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大型舱段装配中的水平对接技术研究

易旺民1,段碧文2,高峰1,韩先国2   

  1. 1.北京卫星环境工程研究所
    2.北京航空航天大学机械工程及自动化学院
  • 出版日期:2014-11-18 发布日期:2014-11-18

Research on the level docking technology in large cabin assembly

  • Online:2014-11-18 Published:2014-11-18

摘要: 舱段对接是航天器总装过程中的关键工序,国内目前仍然采用人工操作方式完成对接。为了满足对接装配的高精度、自动化需求,提出了一种基于自动化手段的大型舱段对接装配技术,即水平对接技术。首先,从理论角度介绍了该技术的工作原理,具体阐述了其基于并联机构的位姿控制和力随动控制两大技术要点,然后进行了舱段水平对接装配试验。最后,通过试验证明了位姿控制方式能将销钉轴线位姿精度从0.3mm提高到0.1mm,满足舱段对接在销钉插入销孔阶段的位姿精度要求,同时证明了力随动控制能根据支链力变化实时变换舱段位姿,满足舱段对接在压紧密封圈阶段的舱段小变形要求。

关键词: 舱段装配, 水平对接, 并联机构, 位姿控制, 力随动控制

Abstract: Cabin docking is a key process in the spacecraft assembly,which is still done manually in the domestic field.In order to improve the assembly quality,efficiency and automation,this paper presents an automatic docking technology in the level direction.Firstly,the paper briefly introduces the principle of this technique,and elaborates its key technologies including the pose control and the force control based on the parallel architectures.Secondly,the cabin level docking tests have been done.Finally,the experiment results demonstrate that the pose control can improve the accuracy of axis pin from 0.3mm to 0.1mm,which meets the requirements in the stage of inserting the pins into the pin holes during the cabin docking.Meanwhile,the force control can achieve real-time cabin posture changes following the branched chain force changes,which meets the requirements of small cabin deformation in the stage of compressing the seal rings between the two of cabins.

Key words: cabin assembly, level docking, parallel architectures, pose control, force control

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