Paired-beam transponder satellite communication

Patent metadata

Field	Value
Publication number	US-10284284-B2
Application number	US-201815925524-A
Country	US
Kind code	B2
Filing date	Mar 19, 2018
Priority date	Sep 4, 2012
Publication date	May 7, 2019
Grant date	May 7, 2019

Abstract

Systems and methods are described for paired-beam satellite communications in a flexible satellite architecture. Embodiments include one or more “bent pipe” satellites having multiple transponders for servicing a number of spot beams. Implementations include novel types of paired-beam transponders that communicatively couple gateway terminals and user terminals in different spot beams. Some implementations also include loopback transponders that communicatively couple gateway terminals and user terminals in the same spot beam. The transponders can use similar components, can provide for flexible forward-link and return-link spectrum allocation, and/or can provide other features. Certain embodiments further include support for utility gateway terminal service and/or redundancy (e.g., active spares) for one or more active components.

First claim

What is claimed is:

1. A method for satellite communications, the method comprising:
receiving, via a satellite transponder of a satellite, a first combined uplink signal in an uplink frequency band during a first time, the first combined uplink signal having a first ratio of forward-channel traffic to return-channel traffic according to a flexible allocation of forward-channel and return-channel portions of the uplink frequency band;
transmitting a first combined downlink signal during the first time, the first combined downlink signal corresponding to the first combined uplink signal translated to a downlink frequency band via a frequency translator of the satellite transponder;
receiving, via the satellite transponder, a second combined uplink signal in the uplink frequency band during a second time, the second combined uplink signal having a second ratio of the forward-channel traffic to the return-channel traffic according to the flexible allocation of forward-channel and return-channel portions of the uplink frequency band, wherein the second ratio is different than the first ratio;
transmitting a second combined downlink signal during the second time, the second combined downlink signal corresponding to the second combined uplink signal translated to the downlink frequency band via the frequency translator of the satellite transponder;
operating one or more switching components of the satellite in a normal mode during the first and second times; and
operating the one or more switching components of the satellite in a utility mode during a third time.

2. The method of claim 1 , wherein:
the receiving the first combined uplink signal during the first time comprises:
receiving a first gateway uplink signal in the uplink frequency band from a gateway terminal;
concurrently with receiving the first gateway uplink signal, receiving a first user uplink signal in the uplink frequency band from a plurality of user terminals; and
combining the first gateway uplink signal and the first user uplink signal to generate the first combined uplink signal; and

the transmitting the first combined downlink signal during the first time comprises:
transmitting the first combined downlink signal to the gateway terminal and to the plurality of user terminals.

3. The method of claim 2 , wherein the first gateway uplink signal and the first user uplink signal are combined non-coherently.

4. The method of claim 2 , wherein:
the forward-channel traffic is transmitted in the uplink frequency band by the gateway terminal via the first gateway uplink signal, and received in the downlink frequency band by plurality of user terminals via the first combined downlink signal; and
the return-channel traffic is transmitted in the uplink frequency band by the plurality of user terminals via the first user uplink frequency band, and received in the downlink frequency band by the gateway terminal via the first combined downlink signal.

5. The method of claim 2 , wherein:
the receiving the first gateway uplink signal and the receiving the first user uplink signal is via one or more feeds of the satellite; and
the transmitting the first combined downlink signal is via the one or more feeds of the satellite.

6. The method of claim 5 , wherein the satellite transponder comprises an input subsystem between the frequency translator and the one or more feeds of the satellite, and an output subsystem between the frequency translator and the one or more feeds of the satellite.

7. The method of claim 5 , wherein:
the one or more feeds is a loopback feed having a loopback beam coverage area;
the gateway terminal and the plurality of user terminals are located in the loopback beam coverage area of the loopback feed;
the receiving the first gateway uplink signal and the first user uplink signal is via the loopback feed;
the combining is via the loopback feed to generate the first combined uplink signal; and
the transmitting the first combined downlink signal is via the loopback feed.

8. The method of claim 1 , wherein the flexible allocation defines a first one or more sub-bands of the uplink frequency band and a first one or more sub-bands of the downlink frequency band to the forward-channel portions, and defines a second one or more sub-bands of the uplink frequency band and a second one or more sub-bands of the downlink frequency band to the return-channel portions.

9. The method of claim 1 , wherein the flexible allocation of forward-channel and return-channel portions of the uplink frequency band is according to a spread-spectrum scheme.

10. The method of claim 1 , wherein the downlink frequency band does not overlap the uplink frequency band.

11. The method of claim 1 , wherein:
the normal mode couples the satellite transponder to one or more feeds of the satellite; and
the utility mode further couples the satellite transponder to a utility gateway feed of the satellite.

12. The method of claim 11 , wherein the utility mode further decouples the satellite transponder from at least one of the one or more feeds of the satellite.

13. The method of claim 1 , wherein the one or more switching components comprises:
a first switching component to selectively couple the utility gateway feed to an input subsystem of the satellite transponder; and
a second switching component to selectively couple the utility gateway feed to an output subsystem of the satellite transponder.

14. The method of claim 1 , wherein:
operating the satellite transponder in the normal mode during the first and second times comprises:
receiving, during the first time, the first combined uplink signal comprising a first gateway uplink signal in the uplink frequency band from a gateway terminal and a first user uplink signal in the uplink frequency band from a plurality of user terminals;
transmitting, during the first time, the first combined downlink signal to the first gateway terminal and to the plurality of user terminals;
receiving, during the second time, the second combined downlink signal comprising a second gateway uplink signal in the uplink frequency band from the gateway terminal and a second user uplink signal in the uplink frequency band from the plurality of user terminals;
transmitting, during the second time, the second combined downlink signal to the gateway terminal and to the plurality of user terminals; and
operating the satellite transponder in the utility mode during the third time comprises:
receiving a utility gateway uplink signal in the uplink frequency band from a utility gateway terminal and a third user uplink signal in the uplink frequency band from the plurality of user terminals;
transmitting a utility gateway downlink signal to the utility gateway terminal, the utility gateway downlink signal corresponding to the third user uplink signal translated to the downlink frequency band; and
transmitting a user downlink signal to the plurality of user terminals, the user downlink signal corresponding to the utility gateway uplink signal translated to the downlink frequency band.

15. The method of claim 14 , wherein:
the gateway terminal and the plurality of user terminals are located in a loopback beam coverage area of a loopback feed of the satellite;
the utility gateway terminal is located outside the loopback beam coverage area;
the receiving the first combined uplink signal, the transmitting the first combined downlink signal, the receiving the second combined uplink signal, the transmitting the second combined downlink signal, and the transmitting the user downlink signal are each via the loopback feed; and

Assignees

• Viasat Inc

Inventors

• Mendelsohn Aaron J
• Miller Mark J

Classifications

• H04W74/006

  in the downlink, i.e. towards the terminal · CPC title

• H04B7/18517

  Transmission equipment in earth stations · CPC title

• H04B7/18513 Primary

  Transmission in a satellite or space-based system · CPC title

• H04B7/0408

  using two or more beams, i.e. beam diversity · CPC title

• H04B7/10

  Polarisation diversity; Directional diversity · CPC title