Simulation of the positioning process of the spacecraft's components at the final stages of assembly

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The paper treats the issue of efficient method of the spacecraft’s components at the final stages of assembly. Measurements of large-sized structure’s surfaces were carried out by the laser coordinate-measuring system. The advantages of using a coordinate measuring system based on the laser radar over patterns are shown. The results of the measurements are presented.

Spacecraft, laser radar, cloud of points, pattern, geometrics control, 3d pattern

Короткий адрес: https://sciup.org/148312588

IDR: 148312588

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