Differential global positioning system using radio data system

• US 5,477,228 A
• Filed: 04/13/1993
• Issued: 12/19/1995
• Est. Priority Date: 04/13/1993
• Status: Expired due to Term

• Current Assignee: Trimble Navigation Limited (Trimble Inc.)
• Original Assignee: Differential Corrections Inc (Trimble Inc.)
• Inventors: Haley, Ronald P., Tiwari, Anil, Weber, Lynn
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US08/042,491
• Time in Patent Office: 980 Days
• Field of Search: 342/357, 455/12.1
• US Class Current: 342/357.44
• CPC Class Codes: G01S 19/41 Differential correction, e.g. DGPS [differential GPS]

Abstract

Differential correction signals for a global positioning system (GPS), which operates with signals from a plurality of orbiting satellites, are provided in a first standard format, such as a RTCM SC-104 format, for each satellite in view of a reference receiver station. The differential correction signals include range error correction signals and range rate error correction information. The differential correction signals are then encoded according to a second standard format, such as the RDS format. The transmission time of the signals in the second standard format are then prioritized. A broadcast transmitter, such as a broadcast FM transmitter, is then modulated by the prioritized signals in the second standard format and a receiver receives and demodulates the broadcast signal. The broadcast prioritized signals in the second standard format are then decoded to provide differential correction signals in the first standard format. Various prioritization schemes are provided such as: prioritizing according to the maximum range acceleration rate for the various satellites; prioritizing according to the range acceleration rate for the various satellites exceeding a predetermined absolute value; prioritizing according to range error correction signals exceeding a predetermined absolute value; and prioritizing according to the range error or acceleration corrections signals for the various satellites. In addition to prioritizing, the RTCM signals is compressed and a 1/8 minute time clock is used to simplify processing at a user receiver.

Claims

1. A system for broadcasting differential correction signals for a global positioning system (GPS) which includes a plurality of orbiting satellites, comprising:

means for providing differential correction signals in a first standard format for various ones of a plurality of satellites;

means for converting said differential corrections signals in the first standard format to signals in a second standard format;

means for prioritizing the broadcast transmission time of the signals in the second standard format;

transmitter means for broadcasting a signal modulated by the prioritized signals in the second standard format;

receiver means for receiving and demodulating the broadcast signal modulated by the prioritized signals in the second standard format;

means for reconverting the broadcast prioritized signals in the second standard format to provide differential correction signals in the first standard format.

2. The system of claim 1 wherein the differential correction signals include range error correction signals and range rate error correction information.

3. The system of claim 2 wherein the means for prioritizing the transmission time of the signals in the second standard format includes means for prioritizing according to the maximum range acceleration rate for the various satellites.

4. The system of claim 2 wherein the means for prioritizing the transmission time of the signals in the second standard format includes means for prioritizing according to the range acceleration rate for the various satellites exceeding a predetermined absolute value.

5. The system of claim 2 wherein the means for prioritizing the transmission time of the signals in the second standard format includes means for prioritizing according to range error correction signals exceeding a predetermined absolute value.

6. The system of claim 2 wherein the means for prioritizing the transmission time of the signals in the second standard format includes means for prioritizing according to the range error corrections signals for the various satellites.

7. The system of claim 1 wherein the first standard format is a Radio Technical Commission for Maritime Services (RTCM) standard format for differential Navstar GPS services.

8. The system of claim 1 wherein the second standard format is a Radio Data Service (RDS) standard format.

9. The system of claim 1 wherein the transmitter means is an FM broadcast transmitter and wherein the receiver means is a FM receiver.

10. A system for broadcast transmitting differential correction signals for global positioning system GPS which includes a plurality of orbiting satellites, comprising:

means for providing differential correction signals in a first standard format for various ones of a plurality of satellites;

means for converting said differential corrections signals in the first standard format to guide in a second standard format;

means for prioritizing the transmission time of the signals in the second standard format;

transmission means for broadcasting a signal modulated by the prioritized signals in the second standard format.

