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Towards Variable Fidelity Optimization with Hardware in the Loop for Flapping Flight

机译:借助硬件在拍打飞行中实现可变逼真度优化

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摘要

This paper presents a method for optimization of real hardware with reduced need to access the hardware. It does so with a variable fidelity modeling approach. The models used are a high fidelity hardware model and a low fidelity physics based model. These models are invoked strategically to minimize the number of calls to the hardware. With this lower cost, designers can more fully explore design spaces that would otherwise be too expensive to explore using traditional design of experiments on hardware-in-the-loop systems. We show that the presented method identifies an optimal design more efficiently than a Box-Behnken DOE based optimization. Results are presented based on physical hardware tests with a cantilever beam in bending and a Butterworth filter. These examples provide a step toward use of the presented method on a flapping mechanism.
机译:本文提出了一种对真实硬件进行优化的方法,减少了对硬件的访问。它使用可变保真度建模方法来做到这一点。使用的模型是高保真度硬件模型和基于低保真度物理模型。从战略上调用这些模型,以最大程度地减少对硬件的调用次数。以较低的成本,设计人员可以更充分地探索设计空间,否则使用在硬件在环系统上进行的传统实验设计就无法进行昂贵的探索。我们表明,与基于Box-Behnken DOE的优化相比,本文提出的方法可以更有效地识别最佳设计。结果是根据物理硬件测试得出的,其中使用了弯曲的悬臂梁和Butterworth滤波器。这些例子提供了朝在襟翼机构上使用所提出的方法的步骤。

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