Method and system for determining the location of a sense antenna associated with a phased array communication system

• US 5,771,019 A
• Filed: 09/09/1996
• Issued: 06/23/1998
• Est. Priority Date: 09/09/1996
• Status: Expired due to Term

• Current Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Original Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Inventors: Berman, Arnold L., Wachs, Marvin R.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US08/709,957
• Time in Patent Office: 652 Days
• Field of Search: 342/127, 342/174, 342/360, 342/442
• US Class Current: 342/442
• CPC Class Codes: B64G 1/1007 Communications satellites
• CPC Class Codes: B64G 1/36 using sensors, e.g. sun-sensors, horizon sensors
• CPC Class Codes: B64G 1/66 Arrangements or adaptations of apparatus or instruments, not otherwise provided for
• CPC Class Codes: G01S 5/12 by co-ordinating position lines of different shape, e.g. hyperbolic, circular, elliptical or radial
• CPC Class Codes: H01Q 3/267 Phased-array testing or checking devices

Abstract

A method and system for determining an actual location of a sense antenna associated with a phased array communications satellite. A plurality of calibration carrier signals are transmitted at known frequencies. Each of the plurality of calibration carrier signals are received at a second frequency and compared with each of the plurality of transmitted calibration carrier signals. The actual location of the sense antenna is determined based on the comparison between the known frequency and the second frequency. The phased array communications satellite then broadcasts communication signals based on the actual location of the sense antenna rather than a desired location of the sense antenna.

Claims

1. A method for determining an actual location of a sense antenna associated with a phased array antenna of a satellite for broadcasting communication signals, the method comprising the steps of:

transmitting a plurality of calibration carrier signals each at a predetermined frequency from one of the sense antenna and the phased array antenna;

receiving each of the plurality of calibration carrier signals at a second frequency at the other one of the sense antenna and the phased array antenna;

comparing the second frequency of each of the plurality of received signals with the predetermined frequency of each of the plurality of transmitted calibration carrier signals; and

determining the actual location of the sense antenna relative to the phased array antenna based on the comparison between the predetermined frequency of each of the transmitted signals and the second frequency of each of the received signals utilizing triangulation techniques.

2. The method as recited in claim 1 wherein the step of comparing includes the step of determining a phase difference between each of the plurality of transmitted calibration carrier signals and each of the corresponding plurality of received signals.

3. The method as recited in claim 2 wherein the step of comparing further includes the step of determining a plurality of distances based on the determined phase differences.

4. The method as recited in claim 3 wherein the step of determining the actual location includes the step of determining a plurality of three dimensional hyperboloid surfaces based on the plurality of distances.

5. The method as recited in claim 4 wherein the step of determining the actual location further comprises the step of determining a point corresponding to the intersection of the plurality of three dimensional hyperboloid surfaces.

6. The method as recited in claim 1 further comprising the step of broadcasting the communication signals based on the determined actual location of the sense antenna.

7. The method as recited in claim 6 wherein the sense antenna has a desired location and wherein the step of broadcasting includes the step of determining a correction factor representing a difference between the actual location and the desired location of the sense antenna.

8. A system for determining an actual location of a sense antenna associated with a phased array antenna of a satellite for broadcasting communication signals and having a transmit phased array antenna and a receive phased array antenna, the system comprising:

a calibration carrier source in communication with the sense antenna and the phased array antenna for generating a plurality of calibration carrier signals each at a predetermined frequency for receipt by one of the sense antenna and the phased array antenna;

the sense antenna for transmitting the plurality of calibration carrier signals to the phased array antenna or for receiving the plurality of calibration carrier signals each at a second frequency from the phased array antenna;

the phased array antenna for transmitting the plurality of calibration carrier signals to the sense antenna for receiving the plurality of calibration carrier signals each at a third frequency from the sense antenna; and

a processor, coupled to the sense antenna and the calibration carrier source, for comparing the second and third frequencies of each of the plurality of received signals with the predetermined frequency of each of the corresponding plurality of transmitted calibration carrier signals to determine the actual location of the sense antenna relative to the phased array antenna based on the comparison and triangulation techniques.

9. The system as recited in claim 8 wherein the calibration carrier source includes a selection switch for sequentially transmitting each of the plurality of calibration carrier signals.

10. The system as recited in claim 8 wherein the processor determines a phase difference between each of the plurality of transmitted calibration carrier signals and each of the plurality of corresponding received signals.

11. The system as recited in claim 10 wherein the processor determines a plurality of distances based on the determined phase differences.

12. The system as recited in claim 11 wherein the processor determines a plurality of three dimensional hyperboloid surfaces based on the plurality of distances.

13. The system as recited in claim 12 wherein the processor determines a point corresponding to an intersection of the plurality of three dimensional hyperboloid surfaces.

14. The system as recited in claim 8 further comprising the phased array antenna for broadcasting the communication signals based on the determined actual location of the sense antenna.

15. The system as recited in claim 14 wherein the sense antenna has a desired location and wherein the processor determines a correction factor representing a difference between the actual location and the desired location of the sense antenna.

16. A communication satellite comprising:

a calibration carrier source for generating a plurality of calibration carrier signals each at a predetermined frequency;

a transmit phased array antenna, in communication with the calibration carrier source, having a first plurality of transmit array elements for transmitting a beam-formed signal wherein a second plurality of the first plurality of transmit array elements selectively transmit the plurality of calibration carrier signals;

a transmit sense antenna, in communication with the calibration carrier source, for receiving each of the plurality of calibration carrier signals transmitted by the second plurality of transmit array elements at a second frequency;

a receive phased array antenna, in communication with the calibration carrier source, having a first plurality of receive array elements for receiving a beam-formed signal wherein a second plurality of the first plurality of receive elements selectively receive the plurality of calibration carrier signals at a third frequency;

a receive sense antenna, in communication with the calibration carrier source, for transmitting each of the plurality of calibration carrier signals to the second plurality of receive array elements; and

a processor connected to the transmit sense antenna, the receive sense antenna, the second plurality of transmit array elements for comparing the second and third frequencies of each of the received signals with the predetermined frequency of each of the corresponding transmitted calibration carrier signals and for determining the actual location of the transmit sense antenna and the receive sense antenna relative to the phased array antenna based on the comparison and triangulation techniques.

17. The communications satellite as recited in claim 16 wherein the calibration carrier source includes a selection switch for sequentially transmitting the plurality of calibration carrier signals.

18. The communications satellite as recited in claim 16 wherein the communications satellite broadcasts communication signals based on the determined actual location of the transmit sense antenna and the receive sense antenna.

19. The communications satellite as recited in claim 18 wherein the transmit sense antenna and the receive sense antenna each has a desired location and wherein the communications satellite broadcasts communication signals based on a difference between the actual location and the desired location of each of the sense antennas.