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Reliability Analysis Of A Satellite Structure With A Parametric And A Non-parametric Probabilistic Model

机译:具有参数和非参数概率模型的卫星结构可靠性分析

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The reliability of a satellite structure subjected to harmonic base excitation in the low frequency range is analyzed with respect to the exceedance of critical frequency response thresholds. Both a parametric model of uncertainties and a more recently introduced non-parametric model are used to analyze the reliability, where the latter model in the present analysis captures the model uncertainties. With both models, the probability of exceedance of given acceleration thresholds is estimated using Monte-Carlo simulation. To reduce the computational cost of the parametric model, a suitable meta-model is used instead. The results indicate that for low levels of uncertainty in the damping, the non-parametric model provides significantly more pessimistic - and hence conservative - predictions about the exceedance probabilities. For high levels of damping uncertainty the opposite is the case.
机译:针对超出临界频率响应阈值的情况,分析了在低频范围内受到谐波基极激励的卫星结构的可靠性。不确定性的参数模型和最近引入的非参数模型都用于分析可靠性,其中本分析中的后者模型捕获了模型的不确定性。在这两个模型中,使用蒙特卡洛仿真估计超过给定加速度阈值的概率。为了减少参数模型的计算成本,可以使用合适的元模型来代替。结果表明,对于较低的阻尼不确定性水平,非参数模型提供了对超出概率的更为悲观的预测,因此提供了更为保守的预测。对于高水平的阻尼不确定性,情况恰恰相反。

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