首页> 外文会议>AIAA aviation forum >Surrogate Models and Mixtures of Experts in Aerodynamic Performance Prediction for Mission Analysis
【24h】

Surrogate Models and Mixtures of Experts in Aerodynamic Performance Prediction for Mission Analysis

机译:特派团分析空气动力学性能预测专家代理模型及其混合

获取原文

摘要

Accurate aircraft fuel burn evaluation requires performing a detailed mission analysis covering the entire mission, from takeoff to landing. This process is computationally expensive, as it requires up to millions of aerodynamic performance evaluations, and thus it is advantageous to use surrogate models as approximations of the actual aerodynamic models. Training surrogate models is challenging due to the high nonlinearity of the aerodynamic performance functions in the transonic regime. Conventional surrogate models, such as radial basis function and kriging, are deemed insufficient to model these functions accurately. To address this issue, we explore several ways to improve the predictive performance of surrogate models. First, we employ an adaptive sampling algorithm in addition to the more traditional space-filling algorithm. Second, we improve the kriging performance by including gradient information in the interpolation (gradient-enhanced kriging), as well as by introducing a known trend in the global model component (kriging with a trend). Lastly, we propose a mixture of experts approach, which is derived based on the divide-and-conquer principle. In this last approach, we use multiple surrogate models as local experts to approximate different parts of the input space, using machine learning techniques to infer about the function profile to automatically partition the input space. These various surrogate models are tested using aerodynamic data for conventional and unconventional aircraft configurations. We then perform a surrogate-based mission analysis using the selected surrogate models. Our results show that the proposed mixture of experts approach can significantly improve the predictive performance when approximating the aerodynamic performance. For example, a mixture of five gradient-enhanced kriging models (with adaptive sampling) achieves 5% approximation error with around 100 samples, whereas the adaptive sampling fails to converge when training a global model. However, when we have a simple function profile, using a global model is more efficient than a mixture of experts, due to the added computational complexity in the latter.
机译:准确的飞机燃料烧伤评估需要进行详细的任务分析,从起飞到着陆。该过程是计算昂贵的,因为它需要多达数百万的空气动力学性能评估,因此利用代理模型作为实际空气动力学模型的近似是有利的。培训代理模型由于跨音制度的空气动力学性能功能的高度非线性而挑战。传统的代理模型,例如径向基函数和克里格,被认为是准确地模拟这些功能的不足。为了解决这个问题,我们探讨了提高代理模型的预测性能的几种方法。首先,除了更传统的空间填充算法之外,我们还使用自适应采样算法。其次,我们通过在插值(梯度增强的Kriging)中包括梯度信息,以及通过在全球模型组件中引入已知趋势(具有趋势的克里格)来提高克里格化性能。最后,我们提出了一个专家方法的混合,这是基于分裂和征服原则来源的。在这最后的方法中,我们使用多个代理模型作为本地专家来近似输入空间的不同部分,使用机器学习技术来推断出函数配置文件来自动分区输入空间。使用传统和非传统飞机配置的空气动力学数据测试这些各种替代模型。然后,我们使用所选代理模型执行基于代理的任务分析。我们的研究结果表明,在近似气动性能的情况下,专家方法的建议混合物可以显着提高预测性能。例如,五个梯度增强的Kriging模型(具有自适应采样)的混合物实现了大约100个样本的5%近似误差,而自适应采样在训练全局模型时无法收敛。然而,当我们有一个简单的功能简单时,由于后者的计算复杂性增加了计算复杂性,使用全球模型比专家的混合更有效。

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