Satellite communication system using RF power sharing for multiple feeds or beams in downlinks
First Claim
1. A communication system, comprising:
- at least one spacecraft in geosynchronous orbit, said spacecraft providing 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 said beams for transmitting uplink signals to said spacecraft;
wherein said spacecraft is comprised of a plurality of receivers for receiving a plurality of the uplink signals in separate channels in said beam from ground stations, a frequency translator for translating the received uplink signals to a transmission frequency of a plurality of downlink signals, a plurality of channel amplifiers, each channel amplifier adapted to amplify a respective transmitted uplink signal and each channel amplifier being gain controlled by a corresponding one of said ground stations, and a plurality of transmitters for transmitting the plurality of downlink signals within the same beams as the corresponding uplink signals; and
wherein each said transmitter is comprised of a combiner for combining together a selected plurality of frequency translated channel amplified signals and a power amplifier for amplifying the combined plurality of frequency translated channel amplified signals, and further comprising an output splitter for separating the amplified combined plurality of frequency translated channel amplified signals into a plurality of downlink signals in a plurality of said beams.
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Accused Products
Abstract
A satellite communication system includes at least one spacecraft in geosynchronous orbit for providing 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 the spacecraft. The 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. An analysis is performed of how many transponder channels can be combined and power amplified in a single TWTA, or multiple paralleled TWTAs, and a determination is then made as to which feeds and/or beams have low data traffic and low required downlink power that makes then suitable candidates for combining their feeds and/or beams into a linearly driven TWTA(s). A reverse output multiplexer is used to separate the combined feeds and/or beams to the separate individual downlinks after the RF power amplification.
45 Citations
20 Claims
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1. A communication system, comprising:
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at least one spacecraft in geosynchronous orbit, said spacecraft providing 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 said beams for transmitting uplink signals to said spacecraft;
whereinsaid spacecraft is comprised of a plurality of receivers for receiving a plurality of the uplink signals in separate channels in said beam from ground stations, a frequency translator for translating the received uplink signals to a transmission frequency of a plurality of downlink signals, a plurality of channel amplifiers, each channel amplifier adapted to amplify a respective transmitted uplink signal and each channel amplifier being gain controlled by a corresponding one of said ground stations, and a plurality of transmitters for transmitting the plurality of downlink signals within the same beams as the corresponding uplink signals; and
whereineach said transmitter is comprised of a combiner for combining together a selected plurality of frequency translated channel amplified signals and a power amplifier for amplifying the combined plurality of frequency translated channel amplified signals, and further comprising an output splitter for separating the amplified combined plurality of frequency translated channel amplified signals into a plurality of downlink signals in a plurality of said beams. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
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12. A method of power sharing in a satellite communication system comprising the steps of:
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receiving a plurality of uplink signals from individual ground stations located in a beam of a satellite, separating the uplink signals in each beam into into a transponder channel;
channel amplifying each transponder channel dependent on a control signal received from a corresponding ground station;
combining a plurality of beams of the satellite, each beam including a plurality of selected uplink signals from fixed users in a designated local to local closed system spot beam area, each selected uplink signal being assigned to a predetermined transponder channel that does not interfere with another selected uplink signal, wherein the signals in each beam are processed as a group;
feeding the combined plurality of beams to a single power amplifier, wherein a sum of a maximum RF power for a plurality of corresponding downlink signals for the beams selected to be combined does not exceed a power handling capability of the power amplifier;
separating the combined feeds into the plurality of downlink signals, each downlink signal assigned to the predetermined channel of the corresponding uplink channel; and
transmitting the individual downlink signals in the plurality of beams.
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13. A communication system using a geostationary earth orbit satellite comprising:
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at least one spacecraft in geosynchronous orbit, said spacecraft providing a plurality of beams on the surface of the earth; and
a plurality of fixed ground stations, individual ones of which are located in one of said beams for transmitting uplink signals to said spacecraft, wherein the system comprises a local to local closed system, and each fixed ground station is located within a designated closed system spot beam area; and
whereinsaid spacecraft is comprised of a plurality of receivers for receiving a plurality of the uplink signals in separate channels in said beam from ground stations, a frequency translator for translating the received uplink signals to a transmission frequency of a plurality of downlink signals, a plurality of channel amplifiers, each channel amplifier adapted to amplify a respective transmitted uplink signal and each channel amplifier being gain controlled by a corresponding one of said ground stations, and a plurality of transmitters for transmitting the plurality of downlink signals within the same beams as the corresponding uplink signals; and
whereineach said transmitter is comprised of a combiner for combining together a selected plurality of frequency translated channel amplified signals and a power amplifier for amplifying the combined plurality of frequency translated channel amplified signals, and further comprising an output splitter for separating the amplified combined plurality of frequency translated channel amplified signals into a plurality of downlink signals in a plurality of said beams.
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14. A satellite communication system comprising:
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at least one spacecraft providing a plurality of downlink beams on the surface of the earth;
a plurality of ground stations, multiple ground stations located in each of the beams, each ground station adapted to transmit and gain control an uplink signal transmitted from the ground station to the spacecraft, wherein each spacecraft comprises;
a plurality of receivers for receiving each uplink signal, each receiver adapted to receive each uplink signal on a separate channel of the receiver;
a frequency translator for translating each received uplink signal to a transmission frequency of a corresponding downlink signal;
a separate channel amplifier for each channel of the receiver, each channel amplifier being individually gain controlled by the ground station corresponding to the received uplink signal;
a combiner for combining together a selected plurality of frequency translated, channel amplified uplink signals;
a single power amplifier adapted to amplify the combined plurality of frequency translated, channel amplified uplink signals; and
an output splitter for separating the amplified the combined plurality of frequency translated, channel amplified uplink signals into a plurality of downlink signals in the beams for transmission.
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15. A method of satellite communication comprising the steps of:
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combining a plurality of lower power downlink beams in a transponder channel;
summing the combined plurality of lower power downlink beams in a combiner;
amplifying the summed, combined plurality of lower power downlink beams in a linearized high powered amplifier;
separating out the power amplified beams into separate beams; and
transmitting each separate beam with an associated downlink antenna.- View Dependent Claims (16, 17, 18, 19, 20)
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Specification