公开(公告)号：US20230182931A1

公开(公告)日：2023-06-15

申请号：US18061844

申请日：2022-12-05

Applicant: HARBIN INSTITUTE OF TECHNOLOGY, SHENZHEN

Inventor： Chengfei YUE ,  Cheng WEI ,  Xibin CAO ,  Xueqin CHEN ,  Shi QIU ,  Tao LIN

IPC: B64G7/00 ,  G01M17/00

CPC classification number: B64G7/00 ,  G01M17/00

Abstract: Disclosed are a ground test system and a test method for a space-oriented multi-arm spacecraft system. A spacecraft system simulator floats on an air-floating platform through four porous air feet, a test truss is placed around the air-floating platform, a simulation auxiliary docking device, a simulation crawling truss and a satellite model are arranged in a middle of a ceiling of the test truss, and an assembly test area and a silent air compressor are arranged on sides of the test truss. The application is used to solve the problems that the prior art cannot simulate the movement and crawling of the multi-arm spacecraft system in space, assembly of large space structures, and the prior art cannot simulate the influence of assembling, catching and other actions on a base in a weightless environment.