GEOPOSITIONING METHOD USING ASSISTANCE DATA

• US 20150268353A1
• Filed: 06/08/2015
• Published: 09/24/2015
• Est. Priority Date: 03/13/2009
• Status: Active Grant

• Current Assignee: Centre National D'Etudes Spatiales
• Original Assignee: Centre National D'Etudes Spatiales
• Inventors: LAURICHESSE, Denis, MERCIER, Flavien
• Granted Patent: US 9,851,447 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: G01S 19/04 providing carrier phase data
• CPC Class Codes: G01S 19/43 using carrier phase measurements, e.g. kinematic positioning; using long or short baseline interferometry
• CPC Class Codes: G01S 19/44 Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method

Abstract

A method for determining assistance data to facilitate processing of radio-navigation signals from a set of radio-navigational satellites of a reference network, each radio-navigational satellite broadcasting at least a first radio-navigation signal on a first frequency and a second radio-navigation signal on a second frequency, the second frequency being distinct from the first frequency, is provided.

Claims

1. A method for determining assistance data to facilitate processing of radio-navigation signals from a set of radio-navigational satellites of a reference network, each radio-navigational satellite broadcasting at least a first radio-navigation signal on a first frequency and a second radio-navigation signal on a second frequency, the second frequency being distinct from the first frequency, the method comprising:

recording, by the at least one signal receiver of the reference network, as radio-navigation signals any first radio-navigation signal and second radio-navigation signal broadcasted by each radio-navigational satellite;

deriving, by the at least one signal receiver, code and phase measurements from the said radio-navigation signals recorded, the phase measurements having ambiguities, each of which is an a priori unknown integer number of cycles;

resolving, by the at least one signal receiver, the ambiguities in the phase measurements on the first frequency in a same manner for all the satellites and reference receivers of the reference network to produce a resolution;

deducing, by the at least one signal receiver, a set of iono-free transmitter phase clock values arising from the resolution and a set of iono-free receiver phase clock values arising from the resolution;

calculating, by the at least one signal receiver, for each satellite-reference receiver pair, a carrier code shift combination value from the code and phase measurements for each respective satellite on the first frequency;

calculating, by the at least one signal receiver, a plurality of measurement residues based on the carrier code shift combination value, modelled a geometric contribution, a contribution of the iono-free receiver phase clock value, an iono-free transmitter phase clock value, and a contribution of the carrier code shift combination value;

separating, by the at least one signal receiver, in a same manner for all the satellites and receivers of the reference network, each of measurement residues into a transmitter part and a receiver part, and

smoothing, by the at least one signal receiver, the transmitter parts of the plurality of measurement residues.

2. The method according to claim 1, wherein the iono-free transmitter phase clock values associated with the resolution of the ambiguities as well as the smoothed transmitter parts are provided to receivers outside the reference network as assistance data.

3. The method according to claim 1, wherein the iono-free transmitter phase clock values associated with the resolution of the ambiguities as well as the smoothed transmitter parts are provided to receivers outside the reference network as assistance data over a telecommunications channel.

4. The method according to claim 1, further comprising:

calculating, by the at least one signal receiver, for each satellite of said set of satellites, a transmitter clock value associated with the carrier code shift combination as the sum of the iono-free transmitter phase clock value and the smoothed transmitter parts.

5. The method according to claim 4, wherein said transmitter clock values associated with the carrier code shift combination are provided to receivers outside the reference network as assistance data.

6. The method according to claim 4, wherein said transmitter clock values associated with the carrier code shift combination are provided to receivers outside the reference network as assistance data over a telecommunications channel.

7. The method according to claim 1, wherein the smoothing of the transmitter parts of the plurality of measurement residues is performed each time by fitting a sine function with a period of 12 hours to the transmitter parts of the plurality of measurement residues.

8. The method according to claim 1, wherein the first frequency is selected from a list including 1575.42 MHz, 1227.6 MHz, 1176.45 MHz, 1207.14 MHz, 1278.75 MHz, 1561.098 MHz, 1589.742 MHz, 1207.14 MHz, and 1268.52 MHz.

