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Coordinate transformation uncertainty analysis and reduction using hybrid reference system for aircraft assembly

机译:混合参考系统用于飞机装配的坐标变换不确定度分析与简化

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Purpose - In aircraft assembly, standard reference points with nominal coordinates are commonly applied for coordinate transformation between multiple measurement stations and the assembly coordinate system. For several reasons in practical application, these points often fail to envelop the key assembly space, which leads to large transformation uncertainty. This paper aims to analyze and further reduce the coordinate transformation uncertainty by introducing a new hybrid reference system (HRS). Design/methodology/approach - Several temporary extension points without known coordinates are added to enhance the tightness between different stations, especially at the weakness area in the network, thus constituting an HRS together with the existing standard reference points. The coordinate transformation model of the HRS-based measurement network is established based on an extend Gauss-Markov model. By using the geometrical differential property and variance-covariance propagation law, the covariance matrixes in the transformation model are calculated, and the analytical solution of the uncertainties of transformation parameters are ultimately derived. The transformation uncertainty of each check points is presented by Helmert error expression. Findings-The proposed analytical solution of transformation uncertainty is verified using the state-of-the-art Monte Carlo simulation method, but the solution process is simpler and the computation expenses are much less. Practical implications - The HRS with three temporary extension points is practically applied to a tail boom in-site measurement for assembly. The average transformation uncertainty has been reduced by 26 per cent to less than 0.05 mm. Originality/value - The hybrid coordinate transformation model is proposed for the first time. The HRS method for transformation uncertainty reduction is more economical and practical than increasing the number of standard reference points.
机译:目的-在飞机装配中,通常将具有名义坐标的标准参考点用于多个测量站与装配坐标系之间的坐标转换。由于实际应用中的几个原因,这些要点通常无法包围关键的装配空间,从而导致较大的转换不确定性。本文旨在通过引入新的混合参考系统(HRS)来分析并进一步减少坐标转换的不确定性。设计/方法/方法-添加了几个未知坐标的临时扩展点,以增强不同站点之间的紧密性,尤其是在网络中的薄弱区域,从而与现有的标准参考点一起构成了HRS。基于扩展的高斯-马尔可夫模型,建立了基于HRS的测量网络的坐标转换模型。利用几何微分性质和方差-协方差传播定律,计算出变换模型中的协方差矩阵,最终得出变换参数不确定性的解析解。每个检查点的变换不确定性由Helmert误差表达式表示。结果-使用最新的蒙特卡洛模拟方法验证了所提出的变换不确定性解析解决方案,但求解过程更简单,计算量也更少。实际意义-具有三个临时延伸点的HRS实际上被应用于尾梁的现场测量以进行组装。平均变形不确定度降低了26%,小于0.05毫米。创意/价值-首次提出了混合坐标转换模型。减少变换不确定性的HRS方法比增加标准参考点的数量更为经济和实用。

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