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SATELLITE CONSTELLATION FORMATION SYSTEM, SATELLITE CONSTELLATION FORMATION METHOD, SATELLITE CONSTELLATION, AND GROUND EQUIPMENT

机译:卫星星座形成系统,卫星星座形成方法,卫星星座,和地面设备

摘要

A satellite constellation forming system forms a satellite constellation (20) having a plurality of orbital planes (21) in each of which a plurality of satellites fly at the same orbital altitude. A satellite constellation forming unit forms the satellite constellation (20) in which orbital altitudes of the orbital planes (21) are mutually different. Furthermore, in the satellite constellation (20), relative altitude differences between adjacent orbital planes in the plurality of orbital planes are sequentially arranged to be sinusoidal. The satellite constellation forming unit sequentially changes an orbital altitude (23) of each orbital plane of the plurality of orbital planes while maintaining a sinusoidal arrangement of the relative altitude differences between adjacent orbital planes in the plurality of orbital planes.
机译:卫星星座形成系统形成具有多个轨道平面(21)的卫星星座(20),其中每个轨道平面中有多个卫星以相同的轨道高度飞行。卫星星座形成单元形成卫星星座(20),其中轨道面(21)的轨道高度相互不同。此外,在卫星星座(20)中,多个轨道平面中相邻轨道平面之间的相对高度差被顺序地布置成正弦曲线。卫星星座形成单元依次改变多个轨道平面中每个轨道平面的轨道高度(23),同时保持多个轨道平面中相邻轨道平面之间的相对高度差的正弦排列。

著录项

  • 公开/公告号EP3978371A1

    专利类型

  • 公开/公告日2022-04-06

    原文格式PDF

  • 申请/专利权人 MITSUBISHI ELECTRIC CORPORATION;

    申请/专利号EP20190931208

  • 发明设计人 MUKAE HISAYUKI;

    申请日2019-05-31

  • 分类号B64G1/10;

  • 国家 EP

  • 入库时间 2022-08-25 00:21:30

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