System and method for reducing VSAT apertures via satellite MIMO

• US 8,346,162 B1
• Filed: 09/25/2009
• Issued: 01/01/2013
• Est. Priority Date: 09/25/2009
• Status: Active Grant

• Current Assignee: Anuvu IP Holdings LLC
• Original Assignee: EMC Satcom Technologies Incorporated
• Inventors: Jayasimha, Sriram, Paladugula, Jyothendar
• Primary Examiner(s): GESESSE, TILAHUN
• Application Number:
  US12/567,246
• Time in Patent Office: 1,194 Days
• Field of Search: 455/12.1, 455/13.1, 455/13.2, 455/427, 455/428, 455/429
• US Class Current: 455/13.1
• CPC Class Codes: H04B 7/18521 Systems of inter linked satellites, i.e. inter satellite service for optical links between satellites H04B10/118

Abstract

A system and method of reducing VSAT apertures via satellite MIMO is disclosed. The system and method comprise a first hub antenna configured to receive a first return signal from and to transmit a first forward signal to a first adjacent satellite, a second hub antenna configured to receive a second return signal from and to transmit a second forward signal to a second adjacent satellite, and a hub station configured to determine time delay and frequency shift between the first return signal and the second return signal after they are received by the first hub antenna and the second hub antenna, and to apply the determined time delay and frequency shift to one of the first forward signal and the second forward signal prior to transmitting them so the first forward signal and the second forward signal are time- and frequency-aligned when received at the remote ground terminal via the first adjacent satellite and the second adjacent satellite, wherein the first return signal and the second return signal are transmitted from the remote ground terminal to the first hub antenna and the second hub antenna via the first adjacent satellite and the second adjacent satellite. Similar time- and frequency-aligning can be achieved at the remote ground terminal using polarized signals transmitted from the remote ground terminal.

Claims

1. A system for communicating with a remote ground terminal via a first satellite and a second satellite adjacent the fist satellite, the system comprising:

a first hub antenna configured to receive a first return signal from and to transmit a first forward signal to the first satellite;

a second hub antenna configured to receive a second return signal from and to transmit a second forward signal to the second satellite; and

a hub station configured to determine time delay and frequency shift between the first return signal and the second return signal after, and to apply the determined time delay and frequency shift to at least one of the first forward signal and the second forward signal so the first forward signal and the second forward signal are time- and frequency-aligned when received at the remote ground terminal via the first satellite and the second satellite,

wherein the first return signal and the second return signal are transmitted from the remote ground terminal to the first hub antenna and the second hub antenna via the first satellite and the second satellite.

2. The system of claim 1, wherein STC encoding is applied to the first forward signal and the second forward signal after the determined differential delay and frequency shift is applied to at least one of the first forward signal and the second forward signal.

3. The system of claim 1, wherein the remote ground terminal includes a reduced-aperture antennae that is pointed at a mid-point between the first satellite and the second satellite.

4. The system of claim 1, wherein the hub station includes a receiver with a diversity combiner and interference canceller for determining the time delay and frequency shift.

5. The system of claim 1, wherein the time delay and frequency shift are determined by using Binary Phase-Shift Keying (BPSK) to determine phase shift with blind estimation, tracking time delay and phase changes with a 2nd-order control loop, and resolving phase ambiguity with forward-error correction.

6. The system of claim 5, wherein the forward-error correction is performed by a Viterbi decoder.

7. The system of claim 1, wherein the first satellite and the second satellite have identical-band transponders.

8. The method of claim 7, wherein the identical-band transponders each have the same downlink power as a transponder in a single-satellite system.

9. A method for communicating with a remote ground terminal via a first satellite and a second satellite adjacent to the first satellite, the method comprising the steps of:

transmitting a return signal from the remote ground terminal to the first satellite and the second satellite;

re-transmitting the return signal from the first satellite as a first return signal;

re-transmitting the return signal from the second satellite as a second return signal;

receiving the fist return signal with a first hub antenna;

receiving the second return signal with a second hub antenna;

determining time delay and frequency shift between the first return signal and the second return signal after they are received with the first hub antenna and the second hub antenna; and

applying the determined time delay and frequency shift to at least one of a first forward signal and a second forward signal prior to transmitting the first forward signal with the first hub antenna and transmitting the second forward signal with the second hub antenna so the first forward signal and the second forward signal are time- and frequency-aligned when received at the remote ground terminal via the first satellite and the second satellite.

10. The method of claim 9, further comprising the step of applying STC encoding to the first forward signal and the second forward signal after the determined differential delay and frequency shift is applied to at least one of the first forward signal and the second forward signal.

11. The method of claim 9, further comprising the step of pointing a reduced-aperture antennae of the remote ground terminal at a mid-point between the first satellite and the second satellite.

12. The method of claim 9, wherein the step of determining differential delay and frequency shift includes estimating differential delay and frequency shift with a diversity combiner and interference canceller at a receiver at the first hub antenna and the second hub antenna.