11. The system of claim 10 wherein the differential correction signals include range error correction signals and range rate error correction information.

12. The system of claim 11 wherein the means for prioritizing the transmission time of the signals in the second standard format includes means for prioritizing according to the maximum range acceleration rate for the various satellites.

13. The system of claim 11 wherein the means for prioritizing the transmission time of the signals in the second standard format includes means for prioritizing according to the range acceleration rate for the various satellites exceeding a predetermined absolute value.

14. The system of claim 11 wherein the means for prioritizing the transmission time of the signals in the second standard format includes means for prioritizing according to range error correction signals exceeding a predetermined absolute value.

15. The system of claim 11 wherein the means for prioritizing the transmission time of the signals in the second standard format includes means for prioritizing according to the range error corrections signals for the various satellites.

16. The system of claim 10 wherein the first standard format is a Radio Technical Commission for Maritime Services (RTCM) standard format for differential Navstar GPS services.

17. The system of claim 10 wherein the second standard format is a Radio Data Service (RDS) standard format.

18. The system of claim 10 wherein the transmitter means is an FM broadcast transmitter and wherein the receiver means is a FM receiver.

19. A method for receiving information from a plurality of Global Positioning System (GPS) satellites and for rebroadcasting a selected portion of this information for receipt by selected recipients, the method comprising the steps of:

providing a GPS receiver/processor to receive GPS signals from K GPS satellites, consecutively numbered k=1, 2, . . . , K(K≧

2);

providing a transmitter connected to the GPS receiver/processor to rebroadcast selected GPS signals in each of a sequence of time intervals given by t_i <

t<

t_i+1, for receipt by selected recipients; and

using the transmitter to rebroadcast selected GPS signal range information received from satellite number k0 at a selected time t in the time interval t_i <

t<

t_i+1, where satellite number k=k0 is chosen according to a criterion based upon the range errors e_i,k and the range error rates v_i,k and range error accelerations a_i,k at the sequence of times {t_i }_i for each of the satellites k=1, 2, . . . , K.

20. The method of claim 19, wherein said criterion for choice of said satellite number k0 is

21. The method of claim 19, wherein said criterion for choice of said satellite number k0 is to rank the acceleration values in descending order and transmit satellite information in that order,

22. The method of claim 19, wherein said criterion for choice of said satellite number k0 is determined as follows:

determining a first range error for satellite number k at a selected time t in said time interval t_i <

t<

t_i+1 by the relation

space="preserve" listing-type="equation">e.sub.i,k (t)=e.sub.i,k (t.sub.i)+(t-t.sub.i)v.sub.i,k (t.sub.i);

determining a second range error for satellite number k at the selected time t by the relation

space="preserve" listing-type="equation">e.sub.i,k '"'"'(t)=e.sub.i-1,k +(t-t.sub.i-1 (v.sub.i-1,k (t.sub.i <

t<

t.sub.i+1);

for the selected time t, forming a difference

space="preserve" listing-type="equation">e.sub.i,k =e.sub.i,k (t)-e.sub.i,k '"'"'(t)

and comparing the magnitude |e_i,k | with a selected threshold e>

0; and

transmitting said present range information for all satellite numbers k for which |e_i,k |≧

e.

23. The method of claim 19, wherein said criterion for choice of said satellite number k0 is determined as follows:

determining a first range error for satellite number k at a selected time t in a time interval t_i <

t<

t_i+1 i by the relation

space="preserve" listing-type="equation">e.sub.i,k (t)=e.sub.i,k (t.sub.i)+(t-t.sub.i)v.sub.i,k (t.sub.i);

determining a second range error for satellite number k at the selected time t by the relation

space="preserve" listing-type="equation">e.sub.i,k '"'"'(t)=e.sub.i-1,k (t.sub.i-1)+(t-t.sub.i-1)v.sub.i-1,k (t.sub.i-1) (t.sub.i <

