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    • 2. 发明授权
    • In-orbit reconfigurable communications satellite
    • 在轨可重构通信卫星
    • US06871045B2
    • 2005-03-22
    • US09907507
    • 2001-07-18
    • Philip A. RubinJeffery B. FreedmanTed M. Kaplan
    • Philip A. RubinJeffery B. FreedmanTed M. Kaplan
    • H04B7/185H04B7/204
    • H04B7/18519H04B7/2041
    • The footprint of a first satellite is reconfigurable in orbit by ground control to switch on and off different transponders. Each transponder is connected to a corresponding downlink antenna feed, each of which transmits a downlink beam independent of the others. The satellite can be moved into different orbits or otherwise changed to service new geographic areas by using different combinations of the transponders. In one embodiment, the satellite includes an antenna and components for an uplink beam corresponding to each downlink beam. Various subsets of the downlink antenna feeds are mechanically linked to move in unison using gimbals, each subset using a corresponding gimbal and mechanical driver. The first satellite is sufficiently reconfigurable that it may serve as a back up satellite to a plurality of other satellites in a constellation of satellites.
    • 第一颗卫星的占地面积可以通过地面控制在轨道上进行重新配置,可以打开和关闭不同的应答器。 每个应答器连接到相应的下行链路天线馈送,每个馈送单独发送下行链路波束。 可以通过使用转发器的不同组合,将卫星移动到不同的轨道或以其他方式改变以服务于新的地理区域。 在一个实施例中,卫星包括用于与每个下行链路波束对应的上行链路波束的天线和分量。 下行链路天线馈送的各种子集被机械地连接以使用万向节一致地移动,每个子集使用对应的万向节和机械驱动器。 第一颗卫星是可重构的,它可以作为卫星星座中多个其他卫星的备用卫星。