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Method for determining the orbital positions of satellites in LEO networks

机译:确定leo网络中卫星轨道位置的方法

摘要

In order to achieve a considerable reduction of the outlay required on the ground in connection with the accurate calculation of the exact orbital position of each individual satellite of a constellation, first the exact orbital position of a preferably central master satellite of a sub-group of satellites embodied as a special formation is determined. This calculation is performed autonomously on board the satellite by means of customary measurements supported from the ground, or respectively by means of GPS, MANS, etc. Then the exact position of all other satellites in the same formation is determined from range and pointing data, which are provided by each IS link terminal. These pointing data are well known after the establishment of the inter- satellite link and are continuously updated.
机译:为了实现与星座的每个单独卫星的精确轨道位置的精确计算有关的地面上所需的支出的显着减少,首先,最好是一个卫星子组的中央主卫星的精确轨道位置。确定体现为特殊编队的卫星。此计算是通过地面上的常规测量值,或者分别通过GPS,MANS等,在卫星上自主进行的。然后,根据距离和指向数据确定同一编队中所有其他卫星的确切位置,由每个IS链路终端提供。这些指向数据在卫星间链路建立之后是众所周知的,并且会不断更新。

著录项

  • 公开/公告号US6219617B1

    专利类型

  • 公开/公告日2001-04-17

    原文格式PDF

  • 申请/专利权人 CONTRAVES SPACE AG;

    申请/专利号US19990225916

  • 发明设计人 JOHANN KELLERMEIER;THOMAS DREISCHER;

    申请日1999-01-05

  • 分类号G01C210/60;G06G77/80;

  • 国家 US

  • 入库时间 2022-08-22 01:04:34

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