Method and apparatus for time or frequency synchronization in non-geosynchronous satellite communication systems

• US 9,900,856 B2
• Filed: 09/23/2015
• Issued: 02/20/2018
• Est. Priority Date: 03/20/2015
• Status: Active Grant

• Current Assignee: Qualcomm, Inc.
• Original Assignee: Qualcomm, Inc.
• Inventors: Wu, Qiang, Black, Peter John
• Primary Examiner(s): Aung, Sai
• Application Number:
  US14/862,822
• Publication Number:
  US 20160278033A1
• Time in Patent Office: 881 Days
• CPC Class Codes: H04B 7/01 Reducing phase shift
• CPC Class Codes: H04B 7/18502 Airborne stations
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system
• CPC Class Codes: H04W 56/0015 one node acting as a reference for the others
• CPC Class Codes: H04W 56/0035 detecting errors in frequency or phase
• CPC Class Codes: H04W 56/0045 compensating for timing error by altering transmission time

Abstract

Method and apparatus for time or frequency synchronization of radio signals transmitted by user terminals in communication with a gateway through a satellite is provided. The satellite may be part of a non-synchronous satellite communication system, such as a low-earth orbit (LEO) satellite communication system for data, voice or video communications. Times of transmission of return link radio signals from the user terminals may be adjusted such that the signals arrive at the satellite or at the gateway without large time delay differentials. Carrier frequencies of return link radio signals transmitted from the user terminals may be adjusted such that the signals arrive at the satellite or at the gateway without large frequency offset differentials.

Claims

1. A method of controlling a time of transmission and radio frequency of a first signal at a first ground station that includes a first user terminal (UT) in communication with a non-geosynchronous satellite, the non-geosynchronous satellite further being in communication with a gateway, the method comprising:

computing a pre-correction time value based on a local time reference and a received signal or ephemeris of the non-geosynchronous satellite;

applying the pre-correction time value to adjust the time of transmission of the first signal at the first ground station;

computing a pre-correction frequency value based on a local frequency reference and the received signal or ephemeris of the non-geosynchronous satellite;

applying the pre-correction frequency value to adjust the radio frequency of the first signal at the first ground station; and

transmitting the first signal to the non-geosynchronous satellite in accordance with the time of transmission that is adjusted based on the pre-correction time value and the radio frequency that is adjusted based on the pre-correction frequency value,

wherein the pre-correction time value is configured to reduce a time-of-arrival (TOA) differential between a TOA of the first signal at the non-geosynchronous satellite and/or the gateway and one or more TOAs of one or more other signals from one or more other UTs at the non-geosynchronous satellite and/or the gateway,

wherein the pre-correction frequency value is configured to reduce a frequency offset differential between a radio frequency of the first signal at the non-geosynchronous satellite and/or the gateway and one or more radio frequencies of the one or more other signals from the one or more other UTs at the non-geosynchronous satellite and/or the gateway, or any combination thereof.

2. The method of claim 1, wherein the non-geosynchronous satellite is operable to communicate with at least a second UT among the one or more other UTs, and wherein the second UT is operable to transmit a second signal to the non-geosynchronous satellite.

3. The method of claim 2, wherein the gateway is operable to receive the first signal from the first UT and the second signal from the second UT through the non-geosynchronous satellite.

4. The method of claim 3, wherein the time of transmission of the first signal at the first UT is adjusted to reduce the TOA differential between TOAs of the first signal and the second signal at the gateway, and wherein the radio frequency of the first signal at the first UT is adjusted to reduce a difference between Doppler shifts of the first signal and the second signal at the gateway.

5. The method of claim 3, wherein a time of transmission of the second signal at the second UT is adjusted to reduce the TOA differential between TOAs of the first signal and the second signal at the gateway, and wherein a radio frequency of the second signal at the second UT is adjusted to reduce a difference between Doppler shifts of the first signal and the second signal at the gateway.

6. The method of claim 3, further comprising:

receiving, from the gateway, at least one command to advance or retard the time of transmission of the first signal at the first UT to reduce the TOA differential between TOAs of the first signal and the second signal at the gateway, and

receiving, from the gateway, at least one additional command to increase or decrease the radio frequency of the first signal at the first UT to reduce a difference between Doppler shifts of the first signal and the second signal at the gateway.

7. The method of claim 2, wherein the time of transmission of the first signal at the first UT is adjusted to reduce the TOA differential between TOAs of the first signal and the second signal at the non-geosynchronous satellite, and wherein a radio frequency of the second signal at the second UT is adjusted to reduce a difference between Doppler shifts of the first signal and the second signal at the non-geosynchronous satellite.

8. The method of claim 2, wherein a time of transmission of the second signal at the second UT is adjusted to reduce the TOA differential between TOAs of the first signal and the second signal at the non-geosynchronous satellite, and wherein a radio frequency of the second signal at the first UT is adjusted to reduce a difference between Doppler shifts of the first signal and the second signal at the non-geosynchronous satellite.

