Zero-gravity compensation device for carbon fiber supporting rod type solar wing

The invention relates to a zero gravity compensation device for a carbon fiber support rod type solar wing, which is characterized by comprising a fixed lifting rope, a fixed device, a follow-up lifting rope and a follow-up device, one end of the fixed lifting rope is fixed on the fixed device, and the other end of the fixed lifting rope is fixed on a support rod connected with a solar wing simulation wall; one end of the follow-up lifting rope is fixed to the follow-up device, and the other end of the follow-up lifting rope is fixed to a supporting rod connected with the solar wing outer plate. The fixed device is mounted at a fixed position and comprises a position-adjustable lifting rope mounting point used for mounting a fixed lifting rope, and the lifting rope mounting point is alwayslocated on the axis of a root hinge, connected with the solar wing simulation wall, of the supporting rod; and the follow-up device can perform compound motion of circular motion and linear motion bytaking the plate hinge as