t<

t.sub.i+1);

for the selected time t, forming a difference

space="preserve" listing-type="equation">e.sub.i,k =e.sub.i,k (t)-e.sub.i,k '"'"'(t)

and comparing the magnitudes |e_i,k |;

rearranging the magnitudes |e_i,k |, fixed, in descending order as a sequence

space="preserve" listing-type="equation">|e.sub.i,k1 |≧

|e.sub.i,k2 |≧

|e.sub.i,k3 |≧

. . . ≧

|e.sub.i,kK |; and

for at least one pair of consecutive integers m and m+1 (1≦

m≦

K-1), transmitting said present range information for satellite number km before transmitting said present range information for satellite k=k(m+1).

24. A system for broadcasting differential correction signals for a global positioning system (GPS) which includes a plurality of orbiting satellites, comprising:

means for providing differential correction signals in a first standard format for various ones of a plurality of satellites, wherein the differential correction signals include range error correction signals and range rate error correction information;

means for converting said differential correction signals in the first standard format to signals in a second standard format;

means for prioritizing the broadcast transmission time of the signals in the second standard format, wherein the means for prioritizing the transmission time of the signals in the second standard format includes means for prioritizing according to the maximum range acceleration rate for the various satellites;

transmitter means for broadcasting a signal modulated by the prioritized signals in the second standard format;

receiver means for receiving and demodulating the broadcast signal modulated by the prioritized signals in the second standard format;

means for reconverting the broadcast prioritized signals in the second standard format to provide differential correction signals in the first standard format.

25. A system for broadcasting differential correction signals for a global positioning system (GPS) which includes a plurality of orbiting satellites, comprising:

means for providing differential correction signals in a first standard format for various ones of a plurality of satellites, wherein the differential correction signals include range error correction signals and range rate error correction information;

means for converting said differential correction signals in the first standard format to signals in a second standard format;

means for prioritizing the broadcast transmission time of the signals in the second standard format, wherein the means for prioritizing the transmission time of the signals in the second standard format includes means for prioritizing according to the range acceleration rate for the various satellites exceeding a predetermined absolute value;

transmitter means for broadcasting a signal modulated by the prioritized signals in the second standard format;

receiver means for receiving and demodulating the broadcast signal modulated by the prioritized signals in the second standard format;

means for reconverting the broadcast prioritized signals in the second standard format to provide differential correction signals in the first standard format.

26. A system for broadcasting differential correction signals for a global positioning system (GPS) which includes a plurality of orbiting satellites, comprising:

means for providing differential correction signals in a first standard format for various ones of a plurality of satellites, wherein the differential correction signals include range error correction signals and range rate error correction information;

means for converting said differential correction signals in the first standard format to signals in a second standard format;

means for prioritizing the broadcast transmission time of the signals in the second standard format, wherein the means for prioritizing the transmission time of the signals in the second standard format includes means for prioritizing according to range error correction signals exceeding a predetermined absolute value;

transmitter means for broadcasting a signal modulated by the prioritized signals in the second standard format;

receiver means for receiving and demodulating the broadcast signal modulated by the prioritized signals in the second standard format;

means for reconverting the broadcast prioritized signals in the second standard format to provide differential correction signals in the first standard format.

27. A system for broadcasting differential correction signals for a global positioning system (GPS) which includes a plurality of orbiting satellites, comprising:

means for providing differential correction signals in a first standard format for various ones of a plurality of satellites, wherein the differential correction signals include range error correction signals and range rate error correction information;

means for converting said differential correction signals in the first standard format to signals in a second standard format;

means for prioritizing the broadcast transmission time of the signals in the second standard format, wherein the means for prioritizing the transmission time of the signals in the second standard format includes means for prioritizing according to the range error corrections signals for the various satellites;

transmitter means for broadcasting a signal modulated by the prioritized signals in the second standard format;

receiver means for receiving and demodulating the broadcast signal modulated by the prioritized signals in the second standard format;

means for reconverting the broadcast prioritized signals in the second standard format to provide differential correction signals in the first standard format.

