High throughput satellite system with optical feeder uplink beams and RF service downlink beams
View Patent ↗Described herein are ground based subsystems, and related methods, for use in transmitting an optical feeder uplink beam to a satellite that is configured to receive the optical feeder uplink beam and in dependence thereon produce and transmit a plurality of RF service downlink beams within a specified RF frequency range to service terminals. Also described herein are space based subsystems of a satellite, and related methods, for use in transmitting a plurality of RF service downlink beams within a specified RF frequency range to service terminals. Beneficially certain embodiments eliminate the need for any frequency down-converters or any other type of frequency conversion equipment in a space segment forward link equipment. Also described herein is space segment return link equipment, and related methods, for use in transmitting an optical feeder downlink beam to a ground based subsystem, as well as ground based return link equipment thereof.
1. A ground based subsystem for use in transmitting an optical feeder uplink beam to a satellite that is configured to receive the optical feeder uplink beam and in dependence thereon produce and transmit a plurality of RF service downlink beams within a specified RF frequency range to service terminals, the ground based subsystem comprising:
a plurality of lasers, each of the lasers operable to emit an optical signal having a different peak wavelength within a specified optical wavelength range;
a plurality of electro-optical modulators (EOMs), each of the EOMs configured to receive an optical signal from a respective one of the plurality of lasers, receive a different data modulated RF carrier signal that has been modulated to carry data for at least one of the plurality of RF service downlink beams, and output an optical data signal carrying data for at least one of the plurality of RF service downlink beams and having an RF frequency within the same specified RF frequency range within which the satellite is configured to transmit the plurality of RF service downlink beams;
a wavelength-division multiplexing (WDM) multiplexer configured to receive the optical data signals output by the plurality of EOMs, and combine the plurality of optical data signals into a wavelength division multiplexed optical signal;
an optical amplifier configured to amplify the wavelength division multiplexed optical signal to thereby produce an optically amplified wavelength division multiplexed optical signal; and
transmitter optics configured to receive the optically amplified wavelength division multiplexed optical signal and transmit an optical feeder uplink beam to the satellite in dependence thereon;
wherein because RF frequencies of the optical data signals output by the plurality of EOMs are within the same specified RF frequency range within which the satellite is configured to transmit the plurality of RF service downlink beams, there is an elimination of any need for the satellite to perform any frequency conversions when producing the plurality of RF service downlink beams in dependence on the optical feeder uplink beam.
2. The subsystem of claim 1 , further comprising:
a plurality of RF modulators configured to produce the data modulated RF carrier signals that are received by the plurality of EOMs;
wherein each of the RF modulators receives an RF carrier signal having an RF frequency within the same specified RF frequency range within which the satellite is configured to transmit the plurality of RF service downlink beams.
3. The subsystem of claim 2 , further comprising:
one or more oscillators configured to produce the RF carrier signals that are provided to the RF modulators, each of the RF carriers signals having an RF frequency within the same specified RF frequency range within which the satellite is configured to transmit the plurality of RF service downlink beams.
4. The subsystem of claim 1 , further comprising:
a plurality of RF modulators that are each used to produce a data modulated RF signal within the same specified RF frequency range within which the satellite is configured to transmit the plurality of RF service downlink beams;
a plurality of frequency division multiplexers that are each configured to receive the data modulated RF signals from at least two of the RF modulators and frequency multiplex the received modulated RF signals to produce one of the data modulated RF carrier signals that are received by the EOMs; and
one or more oscillators configured to produce the RF carrier signals that are provided to the RF modulators, each of the RF carriers signals having an RF frequency within the same specified RF frequency range within which the satellite is configured to transmit the plurality of RF service downlink beams.
5. The subsystem of claim 1 , wherein:
each of the EOMs is configured to output an optical data signal carrying data for at least two of the plurality of RF service downlink beams.
6. The subsystem of claim 1 , wherein the specified RF frequency range within which the satellite is configured to produce and transmit the plurality of RF service downlink beams comprises a downlink portion of the Ka band.
7. The subsystem of claim 6 , wherein the downlink portion of the Ka band is from 17.7 GHz to 20.2 GHz, and thus, has a bandwidth of 2.5 GHz.
8. The subsystem of claim 6 , wherein the downlink portion of the Ka band is from 17.3 GHz to 20.2 GHz, and thus, has a bandwidth of 2.9 GHz.
9. The subsystem of claim 1 , wherein the specified optical wavelength range is a contiguous optical wavelength range within an infrared (IR) spectrum.
10. The subsystem of claim 1 , wherein the specified optical wavelength range is a non-contiguous optical wavelength range within an infrared (IR) spectrum.