9. The method of claim 2, further comprising:

receiving, from the satellite, at least one command to advance or retard the time of transmission of the first signal at the first UT to reduce the TOA differential between TOAs of the first signal and the second signal at the non-geosynchronous satellite, and

receiving, from the satellite, at least one additional command to increase or decrease the radio frequency of the first signal at the first UT to reduce a difference between Doppler shifts of the first signal and the second signal at the non-geosynchronous satellite.

10. The method of claim 1, wherein the local time reference comprises a local global positioning system (GPS) time reference.

11. An apparatus configured to control a time of transmission and radio frequency of a first signal at a first ground station that includes a first user terminal (UT) in communication with a non-geosynchronous satellite, the non-geosynchronous satellite further being in communication with a gateway, the apparatus comprising:

at least one processor coupled to at least one transceiver and configured to;

compute a pre-correction time value based on a local time reference and a received signal or ephemeris of the non-geosynchronous satellite;

apply the pre-correction time value to adjust the time of transmission of the first signal at the first ground station;

compute a pre-correction frequency value based on a local frequency reference and the received signal or ephemeris of the non-geosynchronous satellite;

apply the pre-correction frequency value to adjust the radio frequency of the first signal at the first ground station; and

transmit the first signal to the non-geosynchronous satellite in accordance with the time of transmission that is adjusted based on the pre-correction time value and the radio frequency that is adjusted based on the pre-correction frequency value,

wherein the pre-correction time value is configured to reduce a time-of-arrival (TOA) differential between a TOA of the first signal at the non-geosynchronous satellite and/or the gateway and one or more TOAs of one or more other signals from one or more other UTs at the non-geosynchronous satellite and/or the gateway,

wherein the pre-correction frequency value is configured to reduce a frequency offset differential between a radio frequency of the first signal at the non-geosynchronous satellite and/or the gateway and one or more radio frequencies of the one or more other signals from the one or more other UTs at the non-geosynchronous satellite and/or the gateway, or any combination thereof.

12. The apparatus of claim 11, wherein the non-geosynchronous satellite is operable to communicate with at least a second UT among the one or more other UTs, and wherein the second UT is operable to transmit a second signal to the non-geosynchronous satellite.

13. The apparatus of claim 12, wherein the gateway is operable to receive the first signal from the first UT and the second signal from the second UT through the non-geosynchronous satellite.

14. The apparatus of claim 13, wherein the time of transmission of the first signal at the first UT is adjusted to reduce the TOA differential between TOAs of the first signal and the second signal at the gateway, and wherein the radio frequency of the first signal at the first UT is adjusted to reduce a difference between Doppler shifts of the first signal and the second signal at the gateway.

15. The apparatus of claim 13, wherein a time of transmission of the second signal at the second UT is adjusted to reduce the TOA differential between TOAs of the first signal and the second signal at the gateway, and wherein a radio frequency of the second signal at the second UT is adjusted to reduce a difference between Doppler shifts of the first signal and the second signal at the gateway.

16. The apparatus of claim 13, wherein the at least one processor is further configured to:

receive, from the gateway, at least one command to advance or retard the time of transmission of the first signal at the first UT to reduce the TOA differential between TOAs of the first signal and the second signal at the gateway, and

receive, from the gateway, at least one additional command to increase or decrease the radio frequency of the first signal at the first UT to reduce a difference between Doppler shifts of the first signal and the second signal at the gateway.

17. The apparatus of claim 12, wherein the time of transmission of the first signal at the first UT is adjusted to reduce the TOA differential between TOAs of the first signal and the second signal at the non-geosynchronous satellite, and wherein a radio frequency of the second signal at the second UT is adjusted to reduce a difference between Doppler shifts of the first signal and the second signal at the non-geosynchronous satellite.

18. The apparatus of claim 12, wherein a time of transmission of the second signal at the second UT is adjusted to reduce the TOA differential between TOAs of the first signal and the second signal at the non-geosynchronous satellite, and wherein a radio frequency of the second signal at the first UT is adjusted to reduce a difference between Doppler shifts of the first signal and the second signal at the non-geosynchronous satellite.

19. The apparatus of claim 12, wherein the at least one processor is further configured to:

receive, from the satellite, at least one command to advance or retard the time of transmission of the first signal at the first UT to reduce the TOA differential between TOAs of the first signal and the second signal at the non-geosynchronous satellite, and

receive, from the satellite, at least one additional command to increase or decrease the radio frequency of the first signal at the first UT to reduce a difference between Doppler shifts of the first signal and the second signal at the non-geosynchronous satellite.

