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Stochastic Lookup Tables - A Method for the Integration of Parametric Uncertainties in Non-Linear Simulation Models

机译:随机查找表 - 一种在非线性模拟模型中集成参数不确定性的方法

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Integration of uncertainties in flight physical simulation models opens up a variety of stochastic analysis methods, which can provide highly valuable confidence statements about the computed results. However, embedding random variables in non-linear simulation models of aerospace vehicles is by no means straightforward. They usually contain precomputed results in form of multi-dimensional data arrays, e.g. lookup tables for aerodynamic coefficients. The given variance within those tables is generally not constant, e.g. the confidence about the linear region in aerodynamic coefficients is much higher than for the post-stall behavior. The present study suggests and compares two methods for the low parametric inclusion of uncertainties in lookup tables with non-constant variance. One method injects the uncertainty at sparsely placed pivot points whereas the other one makes use of a principal component decomposition. We conducted Monte Carlo experiments and found that both methods are able to reproduce the demanded uncertainty variation in the sampled lookup table realizations. The eigenvalue method is superior in terms of variance distribution fitting and model order reduction.
机译:飞行中不确定性的整合性地开辟了各种随机分析方法,可以为计算结果提供高度有价值的置信度陈述。然而,在航空航天车辆的非线性模拟模型中嵌入随机变量绝不是直截了当的。它们通常包含以多维数据阵列的形式预先计算的结果,例如,用于空气动力学系数的查找表。例如,这些表中的给定方差通常不是恒定的,例如,空气动力学系数中线性区域的置信度远高于停滞行为。本研究表明,并比较了具有非恒定方差的查找表中的低参数化不确定性的两种方法。一种方法将不确定性注入稀疏放置的枢轴点,而另一个方法在另一个中利用主成分分解。我们进行了Monte Carlo实验,发现两种方法都能够在采样查找表的实现中重现所需的不确定性变化。特征值方法在方差分布拟合和模型顺序减少方面优越。

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