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METHOD AND SYSTEM FOR MONITORING A PHASE FOR TRANSFERRING A SATELLITE FROM AN INTIAL ORBIT TO A MISSION ORBIT

机译:监视从初始轨道向发射轨道转移卫星的阶段的方法和系统

摘要

Disclosed is a method (70) for monitoring a phase for transferring a satellite (20) from one earth orbit, called “initial orbit”, to another earth orbit, called “mission orbit”, in particular a transfer using electric propulsion unit. The monitoring method includes a step for estimating the direction of the satellite during the transfer phase by way of an earth array antenna (30) including a plurality of elementary antennas (31), each elementary antenna having a primary radiation lobe with a width greater than or equal to 20°, the elementary antennas (31) being oriented such that their respective fields of vision overlap, the direction of the satellite being estimated based on at least one useful phase difference measurement between signals corresponding to a target signal, transmitted by the satellite and received on a pair of elementary antennas (31).
机译:公开了一种监视相位的方法( 70 ),该相位用于将卫星( 20 )从一个称为“初始轨道”的地球轨道转移到称为“任务轨道”,特别是使用电动推进装置的转移。该监视方法包括以下步骤:通过包括多个基本天线( 31 )的地球阵列天线( 30 )来估计传输阶段的卫星方向。 ,每个基本天线都具有一个主辐射波瓣,其宽度大于或等于20°,基本天线( 31 )的方向应使其各自的视野重叠,卫星方向为根据卫星发送并在一对基本天线( 31 )上接收的,与目标信号相对应的信号之间的至少一个有用的相位差测量结果进行估算。

著录项

  • 公开/公告号US2016131737A1

    专利类型

  • 公开/公告日2016-05-12

    原文格式PDF

  • 申请/专利权人 AIRBUS DEFENCE AND SPACE SAS;

    申请/专利号US201414392193

  • 发明设计人 JEAN-MARC AYMES;

    申请日2014-06-24

  • 分类号G01S5/02;B64G3/00;B64G1/00;G01S3/46;

  • 国家 US

  • 入库时间 2022-08-21 14:39:02

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