Methods of reducing interference including determination of feeder link signal error and related systems

• US 7,890,050 B2
• Filed: 03/09/2009
• Issued: 02/15/2011
• Est. Priority Date: 03/15/2005
• Status: Expired due to Fees

• Current Assignee: ATC Technology Corporation (FedEx Corporation)
• Original Assignee: ATC Technology Corporation (FedEx Corporation)
• Inventors: Karabinis, Peter D.
• Primary Examiner(s): Anderson; Matthew D
• Assistant Examiner(s): Aminzay; Shaima Q
• Application Number:
  US12/400,143
• Publication Number:
  US 20090170427A1
• Time in Patent Office: 708 Days
• Field of Search: 455/12.1, 455/3.02, 455/3.01, 455/63.1, 455/9, 455 131- 133, 455/67.13, 455/414.1, 455/422.1, 455427-430, 455/455, 455/500, 455/501, 455/562.1, 370/310, 370/316, 370/317, 375/130, 375/133, 375/144, 375/148, 375/346, 342/354
• US Class Current: 455/12.1
• CPC Class Codes: H04B 7/1851 Systems using a satellite or space-based relay H04B7/18508, H04B7/18521 take precedence; providing specific services H04B7/18523 - H04B7/18576
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system

Abstract

Methods of reducing interference in a satellite communications system may include receiving a plurality of feeder link signals and time aligning the plurality of feeder link signals to provide time aligned feeder link signals. At least two of the time aligned feeder link signals may be combined to provide reduced interference of at least one of the feeder link signals. Related systems are also discussed.

Claims

1. A method of reducing interference in a satellite communications system defining a feeder link between a Space-Based Component (SBC) and Ground Based Equipment (GBE), the method comprising:

determining an error of a received feeder link signal communicated over the feeder link between the Space-Based Component (SBC) and the Ground Based Component (GBE);

pre-distorting a first feeder link signal responsive to the error of the received feeder link signal; and

transmitting the pre-distorted first feeder link signal over the feeder link between the Space-Based Component (SBC) and the Ground Based Equipment;

wherein pre-distorting the first feeder link signal responsive to the error comprises combining a measure of the first feeder link signal with a measure of a second feeder link signal that is correlated with the error of the received feeder link signal.

2. A method according to claim 1 wherein transmitting the pre-distorted first feeder link signal comprises transmitting the pre-distorted first feeder link signal to the Space-Based Component (SBC) and determining an error of a received feeder link signal comprises determining an error at the SBC.

3. A method according to claim 1 wherein transmitting the pre-distorted first feeder link signal comprises transmitting the pre-distorted first feeder link signal to the Ground Based Equipment (GBE) and determining an error of a received feeder link signal comprises determining an error at the GBE.

4. A method according to claim 1 wherein the received feeder link signal includes an information component, and wherein determining an error of the received feeder link signal comprises comparing the information component with at least one value of the received feeder link signal.

5. A method according to claim 4 wherein the information component is compared with the at least one value at the Space-Based Component (SBC), and wherein a result of the comparison is transmitted from the SBC.

6. A method according to claim 4 wherein the information component is compared with the at least one value at the Ground-Based Equipment (GBE), and wherein a result of the comparison is transmitted from the GBE.

7. A method according to claim 4 wherein the information component comprises a-priori known information.

8. A satellite communications system comprising:

a processor configured to provide an error of a feeder link signal; and

an interference reducer configured to reduce interference of the feeder link signal responsive to the error;

wherein the interference reducer is further configured to calculate a weight to be applied to a second feeder link signal to provide an error correction signal, and to combine the error correction signal with a measure of the feeder link signal;

wherein the processor is further configured to provide a second error of a second feeder link signal, and the interference reducer is further configured to calculate a second weight to be applied to the feeder link signal to provide a second error correction signal and to combine the second error correction signal with a measure of the second feeder link signal.

9. A satellite communications system according to claim 8 wherein the feeder link signal and the second feeder link signal are received via spatially diverse paths and/or different antenna patterns.

10. A satellite communications system according to claim 8 wherein the feeder link signal and the second feeder link signal are transmitted via spatially diverse paths and/or different antenna patterns.

11. A satellite communications system according to claim 8 wherein the processor and/or the interference reducer is/are at a Space-Based Component (SBC) and/or at a Ground-Based Equipment (GBE).

12. A satellite communications system according to claim 8 wherein the feeder link signal includes an information component, and wherein providing the error of the feeder link signal comprises comparing the information component with at least one value of the feeder link signal.

13. A satellite communications system according to claim 12 wherein the information component is compared with the at least one value at a Space-Based Component (SBC) and/or at a Ground-Based Equipment (GBE).

14. A satellite communications system according to claim 13 wherein a result of the comparison is transmitted to a Space-Based Component (SBC) and/or to a Ground-Based Equipment (GBE).

15. A satellite communications system according to claim 12 wherein the information component comprises a-priori known information.