An Analysis Method of Aircraft Skin Positioning Deviation Based on n-2-1 Positioning
A technology of aircraft skinning and analysis methods, applied in fuselage bulkheads, instruments, calculations, etc., can solve problems such as low stiffness, easy deformation, and inability to accurately calculate the contact stiffness of flexible workpieces
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[0024] The present invention will be further described below in conjunction with accompanying drawing.
[0025] refer to figure 1 , an aircraft skin positioning deviation analysis method based on N-2-1 positioning, the steps are as follows:
[0026] 1. Data collection
[0027] according to figure 2 In the positioning scheme of the middle skin, the data of each positioning point and two measuring points on the skin are collected, including the position data of the positioning point and the error value of the positioning source of each positioning point, and the initial positioning point is determined as (2, 4, 5).
[0028] 2. Calculate the rigid positioning offset and determine the initial state of positioning
[0029] According to the deterministic positioning principle, the constraint equation F(q, r)=0 of the skin at the positioning point is established, and q is the coordinate of the key feature point, that is, the three positioning points (1, 3, 6) and two The measuri...
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