Method for compensating spatial relative position errors of horizontal automatic boring and riveting machine of aircraft panel with temperature factor
A technology of automatic drilling and riveting machines and horizontal wall panels, which is applied in aircraft assembly and other directions, and can solve the problems of not considering the relative pose accuracy requirements between equipment
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[0098] In order to describe the present invention more specifically, the technical solutions of the present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0099] The active positioning device and the driven positioning device described in the present invention are respectively the numerical control positioning device on the hole making side and the numerical control positioning device on the upsetting side in a horizontal automatic drilling and riveting machine tool used for aircraft panel assembly disclosed in CN105643278A Locate the device.
[0100] Such as figure 1 As shown, a method for compensating the space relative pose error of an aircraft panel horizontal automatic drilling and riveting machine combined with temperature factors in the present invention specifically includes:
[0101] Step 1, define the coordinate systems in the horizontal automatic drilling and riveting machine for aircraft panels...
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