LOCATION OF A DISTRESS BEACON

• US 20160003933A1
• Filed: 07/01/2015
• Published: 01/07/2016
• Est. Priority Date: 07/04/2014
• Status: Abandoned Application

• Current Assignee: Centre National D'Etudes Spatiales, Thales SA
• Original Assignee: Centre National D'Etudes Spatiales, Thales SA
• Inventors: CALMETTES, Thibaud Pierre Jean, PETCU, Emanuela Ana Maria, GREGOIRE, Yoan
• Application Number:
  US14/789,767
• Publication Number:
  US 20160003933A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: G01S 19/17 Emergency applications
• CPC Class Codes: G01S 19/42 Determining position
• CPC Class Codes: G01S 5/0072 Transmission between mobile stations, e.g. anti-collision systems
• CPC Class Codes: G01S 5/0081 Transmission between base stations
• CPC Class Codes: G01S 5/02213 Receivers arranged in a network for determining the position of a transmitter
• CPC Class Codes: G01S 5/0231 Emergency, distress or locator beacons
• CPC Class Codes: G01S 5/06 Position of source determined by co-ordinating a plurality of position lines defined by path-difference measurements G01S5/12 takes precedence
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system

Abstract

There is disclosed a computer implemented method for processing the signal emitted by a distress beacon, the signal being received by several satellites and forwarded to at least one ground station, the method comprising the steps consisting in determining a set of hypothetical positions of the beacon, and for at least one of the hypothetical positions, for each satellite, offsetting the signal received and forwarded as a function of the hypothetical position; summing the offset signals; and evaluating the validity of the sum of the offset signals as a function of the presence of a predefined characteristic in the sum. Developments describe aspects such as the temporal and/or frequency offsetting, the construction of a digital replica of the signal transmitted by the beacon, and as the minimizing of the weighted residues of the offsets. System aspects are described, including the calibration of an active antenna or an array of antennas.

Claims

1. A method implemented by a computer for processing the signal emitted by a distress beacon, said signal being received by several satellites and forwarded to at least one ground station, the method comprising the steps:

determining a set of hypothetical positions of the distress beacon; and

for at least one of the hypothetical positions;

for each satellite, offsetting the signal received and forwarded as a function of said hypothetical position;

summing the offset signals by coherent integration; and

evaluating the validity of the sum of the offset signals as a function of the presence of a predefined characteristic in said sum.

2. The method as claimed in claim 1, the step consisting in offsetting the signal from one satellite comprising a step consisting in offsetting the signal from said satellite temporally by a time that is equal to the opposite of the beacon-satellite-station propagation time.

3. The method as claimed in claim 1, the step consisting in offsetting the signal from one satellite comprising a step consisting in offsetting the signal from the satellite in terms of frequency by a frequency equal to the opposite of the Doppler effect.

4. The method as claimed in claim 1, the step consisting in offsetting the signal from a satellite comprising a step consisting in offsetting the signal in terms of power by a power equal to the opposite of the power attenuation measured for said satellite.

5. The method as claimed in claim 1, for which a characteristic of the transmitted signal comprises the presence of a pure carrier, and in which the validity of the sum of the offset signals from the satellites is determined by the appearance of a line in the Fourier transform of the summed signal.

6. The method as claimed in claim 1, for which the signal transmitted further comprises the presence of a synchronization signal, and for which the validity of the sum of the offset signals from the satellites is determined by correlation between the summed signal and a replica of said synchronization signal.

7. The method as claimed in claim 6, for which correlation is obtained for a particular temporal and frequency offset between said signal obtained by summing the offset signals from the satellites and said replica of the synchronization word.

8. The method as claimed in claim 1, a characteristic of the emitted signal being obtained by combining an initial message and a spread code, and the validity of the sum of the offset signals from the satellites being determined by correlation between the summed signal and a replica of the spread code.

9. The method as claimed in claim 8, the correlation being determined for a particular temporal and frequency offset between the summed signal and the replica of the spread code.

10. The method as claimed in claim 1, further comprising, for each satellite, a step consisting in determining a time offset and a frequency offset that maximize the correlation between the signal received from this satellite and the summed signal corresponding to the sum of the offset signals from the satellites that is determined as being valid.

11. The method as claimed in claim 1, further comprising, for each sum of offset signals from the satellites which is determined as being valid, a step consisting in determining the binary content of the signal transmitted by the beacon, relayed by the satellites and received by the station.

12. The method as claimed in claim 1, further comprising, for each sum of offset signals from the satellites which is determined as being valid, after the step consisting in determining the binary content of the signal transmitted by the beacon, a step consisting in constructing a baseband digital replica of the signal transmitted by the distress beacon.

13. The method as claimed in claim 1, further comprising, for each satellite, a step consisting in determining a time offset and a frequency offset that maximize the correlation between the signal received from this satellite and the digital replica after a step consisting in demodulating the coherent composition.

14. The method as claimed in claim 1, further comprising a step consisting in determining the location of the distress beacon, said location minimizing the weighted residue of the time offsets or the weighted residue of the frequency offsets, or the combined weighted residue of the time offsets and of the frequency offsets between the satellites.

15. The method as claimed in claim 14, further comprising a step consisting in calibrating an active antenna or an array of antennas as a function of the location of the distress beacon.

16. The method as claimed in claim 11, further comprising a step consisting in creating an alert bulletin comprising the demodulated content of the signal transmitted by the beacon and/or the determined location of the distress beacon.

17. The method as claimed in claim 1, comprising beforehand a step consisting in removing the contribution of the downlink between the satellite and the ground station or stations.

18. The method as claimed in claim 1, the set of hypothetical positions of the distress beacon being reduced to the positions visible from the satellites visible from the ground receiving station.

19. A computer program product, said computer program comprising code instructions for carrying out the steps of the method as claimed in claim 1 when said program is executed on a computer.

20. A system for locating a distress beacon, the system comprising means for implementing the steps of the method as claimed in claim 1.

21. The system as claimed in claim 20, comprising at least one active antenna or an array of antennas.