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首页> 外文期刊>SAE International Journal of Aerospace >Bivariate 'Cut-Glue' Approximation of Strongly Nonlinear Mathematical Models Based on Experimental Data
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Bivariate 'Cut-Glue' Approximation of Strongly Nonlinear Mathematical Models Based on Experimental Data

机译:基于实验数据的强非线性数学模型的二元“割胶”逼近

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Researchers meet the difficulties of experimental and computer modeling of a statics and dynamics of aircrafts connected with their essential nonlinearity. This is due to the fact that the aerodynamic effects of the interaction complex aircraft designs or their models with air environment generate abrupt changes of the character of the some dependencies. Aerodynamic coefficients in the model of interaction can be obtained only or by full-scale tests or by computer simulations. Therefore, the construction of mathematical models of the objects is associated with the mathematical processing of the points of the experimental data. In this case, the experimentally obtained dependence is usually essentially nonlinear up to piecewise, or even discontinuous nature. Approximation of such dependencies, even with the use of spline functions, is very difficult and is associated with large errors. The solution to this problem was proposed by the author and was reported to the ASME Congress in November 2014 and published in the Proceedings of the Congress in its final form. In that work possibility of "approximating&multiplicative&additive" processing of dot experimental data for creation of unified mathematical model of the studied object or the phenomenon completely is mathematically proved. The offered method is called "Cut-glue" approximation as it is based on "cutting" of the well approximated intervals of the modelled dependence and their "gluing" in the one analytical function. However, this problem has been solved only for the univariate functions case. In this paper the author presents the solution of a problem of the bivariate 《Cut-glue》 approximation, which significantly expands the scope of application of the method. The creation examples of mathematical models are given. Fragments of the flying devices using the aerostatic flight principle are modeled. Examples show that models even piecewise dependences represent the unified analytical functions. However we can approximate their forms to piecewise so, how it is necessary for the accuracy of the description of experimental data. It is shown that combined application of the "Cut-glue" method of approximation and the piecewise description of separate intervals of the modelled experimental dependence by methods of the regression analysis considerably increases the accuracy of the mathematical dependence description in general. For bivariate models the effect of application of a method becomes stronger, because the error of the description of the significantly nonlinear bivariate dependences by regression methods much more, than univariate dependences.
机译:研究人员遇到了与基本非线性相关的飞机静力学和动力学的实验和计算机建模难题。这是由于这样的事实,即复杂飞机的设计或其模型与空气环境的相互作用产生的空气动力效应会突然改变某些依赖项的特性。相互作用模型中的空气动力学系数只能通过全尺寸测试或计算机模拟获得。因此,对象数学模型的构建与实验数据点的数学处理相关联。在这种情况下,通过实验获得的依赖性通常基本上是非线性的,直到分段的,甚至是不连续的。即使使用样条函数,这种依存关系的近似也非常困难,并且与大错误有关。该问题的解决方案由作者提出,并于2014年11月报告给ASME大会,并以最终形式在大会论文集上发表。通过数学证明了对点实验数据进行“近似,乘积,加法”处理以完全建立被研究对象或现象的统一数学模型的工作可能性。所提供的方法称为“切胶”逼近,因为它是基于“切出”建模的依赖关系的良好近似间隔及其在一个分析函数中的“胶合”。但是,仅对于单变量函数情况已解决了该问题。在本文中,作者提出了二元《 Cut-glue》逼近问题的解决方案,这极大地扩展了该方法的应用范围。给出了数学模型的创建示例。使用空气静力飞行原理对飞行装置的碎片进行建模。例子表明,模型甚至是分段依赖都代表了统一的分析函数。但是,我们可以将它们的形式近似地逐段地近似化,以确保准确描述实验数据。结果表明,结合使用“切胶”方法和通过回归分析的方法分别对建模的实验依赖项的各个区间进行分段描述,可以大大提高数学依赖项描述的准确性。对于双变量模型,应用方法的效果变得更强,因为回归方法对显着非线性双变量依赖性的描述误差比单变量依赖性要大得多。

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