11. A method for enabling a ground based subsystem to produce and transmit an optical feeder uplink beam to a satellite that is configured to receive the optical feeder uplink beam and in dependence thereon produce and transmit a plurality of RF service downlink beams within a specified RF frequency range to service terminals, the method for use by the ground based subsystem comprising:
emitting a plurality of optical signals each having a different peak wavelength that is within a specified optical wavelength range;
electro-optically modulating each of the optical signals with one of a plurality of different data modulated RF carrier signals, each of which has been modulated to carry data for at least one of the plurality of RF service downlink beams, to thereby produce a plurality of optical data signals, each of which carries data for at least one of the plurality of RF service downlink beams and has an RF frequency within the same specified RF frequency range within which the satellite is configured to transmit the plurality of RF service downlink beams;
multiplexing the plurality of optical data signals to thereby produce a wavelength division multiplexed optical signal that includes data for the plurality of RF service downlink beams;
producing an optical feeder uplink beam, in dependence on the wavelength division multiplexed optical signal; and
transmitting the optical feeder uplink beam through free-space to the satellite;
wherein because RF frequencies of the optical data signals produced during the electro-optically modulating are within the same specified RF frequency range within which the satellite is configured to transmit the plurality of RF service downlink beams, there is an elimination of any need for the satellite to perform any frequency conversions when producing the plurality of RF service downlink beams in dependence on the optical feeder uplink beam.
12. The method of claim 11 , further comprising:
receiving a plurality of RF carrier signals each of which has a different RF frequency within the same specified RF frequency range within which the satellite is configured to transmit the plurality of RF service downlink beams; and
producing the data modulated RF carrier signals, which are electro-optically modulated with the optical signals, in dependence on the plurality of RF carrier signals.
13. The method of claim 11 , wherein the specified RF frequency range within which the satellite is configured to produce and transmit the plurality of RF service downlink beams comprises a downlink portion of the Ka band.
14. The method of claim 13 , wherein the downlink portion of the Ka band is from 17.7 GHz to 20.2 GHz, and thus, has a bandwidth of 2.5 GHz.
15. The method of claim 13 , wherein the downlink portion of the Ka band is from 17.3 GHz to 20.2 GHz, and thus, has a bandwidth of 2.9 GHz.
16. A space based subsystem of a satellite for use in transmitting a plurality of RF service downlink beams within a specified RF frequency range to service terminals, the space based subsystem comprising:
receiver optics configured to receive an optical feeder uplink beam from a ground based subsystem;
an optical amplifier optically coupled to the receiver optics and configured to amplify an optical feeder uplink signal that is output from the receiver optics;
a wavelength-division multiplexing (WDM) demultiplexer optically coupled to the optical amplifier and configured to separate the amplified optical feeder uplink signal, which is output from the optical amplifier, into a plurality of separate optical signals that each have a different peak wavelength; and
a plurality of photodetectors, each of which converts a different one of the optical signals that are output from the WDM demultiplexer, to a respective electrical data signal having an RF frequency within the same specified RF frequency range within which the space based subsystem is configured to transmit the plurality of RF service downlink beams; and
RF components and antennas configured to produce and transmit, in dependence on the electrical data signals generated by the plurality of PDs, the plurality of RF service downlink beams within the specified RF frequency range;
wherein because the RF frequencies of the electrical data signals output by the plurality of photodetectors are within the same specified RF frequency range within which the space based subsystem is configured to transmit the plurality of RF service downlink beams, there is an elimination of any need for the space based subsystem to perform any frequency conversions when producing the plurality of RF service downlink beams in dependence on the optical feeder uplink beam.
17. The subsystem of claim 16 , wherein the specified RF frequency range within which the satellite is configured to produce and transmit a plurality of RF service downlink beams comprises a downlink portion of the Ka band.
18. The subsystem of claim 17 , wherein the downlink portion of the Ka band is from 17.7 GHz to 20.2 GHz, and thus, has a bandwidth of 2.5 GHz.
19. The subsystem of claim 17 , wherein the downlink portion of the Ka band is from 17.3 GHz to 20.2 GHz, and thus, has a bandwidth of 2.9 GHz.
20. The subsystem of claim 16 , wherein the specified optical wavelength range is either a contiguous, or a non-contiguous, optical wavelength range within an infrared (IR) spectrum.
21. A method for enabling a space based subsystem of a satellite to produce and transmit a plurality of RF service downlink beams within a specified RF frequency range to service terminals, the method for use by the space based subsystem comprising:
receiving an optical feeder uplink beam from a ground based subsystem;
producing, in dependence on the received optical feeder uplink beam, a plurality of separate optical signals that each have a different peak wavelength;
converting each of the separate optical signals into a respective electrical data signal having an RF frequency within the same specified RF frequency range within which the space based subsystem is configured to transmit the plurality of RF service downlink beams;
producing, in dependence on the electrical data signals, the plurality of RF service downlink beams within the specified RF frequency range; and
transmitting the plurality of RF service downlink beams within the specified RF frequency range;
wherein because the RF frequencies of the electrical data signals resulting from the converting are within the same specified RF frequency range within which the space based subsystem is configured to transmit the plurality of RF service downlink beams, there is an elimination of any need for the space based subsystem to perform any frequency conversions when producing the plurality of RF service downlink beams in dependence on the optical feeder uplink beam.
22. The method of claim 21 , wherein the specified RF frequency range within which the satellite is configured to produce and transmit a plurality of RF service downlink beams comprises a downlink portion of the Ka band.
23. The method of claim 22 , wherein the downlink portion of the Ka band is from 17.7 GHz to 20.2 GHz, and thus, has a bandwidth of 2.5 GHz.
24. The method of claim 22 , wherein the downlink portion of the Ka band is from 17.3 GHz to 20.2 GHz, and thus, has a bandwidth of 2.9 GHz.
25. The method of claim 21 , wherein the specified optical wavelength range is either a contiguous, or a non-contiguous, optical wavelength range within an infrared (IR) spectrum.