they are continuous, differentiable at least once, and have a relatively low degree. The paper provides the steps needed to generate such piecewise polynomial functions using readily available tools, and then compares Piecewise Cubic Hermite Interpolating Polynomial (PCHIP), cubic splines, and piecewise linear functions, and their variant, as potential curve fitting methods to approximate the aerodynamics of a generic small arms projectile. A key contribution of the paper is the application of PCHIP to the approximation of projectile aerodynamics, and its evaluation against a set of criteria. Finally, the paper provides a baseline assessment of the impact of the polynomial functions on flight trajectory predictions obtained with 6-degree-of-freedom simulations of a generic projectile. This is an extended abstract of a paper published in Defence Technology, 2019.
机译:弹丸飞行的建模和仿真是弹道计算机软件的核心,对于研究各种参与条件下的步枪和弹丸的性能至关重要。有效且具有代表性的弹丸飞行数值模型需要相对良好的空气动力学近似值。弹丸模型的空气动力学系数应描述为一系列马赫数的分段多项式函数,这些函数理想地满足以下条件:它们是连续的,至少可微分的并且具有相对较低的程度。本文提供了使用易于使用的工具生成此类分段多项式函数所需的步骤,然后比较了分段三次Hermite插值多项式(PCHIP),三次样条和分段线性函数,以及它们的变体,作为近似于空气动力学的潜在曲线拟合方法。通用小型武器弹丸。本文的主要贡献是将PCHIP应用于弹丸空气动力学的逼近,并根据一组标准对其进行了评估。最后,本文对多项式函数对通用弹丸的6自由度模拟获得的飞行轨迹预测的影响进行了基线评估。这是在《国防技术》 2019年发表的论文的扩展摘要。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号