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Alternative TitleGround microgravity dynamic loading simulation mechanism for satellite
徐志刚; 王亚军; 王军义; 刘勇
Rights Holder中国科学院沈阳自动化研究所
Patent Agent沈阳科苑专利商标代理有限公司 21002
Other AbstractThe invention relates to simulation equipment for ground integrated dynamic analog after a flexible solar wing is installed on a moonlet, in particular to a ground microgravity dynamic loading simulation mechanism for a satellite. The ground microgravity dynamic loading simulation mechanism for the satellite comprises a marble platform, a five-degree-of-freedom air-floating platform, a three-degree-of-freedom hoist, a two-dimensional servo platform, a Stewart platform, a constant force hanging mechanism, a solar wing follow truss and a loading mechanical arm. The three-degree-of-freedom hoist is arranged above the marble platform, a truss is arranged below the three-degree-of-freedom hoist, the two-dimensional servo platform and the Stewart platform are installed below the truss, the solar wing follow truss is installed below the Stewart platform, the loading mechanical arm is installed on the solar wing follow truss, the five-degree-of-freedom air-floating platform is placed on the marble platform, and a solar wing is installed on the five-degree-of-freedom air-floating platform. The constant force hanging mechanism is installed below the two-dimensional servo platform and is in spherical hinge connection with the center of mass of the solar wing. The ground microgravity dynamic loading simulation mechanism for the satellite has the advantages of being reliable in structure, accurate in pose following, complete and vivid in simulation, controllable in disturbance loading, safe to operate and the like.
PCT Attributes
Application Date2015-05-06
Date Available2016-08-24
Application NumberCN201510227675.4
Open (Notice) NumberCN104787363A
Contribution Rank1
Document Type专利
Recommended Citation
GB/T 7714
徐志刚,王亚军,王军义,等. 一种卫星地面微重力动态加载模拟机构[P]. 2015-07-22.
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File name: CN201510227675.4.pdf
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