28. A system for broadcasting differential correction signals for a global positioning system (GPS) which includes a plurality of orbiting satellites, comprising:

means for providing differential correction signals in a first standard format for various ones of a plurality of satellites;

means for converting said differential correction signals in the first standard format to signals in a second standard format, wherein the second standard format is a Radio Data Service (RDS) standard format;

means for prioritizing the broadcast transmission time of the signals in the second standard format;

transmitter means for broadcasting a signal modulated by the prioritized signals in the second standard format;

receiver means for receiving and demodulating the broadcast signal modulated by the prioritized signals in the second standard format;

means for reconverting the broadcast prioritized signals in the second standard format to provide differential correction signals in the first standard format.

29. A system for broadcast transmitting differential correction signals for a global positioning system GPS which includes a plurality of orbiting satellites, comprising:

means for providing differential correction signals in a first standard format for various ones of a plurality of satellites;

means for converting said differential correction signals in the first standard format to provide signals in a second standard format, wherein the differential correction signals include range error correction signals and range rate error correction information;

means for prioritizing the broadcast transmission time of the signals in the second standard format, wherein the means for prioritizing the broadcast transmission time of the signals in the second standard format includes means for prioritizing according to the maximum range acceleration rate for the various satellites;

transmitter means for broadcasting a signal modulated by the prioritized signals in the second standard format.

30. A system for broadcast transmitting differential correction signals for a global positioning system GPS which includes a plurality of orbiting satellites, comprising:

means for providing differential correction signals in a first standard format for various ones of a plurality of satellites;

means for converting said differential correction signals in the first standard format to provide signals in a second standard format, wherein the differential correction signals include range error correction signals and range rate error correction information;

means for prioritizing the transmission time of the signals in the second standard format, wherein the means for prioritizing the transmission time of the signals in the second standard format includes means for prioritizing according to the range acceleration rate for the various satellites exceeding a predetermined absolute value;

transmitter means for broadcasting a signal modulated by the prioritized signals in the second standard format.

31. A system for broadcast transmitting differential correction signals for a global positioning system GPS which includes a plurality of orbiting satellites, comprising:

means for providing differential correction signals in a first standard format for various ones of a plurality of satellites;

means for converting said differential correction signals in the first standard format to provide signals in a second standard format, wherein the differential correction signals include range error correction signals and range rate error correction information;

means for prioritizing the transmission time of the signals in the second standard format, wherein the means for prioritizing the transmission time of the signals in the second standard format includes means for prioritizing according to range error correction signals exceeding a predetermined absolute value;

transmitter means for broadcasting a signal modulated by the prioritized signals in the second standard format.

32. A system for broadcast transmitting differential correction signals for a global positioning system GPS which includes a plurality of orbiting satellites, comprising:

means for providing differential correction signals in a first standard format for various ones of a plurality of satellites;

means for converting said differential correction signals in the first standard format to provide signals in a second standard format, wherein the differential correction signals include range error correction signals and range rate error correction information;

means for prioritizing the transmission time of the signals in the second standard format, wherein the means for prioritizing the transmission time of the signals in the second standard format includes means for prioritizing according to the range error corrections signals for the various satellites;

transmitter means for broadcasting a signal modulated by the prioritized signals in the second standard format.

33. A system for broadcast transmitting differential correction signals for a global positioning system GPS which includes a plurality of orbiting satellites, comprising:

means for providing differential correction signals in a first standard format for various ones of a plurality of satellites;

means for converting said differential correction signals in the first standard format to provide signals in a second standard format, wherein the second standard format is a Radio Data Service (RDS) standard format;

means for prioritizing the transmission time of the signals in the second standard format;

transmitter means for broadcasting a signal modulated by the prioritized signals in the second standard format.