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A comparison of piecewise cubic Hermite interpolating polynomials,cubic splines and piecewise linear functions for the approximation of projectile aerodynamics 被引量:4
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作者 C.A.Rabbath D.Corriveau 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2019年第5期741-757,共17页
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 repr... 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. 展开更多
关键词 Aerodynamic coefficients PIECEWISE POLYNOMIAL functionS cubic splines Curve fitting PIECEWISE linear functionS PIECEWISE cubic hermite interpolating POLYNOMIAL PROJECTILE modelling and simulation Fire control inputs Precision Ballistic computer software
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欧拉弯曲梁三次Hermite区间样条多小波有限元分析 被引量:1
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作者 夏逸鸣 唐敢 江世永 《河海大学学报(自然科学版)》 CAS CSCD 北大核心 2012年第3期313-318,共6页
基于小波多辨分析思想,选择三次Hermite区间样条函数作为多小波尺度基函数,用于构建梁单元多尺度位移近似空间;由最小势能原理,推导出欧拉弯曲梁有限元平衡方程.结果表明:该小波单元可通过改变多小波尺度函数的尺度来重新划分网格,从而... 基于小波多辨分析思想,选择三次Hermite区间样条函数作为多小波尺度基函数,用于构建梁单元多尺度位移近似空间;由最小势能原理,推导出欧拉弯曲梁有限元平衡方程.结果表明:该小波单元可通过改变多小波尺度函数的尺度来重新划分网格,从而可自由调节小波单元的计算精度;其计算精度与采用具有相同网格划分的任意多个传统欧拉弯曲梁单元求解的精度完全相同;该小波单元更加清晰地反映了小波有限元与传统有限元之间的关联. 展开更多
关键词 三次hermite区间样条函数 尺度函数 多小波 有限元
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基于非等间距灰色模型的捷联惯组误差系数建模预测 被引量:3
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作者 张志警 刘洁瑜 马学文 《导弹与航天运载技术》 北大核心 2011年第5期40-42,共3页
捷联惯组历次测试数据由于受到各种因素的影响,数据量少,而且测试时间也是非等间隔的。针对这一特点,提出了捷联惯组误差系数非等间隔灰色建模预测新方法。通过3次样条函数插值,将不等间隔序列调整为等间隔序列;同时将基本预测模型中参... 捷联惯组历次测试数据由于受到各种因素的影响,数据量少,而且测试时间也是非等间隔的。针对这一特点,提出了捷联惯组误差系数非等间隔灰色建模预测新方法。通过3次样条函数插值,将不等间隔序列调整为等间隔序列;同时将基本预测模型中参数的构造方法加以改进,从而建立非等间隔时序灰色模型。实例分析证明该模型能够准确反映捷联惯组历次测试数据的变化规律,为解决捷联惯组历次测试数据小样本建模问题提供一种可行的途径。 展开更多
关键词 捷联惯组 灰色模型 3次样条函数插值 非等间隔 预测
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