Attitude sensor for spacecraft
    1.
    发明授权
    Attitude sensor for spacecraft 失效
    航天器姿态传感器

    公开(公告)号:US06634601B2

    公开(公告)日:2003-10-21

    申请号:US10044145

    申请日:2002-01-11

    IPC分类号: B64G166

    摘要: A spacecraft is provided that includes a communications payload having an antenna support structure and an antenna boom coupled to the antenna support structure. An attitude sensor may be mounted to the antenna boom. The attitude sensor (such as an Earth sensor, a star tracker and/or a sun sensor) may be mounted at a root of the antenna boom.

    摘要翻译: 提供了一种航天器,其包括具有天线支撑结构的通信有效载荷和耦合到天线支撑结构的天线臂。 姿态传感器可以安装到天线臂。 姿态传感器(例如地球传感器,星形跟踪器和/或太阳传感器)可以安装在天线臂的根部。