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Electronically steered inter-satellite optical communication system and methods

机译:电子控制的卫星间光通信系统和方法

摘要

Aspects are generally directed to an inter-satellite communication system and method of communicating between satellites. In one example, an inter-satellite communication system includes a first satellite transceiver having an entrance aperture, and a non-mechanical beamsteering device configured to steer a first beam of encoded optical data over a field of view thereof. The first satellite transceiver may include coarse steering optics configured to extend a field of regard of the non-mechanical beamsteering device. During a transmit mode, the coarse steering optics are positioned to transmit the first beam of encoded optical data through the entrance aperture in a direction of a second satellite transceiver. The first satellite transceiver may also include a beam splitter positioned, during a receive mode, to receive a second beam of encoded optical data from the second satellite transceiver and direct the second beam of encoded optical data to an optical sensor.
机译:方面通常针对卫星间通信系统和卫星之间的通信方法。在一个示例中,卫星间通信系统包括:具有入口孔的第一卫星收发器;以及非机械波束控制装置,其被配置为在其视场上引导编码的光学数据的第一波束。第一卫星收发器可以包括粗略转向光学器件,该粗略转向光学器件被配置为扩展非机械波束转向设备的视场。在发射模式期间,定位粗略转向光学器件以在第二卫星收发器的方向上通过入射孔发射编码的光学数据的第一光束。第一卫星收发器还可以包括分束器,该分束器定位成在接收模式期间从第二卫星收发器接收编码的光学数据的第二束,并将编码的光学数据的第二束引导至光学传感器。

著录项

  • 公开/公告号US10243654B1

    专利类型

  • 公开/公告日2019-03-26

    原文格式PDF

  • 申请/专利权人 RAYTHEON COMPANY;

    申请/专利号US201815941821

  • 发明设计人 GERALD P. UYENO;SEAN D. KELLER;

    申请日2018-03-30

  • 分类号H04B10/118;H04B10/40;

  • 国家 US

  • 入库时间 2022-08-21 12:11:52

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