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A data-driven approach to model calibration for nonlinear dynamical systems

机译:用于非线性动力系统模型校准的数据驱动方法

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摘要

A data-driven approach to model calibration is developed to accurately obtain the input parameters for nonlinear dynamical systems. The paper focuses on the convergence properties of the proposed method, which play a significant role in understanding the validity and usefulness of any data-driven model. The input parameters of nonlinear dynamical systems are optimized to a reference solution, which can be experimental data or results from a high-fidelity computer simulation, using the Wasserstein metric and a phase-space representation of a set of time-dependent signals. Test cases shown in this paper include the Lorenz system and the discharge plasma of a Hall effect thruster to characterize the numerical uncertainties of the proposed data-driven approach, given a constructed reference solution. Distinct wells in the cost function, the Wasserstein metric, are obtained relative to the reference solution, illustrating the applicability of the proposed method to dynamical problems. The numerical uncertainties associated with the phase-space portrait and sampling time are discussed.
机译:开发了一种数据驱动的模型校准方法,以准确地获得非线性动力系统的输入参数。本文侧重于所提出的方法的收敛特性,这在了解任何数据驱动模型的有效性和有用性方面发挥着重要作用。非线性动力系统的输入参数被优化到参考解决方案,参考解决方案可以是使用Wasserstein度量和一组时间相关信号的相位空间表示的高保真计算机模拟的实验数据或结果。本文所示的测试用例包括Lorenz系统和霍尔效应推进器的放电等离子体,以表征所构造的参考解决方案,表征所提出的数据驱动方法的数值不确定性。在成本函数中,Wassersein度量的明显孔是相对于参考解决方案获得的,说明所提出的方法对动态问题的适用性。讨论了与相位空间纵向和采样时间相关的数值不确定性。

著录项

  • 来源
    《Journal of Applied Physics》 |2019年第24期|244901.1-244901.15|共15页
  • 作者单位

    Texas A&M Univ Dept Aerosp Engn College Stn TX 77843 USA;

    Texas A&M Univ Dept Aerosp Engn College Stn TX 77843 USA;

    Air Force Res Lab Edwards Afb CA 93524 USA;

    Air Force Res Lab Edwards Afb CA 93524 USA;

    Air Force Res Lab Edwards Afb CA 93524 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
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