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引用次数: 0

摘要

飞机舱室换热数学模型参数估计的不确定性要求使用联合置信区间对模型参数进行估计。参数估计的联合置信区域在模型参数空间中描述了以模型参数实际值向量为中心的r维椭球体,其中$r$为模型参数个数。在参数向量维数较大的情况下,联合置信区域的使用存在计算困难。因此,将各所需参数的条件联合置信区间以联合置信区域在参数空间相应坐标轴上的投影形式引入,相当于将椭圆区域替换为其周边的平行六面体。近二三十年来,随着强大的超级计算机技术的出现,为耗时任务(包括多维任务)的数值求解开辟了新的可能性。由于蒙特卡罗方法具有良好的并行性和有效性,并且与其他方法相比,它对劳动强度对问题维数增加的敏感性要小得多,因此具有很强的竞争力。特别是,基于抛物方程决策的概率概念的多维问题可以用统计建模的方法来解决。在随机微分方程数值解的基础上,利用对扩散过程预期功能参数的导数评估,利用不连续系数抛物型边值问题求解飞机机身蜂窝芯和网格结构的热状态逆问题成为可能。
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Confidence Intervals for Identification Parameters of Heat Exchange Processes in Aircraft Instrument Compartments
Uncertainty of estimating the parameters of the aircraft compartments heat exchange mathematical model requires the use of a joint confidence region for estimating the model parameters. The joint confidence regions of parameter estimates describe in the model parameter space the r- dimensional ellipsoid with the center in the vector of the model parameters actual values, where $r$ is the number of model parameters. In the case of a large dimension of the parameter vector, the use of the joint confidence region is associated with computational difficulties. Therefore, conditional joint confidence intervals of each required parameters are introduced in the form of projections of the joint confidence region on the corresponding coordinate axes of the parameter space, which is equivalent to replacing the elliptical region by the parallelepiped circumscribed around it. In recent two or three decades, with the emergence of a powerful supercomputer technology, new possibilities for the numerical solution of the time-consuming tasks, including multidimensional ones, have opened up. Due to the fact that the Monte-Carlo methods are parallelized with a good measure of effectiveness and compared with other methods they are far less sensitive by labor intensity to the dimension of problems increase, they become more competitive. In particular, multi-dimensional problems for parabolic equations on the basis of probabilistic concepts of their decisions can be solved by the method of statistical modeling. Among other things, it is possible to solve inverse problems of the thermal state of the aircraft fuselage honeycomb core and grid constructions using the parabolic boundary value problem with discontinuous coefficients basing on the numerical solution of stochastic differential equations with the use of derivatives assessments on the expected functional parameters of the diffusion processes.
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