A satellite solar wing positioning tooling

The present invention relates to a positioning satellite solar wing assemblies, including transport vehicle, said transport vehicle having a loading platform, said carrier having a platform translation mechanism thereof; said translation mechanism comprises a first flange, Tic-Tac-beams, the first two flange fixedly mounted on the first flange of the first and second ball screw ball screw fixedly mounted on said second flange; upon rotation of the first ball screw, can slide along the crosswise beam in a first direction on a first ball screw flange; when the rotation of the second ball screw, enables the second flange of the beam along a second ball screw Tic the sliding direction.