20. An apparatus for controlling a time of transmission and radio frequency of a first signal at a first ground station that includes a first user terminal (UT) in communication with a non-geosynchronous satellite, the non-geosynchronous satellite further being in communication with a gateway, the apparatus comprising:

means for computing a pre-correction time value based on a local time reference and a received signal or ephemeris of the non-geosynchronous satellite;

means for applying the pre-correction time value to adjust the time of transmission of the first signal at the first ground station;

means for computing a pre-correction frequency value based on a local frequency reference and the received signal or ephemeris of the non-geosynchronous satellite;

means for applying the pre-correction frequency value to adjust the radio frequency of the first signal at the first ground station; and

means for transmitting the first signal to the non-geosynchronous satellite in accordance with the time of transmission that is adjusted based on the pre-correction time value and the radio frequency that is adjusted based on the pre-correction frequency value,

wherein the pre-correction time value is configured to reduce a time-of-arrival (TOA) differential between a TOA of the first signal at the non-geosynchronous satellite and/or the gateway and one or more TOAs of one or more other signals from one or more other UTs at the non-geosynchronous satellite and/or the gateway,

wherein the pre-correction frequency value is configured to reduce a frequency offset differential between a radio frequency of the first signal at the non-geosynchronous satellite and/or the gateway and one or more radio frequencies of the one or more other signals from the one or more other UTs at the non-geosynchronous satellite and/or the gateway, or any combination thereof.

21. The apparatus of claim 20, wherein the non-geosynchronous satellite is operable to communicate with at least a second UT among the one or more other UTs, and wherein the second UT is operable to transmit a second signal to the non-geosynchronous satellite.

22. The apparatus of claim 21, wherein the gateway is operable to receive the first signal from the first UT and the second signal from the second UT through the non-geosynchronous satellite.

23. The apparatus of claim 22, wherein the time of transmission of the first signal at the first UT is adjusted to reduce the TOA differential between TOAs of the first signal and the second signal at the gateway, and wherein the radio frequency of the first signal at the first UT is adjusted to reduce a difference between Doppler shifts of the first signal and the second signal at the gateway.

24. The apparatus of claim 21, wherein the time of transmission of the first signal at the first UT is adjusted to reduce the TOA differential between TOAs of the first signal and the second signal at the non-geosynchronous satellite, and wherein a radio frequency of the second signal at the second UT is adjusted to reduce a difference between Doppler shifts of the first signal and the second signal at the non-geosynchronous satellite.

25. A non-transitory computer-readable medium comprising instructions to cause a computer or processor to control a time of transmission and radio frequency of a first signal at a first ground station that includes a first user terminal (UT) in communication with a non-geosynchronous satellite, the non-geosynchronous satellite further being in communication with a gateway, the instructions comprising instructions to:

compute a pre-correction time value based on a local time reference and a received signal or ephemeris of the non-geosynchronous satellite;

apply the pre-correction time value to adjust the time of transmission of the first signal at the first ground station;

compute a pre-correction frequency value based on a local frequency reference and the received signal or ephemeris of the non-geosynchronous satellite;

apply the pre-correction frequency value to adjust the radio frequency of the first signal at the first ground station; and

transmit the first signal to the non-geosynchronous satellite in accordance with the time of transmission that is adjusted based on the pre-correction time value and the radio frequency that is adjusted based on the pre-correction frequency value,

wherein the pre-correction time value is configured to reduce a time-of-arrival (TOA) differential between a TOA of the first signal at the non-geosynchronous satellite and/or the gateway and one or more TOAs of one or more other signals from one or more other UTs at the non-geosynchronous satellite and/or the gateway,

wherein the pre-correction frequency value is configured to reduce a frequency offset differential between a radio frequency of the first signal at the non-geosynchronous satellite and/or the gateway and one or more radio frequencies of the one or more other signals from the one or more other UTs at the non-geosynchronous satellite and/or the gateway, or any combination thereof.

26. The non-transitory computer-readable medium of claim 25, wherein the non-geosynchronous satellite is operable to communicate with at least a second UT among the one or more other UTs, and wherein the second UT is operable to transmit a second signal to the non-geosynchronous satellite.

27. The non-transitory computer-readable medium of claim 26, wherein the gateway is operable to receive the first signal from the first UT and the second signal from the second UT through the non-geosynchronous satellite.

28. The non-transitory computer-readable medium of claim 27, wherein the time of transmission of the first signal at the first UT is adjusted to reduce the TOA differential between TOAs of the first signal and the second signal at the gateway, and wherein the radio frequency of the first signal at the first UT is adjusted to reduce a difference between Doppler shifts of the first signal and the second signal at the gateway.

29. The non-transitory computer-readable medium of claim 26, wherein the time of transmission of the first signal at the first UT is adjusted to reduce the TOA differential between TOAs of the first signal and the second signal at the non-geosynchronous satellite, and wherein a radio frequency of the second signal at the second UT is adjusted to reduce a difference between Doppler shifts of the first signal and the second signal at the non-geosynchronous satellite.