9. A computer program product comprising a non-transitory computer readable medium storing computer program code for determining assistance data to facilitate processing of radio-navigation signals from a set of radio-navigational satellites of a reference network, each radio-navigational satellite broadcasting at least a first radio-navigation signal on a first frequency and a second radio-navigation signal on a second frequency, the second frequency being distinct from the first frequency, the computer program code being executable by a processor of at least one signal receiver of the reference network to cause the processor to perform:

recording as radio-navigation signals any first radio-navigation signal and second radio-navigation signal broadcasted by each radio-navigational satellite;

deriving code and phase measurements from the said radio-navigation signals recorded, the phase measurements having ambiguities, each of which is an a priori unknown integer number of cycles;

resolving the ambiguities in the phase measurements on the first frequency in a same manner for all the satellites and reference receivers of the reference network to produce a resolution;

deducing a set of iono-free transmitter phase clock values arising from the resolution and a set of iono-free receiver phase clock values arising from the resolution;

calculating for each satellite-reference receiver pair, a carrier code shift combination value from the code and phase measurements for each respective satellite on the first frequency;

calculating plurality of measurement residues based on the carrier code shift combination value, a modelled geometric contribution, a contribution of the iono-free receiver phase clock value, an iono-free transmitter phase clock value, and a contribution of the carrier code shift combination value;

separating in a same manner for all the satellites and receivers of the reference network, each of measurement residues into a transmitter part and a receiver part, and

smoothing the transmitter part of the plurality of measurement residues.

10. The computer program product according to claim 9, wherein the iono-free transmitter phase clock values associated with the resolution of the ambiguities as well as the smoothed transmitter parts are provided to receivers outside the reference network as assistance data.

11. The computer program product according to claim 9, wherein the iono-free transmitter phase clock values associated with the resolution of the ambiguities as well as the smoothed transmitter parts are provided to receivers outside the reference network as assistance data over a telecommunications channel.

12. The computer program product according to claim 9, wherein the computer program code being executable by the processor of at least one signal receiver of the reference network to cause the processor to further perform:

calculating, by the at least one signal receiver, for each satellite of said set of satellites, a transmitter clock value associated with the carrier code shift combination as the sum of the iono-free transmitter phase clock value and the smoothed transmitter parts.

13. The computer program product according to claim 12, wherein said transmitter clock values associated with the carrier code shift combination are provided to receivers outside the reference network as assistance data.

14. The computer program product according to claim 12, wherein said transmitter clock values associated with the carrier code shift combination are provided to receivers outside the reference network as assistance data over a telecommunications channel.

15. The computer program product according to claim 9, wherein the smoothing of the transmitter parts of the plurality of measurement residues is performed each time by fitting a sine function with a period of 12 hours to the transmitter parts of the plurality of measurement residues.

16. The computer program product according to claim 9, wherein the first frequency is selected from a list including 1575.42 MHz, 1227.6 MHz, 1176.45 MHz, 1207.14 MHz, 1278.75 MHz, 1561.098 MHz, 1589.742 MHz, 1207.14 MHz, and 1268.52 MHz.

17. A system comprising radio-navigational satellites and at least one signal receiver, the at least one signal receiver configured to determine assistance data to facilitate processing of radio-navigation signals from a set of radio-navigational satellites of a reference network, each radio-navigational satellite broadcasting at least a first radio-navigation signal on a first frequency and a second radio-navigation signal on a second frequency, the second frequency being distinct from the first frequency, the at least one signal receiver configured to:

record as radio-navigation signals any first radio-navigation signal and second radio-navigation signal broadcasted by each radio-navigational satellite;

derive code and phase measurements from the said radio-navigation signals recorded, the phase measurements having ambiguities, each of which is an a priori unknown integer number of cycles;

resolve the ambiguities in the phase measurements on the first frequency in a same manner for all the satellites and reference receivers of the reference network to produce a resolution;

deduce a set of iono-free transmitter phase clock values arising from the resolution and a set of iono-free receiver phase clock values arising from the resolution;

calculate for each satellite-reference receiver pair, a carrier code shift combination value from the code and phase measurements for each respective satellite on the first frequency;

calculate plurality of measurement residues based on the carrier code shift combination value, a modelled geometric contribution, a contribution of the iono-free receiver phase clock value, an iono-free transmitter phase clock value, and a contribution of the carrier code shift combination value;

separate in a same manner for all the satellites and receivers of the reference network, each of measurement residues into a transmitter part and a receiver part, and

smooth the transmitter part of the plurality of measurement residues.

18. The system according to claim 17, wherein the iono-free transmitter phase clock values associated with the resolution of the ambiguities as well as the smoothed transmitter parts are provided to receivers outside the reference network as assistance data.

19. The system according to claim 17, wherein the iono-free transmitter phase clock values associated with the resolution of the ambiguities as well as the smoothed transmitter parts are provided to receivers outside the reference network as assistance data over a telecommunications channel.

20. The system according to claim 17, wherein the at least one signal receiver is further configured to:

calculate, for each satellite of said set of satellites, a transmitter clock value associated with the carrier code shift combination as the sum of the iono-free transmitter phase clock value and the smoothed transmitter parts.