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PARAMETER IDENTIFICATION OF FLYING WING WITH SIGNIFICANT DEFORMATION

机译:具有显着变形的飞翼参数识别

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The in-flight deformation is a characteristic challenge in the design of the HALE UAVs. This paper deals with identifying the parameters of a multibody model of a flying wing of high aspect ratio, where the pressure distribution over the wing is calculated using a built-in Vortex-Lattice method in every step of the simulation. The identification is based on drop tests of a scale model of a flat wing and image processing.
机译:飞行中变形是HALE UAV的设计中的特征挑战。本文涉及识别高纵横比的飞翼的多体模型的参数,其中在模拟的每个步骤中使用内置涡旋晶格方法计算机翼上的压力分布。该识别基于扁平翼和图像处理的比例模型的掉落测试。

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