13. The method of claim 9, wherein the step of determining differential delay and frequency shift includes using Binary Phase-Shift Keying (BPSK) to determine phase shift with blind estimation, tracking time delay and phase changes with a 2nd-order control loop, and resolving phase ambiguity with forward-error correction.

14. The method of claim 13, wherein the step of a resolving phase ambiguity with forward-error correction is performed by a Viterbi decoder.

15. The method of claim 9, wherein the first satellite and the second satellite have identical-band transponders.

16. The method of claim 15, wherein the identical-band transponders have the same downlink power as a transponder in a single-satellite system.

17. A system for communicating with a remote ground terminal via adjacent satellites comprising:

a remote ground terminal configured to send two or more first polarized signals to the adjacent satellites and to receive the two or more first polarized signals from the adjacent satellites when the adjacent satellites re-transmit the two or more first polarized signals,

wherein the remote ground terminal receives the re-transmitted two or more first polarized signals, determines differential delay and frequency shift between the re-transmitted two or more first polarized signals, and applies the determined differential delay and frequency shift to two or more subsequently received second polarized signals so the two or more subsequently received second polarized signals are time- and -frequency aligned for processing at the remote ground terminal.

18. The system of claim 17, wherein the two or more polarized signals are right- and left-handed circularly polarized signals.

19. The system of claim 17, wherein the remote ground terminal determines differential delay and frequency shift with a diversity combiner and interference canceller.

20. The system of claim 17, wherein cross-polarization discrimination (XPD) is minimized before diversity combining the two or more polarized signals.

21. The method of claim 17, wherein the two or more adjacent satellites include transponders configured to have different polarizations from one another.

22. The method of claim 21, wherein a first adjacent satellite includes a Global C-band A transponder and a second adjacent satellite includes a Global C-band B transponder.

23. The method of claim 17, wherein the remote ground terminal includes a reduced-aperture antenna with dual polarization transmitters and receivers.

24. A method for enabling reduced antenna aperture in a remote ground terminal, comprising the steps of:

sending two or more polarized signals from the remote ground terminal to two or more adjacent satellites;

receiving the two or more polarized first signals at the remote ground terminal when they are repeated for transmission by the two or more adjacent satellites;

determining differential delay and frequency shift between the repeated two or more polarized signals received at the remote ground terminal;

applying the determined differential delay and frequency shift to subsequently received signals from the two or more adjacent satellites to time- and frequency-align the subsequently received signals for processing at the remote ground terminal.

25. The method of claim 24, wherein the step of sending two or more polarized signals includes sending right- and left-handed circularly polarized signals.

26. The method of claim 24, wherein the step of determining differential delay and frequency shift includes estimating differential delay and frequency shift with a diversity combiner and interference canceller at the remote ground terminal.

27. The method of claim 24, further comprising the step of minimizing cross-polarization discrimination (XPD) before diversity combining the two or more polarized signals.

28. The method of claim 24, wherein the two or more adjacent satellites include transponders configured to have different polarizations from one another.

29. The method of claim 28, wherein a first adjacent satellite includes a Global C-band A transponder and a second adjacent satellite includes a Global C-band B transponder.

30. The method of claim 24, wherein the remote ground terminal includes a reduced-aperture antenna with dual polarization transmitters and receivers.

31. A for communicating with a remote ground terminal via adjacent satellites comprising the steps of:

sending a first polarized signal and a second polarized signal to the remote ground terminal from a first hub antenna and a second hub antenna via a first satellite and a second satellite adjacent to the first satellite, the first and second polarized signals each having a dominant component and an interference component;

auto-correlating the first and second polarized signals at the remote ground terminal to identify the dominant component in each of the first and second polarized signals;

determining the values for frequency shift and time delay between the dominant components of the first and second polarized signals;

time- and frequency-aligning the dominant component of the first polarized signal with the interference component of the second polarized signal and the dominant component of the second polarized signal with the interference component of the first polarized signal using the determined values for frequency shift and time delay;

cancelling the interference component of the second polarized signal from the time- and frequency-aligned dominant component of the first polarized signal;

cancelling the interference component of the first polarized signal from the time- and frequency-aligned dominant component of the second polarized signal; and

combining the dominant component of the first polarized signal with the dominant component of the second polarized signals after cancelling the interference components,

wherein the interference components of the first and second polarized signals are cancelled and the dominant components of the first and second polarized signals are combined using a plurality of interference cancellers that operate iteratively with one another.

32. The method of claim 31, further comprising a step of offsetting a repetition encoder'"'"'s output streams at the hub station by a fixed time that is slightly longer than a maximum time delay between the first and second polarized signals to ensure that the dominant component of the first polarized signal is received at the remote ground terminal later than the dominant component of the second polarized signal.

33. The method of claim 31, wherein the step of auto-correlating utilizes a time-frequency ambiguity function.

34. The method of claim 31, wherein the step of determining the values for frequency shift and time delay utilizes diversity combining and interference cancellation at the remote ground terminal.