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Uncertainty Analysis of a Large-Scale Satellite Finite Element Model

机译:大型卫星有限元模型的不确定度分析

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摘要

The effects of uncertainties in the material properties and the geometry of a satellite structure are investigated fornvarious aspects of the structural performance. The underlying numericalmodel is a refined large-scale finite elementnmodel, which naturally implies a large number of uncertain parameters. To cope with the computational challengenassociated with the large number of parameters, recently developed advancedMonte Carlo simulation methods arenapplied.Because of their insensitivitywith respect to the number of uncertain parameters, thesemethods are suitablenfor large-scale finite element models arising in aerospace applications. The numerical results indicate significantnscatter in the quantities of interest and hence emphasize the importance of accounting for uncertainties in thennumericalmodel to rationally assess the structural performance and to ensure its reliability. Furthermore, the paperndemonstrates that due to the efficiency of the adopted uncertainty analysis methods, the associated computationalnefforts are greatly reduced and hence manageable, if compared with traditional methods.
机译:对于结构性能的各个方面,研究了不确定性对卫星结构的材料特性和几何形状的影响。潜在的数值模型是一个经过精炼的大规模有限元模型,它自然意味着存在大量不确定参数。为了应对与大量参数相关的计算难题,因此未使用最近开发的先进的蒙特卡洛模拟方法。由于它们对不确定参数的数量不敏感,因此这些方法适用于航空航天应用中的大型有限元模型。数值结果表明感兴趣量的显着分散,因此强调了在数值模型中考虑不确定性的重要性,以便合理地评估结构性能并确保其可靠性。此外,该论文表明,由于采用了不确定性分析方法,因此与传统方法相比,相关的计算工作量大大减少,因此可管理。

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  • 来源
    《Journal of Spacecraft and Rockets》 |2009年第1期|p.191-202|共12页
  • 作者单位

    University of Innsbruck, 6020 Innsbruck, AustriaESA, 2200 AG Noordwijk, The NetherlandsManuel F. Pellissetti‡and Helmut J. Pradlwarter§University of Innsbruck, 6020 Innsbruck, Austria;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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