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Satellite constellation forming system, satellite constellation forming method, satellite constellation, deorbit method, debris recovery method, and ground device

机译:卫星星座形成系统,卫星星座形成方法,卫星星座,脱毛方法,碎屑回收方法和地面装置

摘要

The satellite constellation formation system forms two satellite constellation (20), which has two orbital planes with different normal orientations and two orbital planes where the same number of satellites fly.In the satellite constellation formation part, the satellite passing timing is shifted from the state in which the satellite passing timing of the satellite passing through each track plane deviates from the state where the satellite passing through each track plane is deviated from the state in which the satellite passing timing is shifted in the point of intersection (PC) of the two track planes in each track plane of two track planes The orbit height of at least one of the two orbital planes is gradually varied.
机译:卫星星座形成系统形成两颗卫星星座(20),其具有两个具有不同正常取向的两个轨道平面和两个轨道平面,其中两个轨道平面在相同数量的卫星飞行中。在卫星星座形成部分中,卫星通过定时从状态移位 其中通过每个轨道平面的卫星通过的卫星通过定时偏离通过每个轨道平面的卫星偏离卫星通过定时在两者的交叉点(PC)的位置偏离的状态 两个轨道平面的每个轨道平面中的轨道平面逐渐变化了两个轨道平面中的至少一个的轨道高度。

著录项

  • 公开/公告号JPWO2020240825A1

    专利类型

  • 公开/公告日2021-10-21

    原文格式PDF

  • 申请/专利权人 三菱電機株式会社;

    申请/专利号JP20210521733

  • 发明设计人 迎 久幸;

    申请日2019-05-31

  • 分类号B64G1/10;B64G3;

  • 国家 JP

  • 入库时间 2022-08-24 21:50:10

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