首页> 外国专利> SPACE TRAVEL INFORMATION RECORDING DEVICE, Collision Avoidance SUPPORT SYSTEM, Collision Avoidance SUPPORT PROGRAM, Collision Avoidance SUPPORT DEVICE, INFORMATION MANAGEMENT PROCEDURE, MEGA CONSTELATION BUSINESS DEVICE, DRUM SUPPLY BUSINESS DEVICE, DRUM SUPPLY SYSTEM, DRUM SUPPLY PROGRAM, SSA BUSINESS DEVICE, COLISION AVOIDANCE SUPPORT BUSINESS EQUIPMENT, SATELLITE BUSINESS EQUIPMENT, CONSTELLATION BUSINESS EQUIPMENT, RACE START BUSINESS EQUIPMENT, OPEN ARCHITECTURE BUSINESS AND DATA STORAGE

SPACE TRAVEL INFORMATION RECORDING DEVICE, Collision Avoidance SUPPORT SYSTEM, Collision Avoidance SUPPORT PROGRAM, Collision Avoidance SUPPORT DEVICE, INFORMATION MANAGEMENT PROCEDURE, MEGA CONSTELATION BUSINESS DEVICE, DRUM SUPPLY BUSINESS DEVICE, DRUM SUPPLY SYSTEM, DRUM SUPPLY PROGRAM, SSA BUSINESS DEVICE, COLISION AVOIDANCE SUPPORT BUSINESS EQUIPMENT, SATELLITE BUSINESS EQUIPMENT, CONSTELLATION BUSINESS EQUIPMENT, RACE START BUSINESS EQUIPMENT, OPEN ARCHITECTURE BUSINESS AND DATA STORAGE

机译:太空旅行信息记录装置、防撞支持系统、防撞支持程序、防撞支持设备、信息管理程序、大型星座业务设备、鼓供应业务设备、鼓供应系统、鼓供应程序、SSA业务设备、防撞支持业务设备、卫星业务设备、星座业务设备、竞赛启动业务设备、开放式架构业务和数据存储

摘要

A space information recorder (100) acquires space object information (500), which is orbit forecast information of a plurality of space objects (60), from a management business device (40) used by a management business operator that manages the plurality of space objects (60), and records the space object information (500). The space object information (500) includes a forecast epoch, a forecast orbital element, and a forecast error of each of the plurality of space objects (60). When it is foreseen that a space object A included in the plurality of space objects (60) will intrude into a range at orbital altitudes of 300 km to 1000 km in which a satellite group of LST 10:00 to 11:00 is present, a time period from intrusion to exit and orbit forecast information are recorded.
机译:空间信息记录器(100)从管理多个空间物体(60)的管理业务经营者使用的管理业务设备(40)获取空间物体信息(500),即多个空间物体(60)的轨道预报信息(60),并记录该空间物体信息(500)。空间物体信息(500)包括一个预测周期、一个预测轨道元素和多个空间物体(60)中每个空间物体的预测误差。当预见到多个空间物体(60)中包括的空间物体A将侵入轨道高度为300公里至1000公里的范围,其中存在LST 10:00至11:00的卫星群时,记录从入侵到退出的时间段和轨道预报信息。

著录项

  • 公开/公告号EP4119449A4;EP2023004119449A4;EP4119449A4;EP4119449

    专利类型

  • 公开/公告日2023-08-09

    原文格式PDF

  • 申请/专利权人 MITSUBISHI ELECTRIC CORPORATION;

    申请/专利号EP21768351A;EP202100000768351A;EP21768351A;EP20210768351

  • 发明设计人

    申请日2021-03-09

  • 分类号B64G1/10;B64G1/24;B64G1/56;B64G1/64;B64G1/68;B64G3;

  • 国家

  • 入库时间 2024-06-15 00:02:15

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