High-precision cabin connection method suitable for whole-satellite micro-vibration test

CN115343004BActive Publication Date: 2025-01-10CHINA ACADEMY OF SPACE TECHNOLOGY
View PDF 2 Cites 0 Cited by

Patent Information

Application Number
CN202210790060.2
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2022-07-05
Publication Date
2025-01-10
Estimated Expiration
2042-07-05

Smart Images

  • Figure CN115343004B_ABST
    Figure CN115343004B_ABST
Patent Text Reader

Abstract

The present invention discloses a high-precision cabin segment connection method suitable for whole-satellite micro-vibration tests, and belongs to the field of spacecraft test technology. The method first roughly adjusts the lateral and longitudinal relative deviations of the upper cabin segment relative to the flexible connection device, and then precisely adjusts the longitudinal position and posture of the upper cabin segment relative to the flexible connection device; then, by operating the adjustment device, the X and Y distance deviations of the connection points on the adjustment device relative to the connection points of the flexible connection device meet the docking requirements; then confirm whether the lateral docking accuracy of the upper cabin segment relative to the flexible connection device meets the docking requirements, and finally precisely adjust the longitudinal position of the upper cabin segment relative to the flexible connection device, so that the upper docking surface of the adjustment device is docked with the docking surface of the flexible connection device. The present invention can solve the problem that when a satellite micro-vibration test is conducted with a flexible connection device between cabin segments, when the upper and lower cabin segments are unloaded at the same time, the upper and lower cabin segments cannot be precisely docked using ordinary lifting equipment.
Need to check novelty before this filing date? Find Prior Art

Citation Information

Patent Citations

  • Double-star combination spacecraft in-orbit separation ground testing device and detecting method

    CN108001713A

  • Self-adaptation leveling spacecraft precise butt-joint technology

    CN108356512A