FIELD: testing equipment.
SUBSTANCE: invention relates to testing equipment and may be used in particular to assemble and test multilink large-size structures designed for operation under zero gravity in space. System comprises control unit, which includes personal computer, microcontroller and appropriate software. System comprises three actuating mechanisms, every of which consists of weight-measuring cell connected to platform to sensor of angle of sling horizontal deviation and electric drive, reducer of which is connected to coil, on which sling is wound as going to wirerope layer, on which angle sensor is installed to identify its vertical deviation, together with sensor of sling expenditure. Ends of sling from actuating mechanisms are connected to form a point for suspension of element made weightless. Actuating mechanisms are installed onto coordinate grid.
EFFECT: increased working zone of the system.
3 dwg
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Authors
Dates
2010-10-27—Published
2008-11-17—Filed