GNSS local constellation/acquisition aiding system

• US 5,886,665 A
• Filed: 08/07/1997
• Issued: 03/23/1999
• Est. Priority Date: 08/07/1997
• Status: Expired due to Term

• Current Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rockwell International Corporation
• Inventors: Carlson, Stephen G., Dosh, Mervin K.
• Primary Examiner(s): Tarcza, Thomas
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US08/908,399
• Time in Patent Office: 593 Days
• Field of Search: 342/357, 342/352, 701/213, 455/12.1
• US Class Current: 342/357.42
• CPC Class Codes: G01S 19/11 wherein the cooperating elements are pseudolites or satellite radio beacon positioning system signal repeaters
• CPC Class Codes: G01S 19/235 Calibration of receiver components
• CPC Class Codes: G01S 19/46 the supplementary measurement being of a radio-wave signal type

Abstract

An apparatus and method are disclosed of providing position indicating signals to a GNSS receiver in an area of poor reception of satellite signals from the GNSS or when a dedicated system under local control is required. The method includes the steps of disposing a plurality of stationary transceivers proximate the area of poor reception and calculating a global position of each stationary transceiver based upon information contained within signals received from at least some satellites of the GNSS. The method further includes the steps of transmitting a local global positioning signal from each of the stationary transceivers to the GNSS receiver in the area of poor reception, such local global positioning signals including at least the global position of the transmitting stationary transceiver.

Claims

1. A method of providing position indicating signals to a GNSS receiver in an area of poor reception of satellite signals from the GNSS or when a dedicated system under local control is required, such method comprising the steps of:

disposing a plurality of stationary transceivers proximate the area of poor reception; and

transmitting a local global positioning signal from each of the stationary transceivers to the GNSS receiver in the area of poor reception, such local global positioning signals including at least a global position of the transmitting stationary transceiver.

2. The method of providing position indicating signals as in claim 1 further comprising calculating a global position of each stationary transceiver based upon information contained within signals received from at least some satellites of the GNSS.

3. The method of providing position indicating signals as in claim 1 further comprising including an identifier of each stationary transceiver in the local positioning signal.

4. The method of providing position indicating signals as in claim 1 further comprising synchronizing a reference clock of each stationary transceiver with a GNSS reference clock based upon a detected time of arrival of the signals received from the at least some satellites of the GNSS.

5. The method of providing position indicating signals as in claim 4 further comprising receiving almanac data from the at least some satellites of the plurality of satellites of the GNSS.

6. The method of providing position indicating signals as in claim 5 further comprising receiving ephemeris data from at least some satellites of the plurality of satellites of the GNSS.

7. The method of providing position indicating signals as in claim 6 wherein the step of calculating a global position of each stationary transceiver based upon information from a plurality of satellites of the GNSS further comprises determining a position of each of the at least some satellites using the received ephemeris data and a set of Kepler equations.

8. The method of providing a position indicating signal as in claim 7 wherein the step of calculating a global position of each stationary transceiver based upon information from a plurality of satellites of the GNSS further comprises determining a distance from each stationary transceiver and at least some satellites based upon a measured time difference between the GNSS reference clock and signals arriving from each of the at least some satellites of the GNSS.

9. The method of providing a position indicating signal as in claim 8 wherein the step of calculating a global position of each stationary transceiver based upon information from a plurality of satellites of the GNSS further comprises triangulating the position of each stationary transceiver based upon the position of each of at least some satellites and the measured distance of the satellite from each of the stationary transceivers.

10. Apparatus for providing position indicating signals to a GNSS receiver in an area of poor reception of satellite signals from the GNSS, such apparatus comprising:

a plurality of stationary transceivers proximate the area of poor reception;

means for calculating a global position of each stationary transceiver based upon information contained within signals received from at least some satellites of the GNSS; and

means for transmitting a local global positioning signal from each of the stationary transceivers to the GNSS receiver in the area of poor reception, such local global positioning signals including at least the global position of the transmitting stationary transceiver.

