| 摘要 |
A satellite communication system includes a plurality of spacecraft in geosynchronous orbit, where each spacecraft provides a plurality of beams on the surface of the earth, and a plurality of ground stations individual ones of which are located in one of the beams for transmitting uplink signals to one of the spacecraft. Each spacecraft has a plurality of receivers for receiving a plurality of the uplinked signals from ground stations, a frequency translator for translating the received uplink signals to a transmission frequency of a plurality of downlink signals, and a plurality of transmitters for transmitting the plurality of downlink signals within the same beams as the corresponding uplink signals. Each transmitter includes a combiner for combining together a plurality of frequency translated signals and a power amplifier, such as a TWTA, for amplifying the combined plurality of frequency translated signals. Each of the plurality of receivers is gain controlled by a corresponding one of the ground stations for providing immunity to rain attenuation. Preferably the beams have different sizes and shapes, and are non-contiguous over a least a portion of the earth's surface. It is also preferred that the uplink beams to a first one of the satellites have a first polarization and downlink beams have a second, opposite polarization, and that uplink beams to a second one of the satellites have the second polarization and downlink beams have the first polarization. The uplink and downlink signals may be digital television signals, and each of the spot beams overlies a predetermined designated television market area.
|
