首页> 外文期刊>The Aeronautical Journal >GPR-based novel approach for non-linear aerodynamic modelling from flight data
【24h】

GPR-based novel approach for non-linear aerodynamic modelling from flight data

机译:基于GPR的飞行数据非线性空气动力学建模的新型方法

获取原文
获取原文并翻译 | 示例
       

摘要

In this paper, a Gaussian process regression (GPR)-based novel method is proposed for non-linear aerodynamic modelling of the aircraft using flight data. This data-driven regression approach uses the kernel-based probabilistic model to predict the non-linearity. The efficacy of this method is examined and validated by estimating force and moment coefficients using research aircraft flight data. Estimated coefficients of aerodynamic force and moment using GPR method are compared with the estimated coefficients using maximum-likelihood estimation (MLE) method. Estimated coefficients from the GPR method are statistically analysed and found to be at par with estimated coefficients from MLE, which is popularly used as a conventional method. GPR approach does not require to solve the complex equations of motion. GPR further can be directed for the generalised applications in the area of aeroelasticity, load estimation, and optimisation.
机译:本文采用了使用飞行数据的飞机的非线性空气动力学建模,提出了基于高斯进程回归(GPR)的新方法。该数据驱动的回归方法使用基于内核的概率模型来预测非线性度。通过使用研究飞行飞行数据估计力和矩系数来检查和验证该方法的功效。使用最大似然估计(MLE)方法将使用GPR方法进行比较使用GPR方法的空气动力力和时刻的估计系数。来自GPR方法的估计系数在统计学上分析,发现与来自MLE的估计系数相同,其普遍用作传统方法。 GPR方法不需要解决动作复杂方程。 GPR进一步可以针对空气弹性,负荷估计和优化领域的广义应用。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号