航空学报 > 2010, Vol. 31 Issue (3): 546-552

结构动力学模型修正的三步策略及其实践

丁继锋1, 马兴瑞2, 韩增尧1, 庞世伟1   

  1. 1.北京空间飞行器总体设计部 2.中国航天科技集团公司
  • 收稿日期:2009-02-03 修回日期:2009-05-05 出版日期:2010-03-25 发布日期:2010-03-25
  • 通讯作者: 韩增尧

Three-step Model Updating Method in Structure Dynamics and Its Application

Ding Jifeng1, Ma Xingrui2, Han Zengyao1, Pang Shiwei1   

  1. 1 Beijing Institute of Spacecraft Systems Engineering 2 China Aerospace Science and Technology Corporation
  • Received:2009-02-03 Revised:2009-05-05 Online:2010-03-25 Published:2010-03-25
  • Contact: Han Zengyao

摘要: 首先构建了由模型结构调整、模型参数修正以及模型确认组成的三步模型修正策略。该方法优于传统模型修正方法的是:在模型修正之初基于误差定位、灵敏度分析以及工程经验进行的模型结构调整可以给出一个适于参数修正的初始有限元模型,从而保证了模型修正的成功。然后,采用三步法针对国际上模型修正的标准考题——GARTEUR19结构动力学模型进行修正,详尽论述了模型结构调整、参数修正以及模型确认的过程,并将修正结果与国外同行的研究结果进行了对比,综合精度与国际先进水平相当,从而验证了三步模型修正策略的有效性。

关键词: 三步策略, 模型结构调整, 参数修正, 模型确认, 灵敏度分析, GARTEUR19模型

Abstract: A three-step method for model updating consisting of model structure tuning, model parameter updating and model validation is presented in this article. The method is thought to be better than the traditional model updating method in that model structure tuning based on error location, sensitivity analysis and engineering insight can generate an appropriate initial model in the first step and ensure the success of model updating. Then, the model of the GARTEUR19 benchmark structure is updated by the three-step method, and details of the process for model structure tuning, parameter updating and model validation are provided. The prediction accuracy of the updated model is on a par with pioneering results of European research, which confirms the effectiveness of the method.

Key words: three-step method, model structure tuning, model parameter updating, model validation, sensitivity analysis, GARTEUR19

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