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MEASUREMENT METHOD OF DYNAMIC POSITION OFWING BASELINE BASED ON IFEM AND RZT

机译:基于IFEM和RZT的机翼基线动态位置测量方法。

摘要

A measurement method of a dynamic position of a wing baseline based on the Inverse Finite Element Method (iFEM) and the Refined Zigzag Theory (RZT) is disclosed, which comprises four steps: determining a three-dimensional model of a selected wing; designing arrangement of a fiber Bragg grating (FBG) sensor array and a strain rosette on the surface of the wing; establishing an RZT-based inverse finite element simulation model; and finally reading and converting measured data, to obtain a dynamic position of a wing baseline. The present invention realizes an RZT-based measurement method of a dynamic position of a wing baseline, having good robustness and high applicability.
机译:公开了一种基于逆有限元法(iFEM)和精细之字形理论(RZT)的机翼基线动态位置的测量方法,该方法包括四个步骤:确定所选机翼的三维模型;确定所述机翼的三维模型。机翼表面的光纤布拉格光栅(FBG)传感器阵列和应变花环的设计布置;建立基于RZT的逆有限元仿真模型;最后读取并转换测量数据,以获得机翼基线的动态位置。本发明实现了一种基于RZT的机翼基线动态位置测量方法,具有良好的鲁棒性和较高的适用性。

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