11. The apparatus for providing position indicating signals as in claim 10 further comprising means for including an identifier of each stationary transceiver in the local positioning signal.

12. The apparatus for providing position indicating signals as in claim 10 further comprising means for synchronizing a reference clock of each stationary transceiver with a GNSS reference clock based upon a detected time of arrival of the signals received from the at least some satellites of the GNSS.

13. The apparatus for providing position indicating signals as in claim 12 further comprising means for receiving almanac data from the at least some satellites of the plurality of satellites of the GNSS.

14. The apparatus for providing position indicating signals as in claim 13 further comprising means for receiving ephemeris data from the at least some satellites of the plurality of satellites of the GNSS.

15. The apparatus for providing position indicating signals as in claim 14 wherein the means for calculating a global position of each stationary transceiver based upon information from a plurality of satellites of the GNSS further comprises means for determining a position of each of the at least some satellites using the received ephemeris data and a set of Kepler equations.

16. The apparatus for providing a position indicating signal as in claim 15 wherein the means for calculating a global position of each stationary transceiver based upon information from a plurality of satellites of the GNSS further comprises means for determining a distance from each stationary transceiver and the at least some satellites based upon a measured time difference between the GNSS reference clock and signals arriving from each of the at least some satellites of the GNSS.

17. The apparatus for providing a position indicating signal as in claim 16 wherein the means for calculating a global position of each stationary transceiver based upon information from a plurality of satellites of the GNSS further comprises means for triangulating the position of each stationary transceiver based upon the position of each of the at least some satellites and the measured distance of the satellite from each of the stationary transceivers.

18. Apparatus for providing position indicating signals to a GNSS receiver in an area of poor reception of satellite signals from the GNSS, such apparatus comprising:

a plurality of stationary transceivers proximate the area of poor reception;

a GNSS position processor within each stationary transceiver of the plurality of stationary transceivers which calculates a global position of each stationary transceiver based upon information contained within signals received from at least some satellites of the GNSS; and

a communications processor which transmits a local global positioning signal from each of the stationary transceivers to the GNSS receiver in the area of poor reception, such local global positioning signals including at least the global position of the transmitting stationary transceiver.

19. The apparatus for providing position indicating signals as in claim 18 further comprising a multiplexer which multiplexes an identifier of each stationary transceiver into the local positioning signal.

20. The apparatus for providing position indicating signals as in claim 18 further comprising a phase comparator which synchronizes a local clock with a GNSS reference clock based upon a detected time of arrival of the signals received from the at least some satellites of the GNSS.

21. The apparatus for providing position indicating signals as in claim 20 further comprising an almanac buffer which receives almanac data from the at least some satellites of the plurality of satellites of the GNSS.

22. The apparatus for providing position indicating signals as in claim 21 further comprising an ephemeris buffer which receives ephemeris data from at least some satellites of the plurality of satellites of the GNSS.

23. The apparatus for providing position indicating signals as in claim 22 wherein the GNSS position processor which calculates a global position of each stationary transceiver based upon information from a plurality of satellites of the GNSS further comprises a trajectory processor which determines a position of each of the at least some satellites using the received ephemeris data and a set of Kepler equations.

24. The apparatus for providing a position indicating signal as in claim 23 wherein the GNSS position processor which calculates a global position of each stationary transceiver based upon information from a plurality of satellites of the GNSS further comprises propagation processor which determines a distance from each stationary transceiver and the at least some satellites based upon a measured time difference between the GNSS reference clock and signals arriving from each of the at least some satellites of the GNSS.

25. The apparatus for providing a position indicating signal as in claim 24 wherein the GNSS position processor which calculates a global position of each stationary transceiver based upon information from a plurality of satellites of the GNSS further comprises a triangulating processor which triangulates the position of each stationary transceiver based upon the position of each of the at least some satellites and the measured distance of the satellite from each of the stationary transceivers.