The invention discloses a space control test system. The space control test system comprises a task sample section, a microsatellite simulator and a marble platform, the microsatellite simulator is arranged on the task sample section through the ejection separation mechanism, and after the microsatellite simulator is separated from the task sample section through the ejection separation mechanism, the microsatellite simulator is suspended on the marble platform through the first air floating piece and located in the control range of the task sample section. The first air floating piece is used for simulating a vacuum weightlessness environment of the microsatellite simulator, and the task sample section further comprises a multi-degree-of-freedom flexible gripper assembly configured in a control range and used for gripping the microsatellite simulator and a high-pressure gas cylinder providing an inflation gas source for the first air floating piece. The space control test system can reduce or overcome the influence of the gravity effect under the ground condition, simulates the weightless space environment, further verifies the motion state of the satellite equipment in the environment, and grabs the satellite equipment through the gripper.

    本发明公开了一种空间操控试验系统,该空间操控试验系统包括:任务样段,微小卫星模拟器及大理石平台;微小卫星模拟器通过弹射分离机构设置在任务样段上,在弹射分离机构将微小卫星模拟器与任务样段分离后,微小卫星模拟器通过第一气浮件悬浮于大理石平台上并位于任务样段的操控范围内,第一气浮件用于模拟微小卫星模拟器的真空失重环境,任务样段还包括配置在操控范围内用于抓取微小卫星模拟器的多自由度柔性抓手组件以及为第一气浮件提供充气气源的高压气瓶。本发明的空间操控试验系统可以在地面条件下减小或克服重力作用影响,模拟出失重的太空环境,进而验证卫星设备在该环境下的运动状态并通过抓手对其进行抓取等操作。


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    Title :

    Space control test system


    Additional title:

    空间操控试验系统


    Contributors:
    DING YUN (author) / LONG KEYOU (author) / CHEN YANG (author) / ZHAN QINGXI (author) / REN SHAOCHEN (author)

    Publication date :

    2024-11-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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