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SATELLITE COMMUNICATIONS SUBSYSTEM IN-ORBIT VERIFICATION SYSTEM AND METHODOLOGIES

机译:卫星通信子系统在轨验证系统和方法

摘要

The present invention relates to satellite systems and more particularly, to the provision of novel systems and methods for verifying the in-orbit performance and operation of satellite communications subsystems. In contrast to traditional Payload IOT (in-orbit test), the invention operates without an uplink signal, by generating hardware-specific signatures using isolated, internally generated, thermal noise. It has been found that this noise provides a very stable, repeatable signal for testing. Prior to launch, a repeater command sequence is executed to generate a hardware-specific signature based on the internally-generated noise. The same repealer command sequence is then executed in-orbit to determine whether the hardware-specific signature has changed. The two signatures may be recorded and compared using a simple tool such as a spectrum analyzer. The methods also include novel use of the sun as a test signal source to calibrate equipment, to quantify atmospheric effects and to be used as an intermediate reference power level during measurements.
机译:本发明涉及卫星系统,更具体地说,涉及用于检验卫星通信子系统的在轨性能和操作的新颖系统和方法的提供。与传统的有效载荷IOT(在轨测试)相反,本发明通过使用隔离的,内部产生的热噪声来产生硬件特定的签名,而无需上行链路信号即可操作。已经发现,这种噪声为测试提供了非常稳定,可重复的信号。在启动之前,将执行转发器命令序列以基于内部生成的噪声来生成硬件特定的签名。然后,在轨执行相同的中继器命令序列,以确定特定于硬件的签名是否已更改。可以使用简单的工具(例如频谱分析仪)记录并比较两个签名。该方法还包括新颖地使用太阳作为测试信号源来校准设备,量化大气影响并在测量过程中用作中间参考功率水平。

著录项

  • 公开/公告号EP3381142A4

    专利类型

  • 公开/公告日2019-07-17

    原文格式PDF

  • 申请/专利权人 TELESAT CANADA;

    申请/专利号EP20160867497

  • 发明设计人 REID STEPHEN;YIP ROGER;

    申请日2016-11-28

  • 分类号H04B17/40;H04B7/185;H04B17/21;

  • 国家 EP

  • 入库时间 2022-08-21 12:29:58

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