Multi-tone DGPS beacon transmitter and receiver

• US 5,745,075 A
• Filed: 06/05/1996
• Issued: 04/28/1998
• Est. Priority Date: 06/05/1996
• Status: Expired due to Term

• Current Assignee: Trimble Navigation Limited (Trimble Inc.)
• Original Assignee: Trimble Navigation Limited (Trimble Inc.)
• Inventors: Young, David W., Enge, Per K.
• Primary Examiner(s): Issing, Gregory C.
• Application Number:
  US08/658,484
• Time in Patent Office: 692 Days
• Field of Search: 342/357, 342/353, 342/367, 342/352, 455/59, 455/65
• US Class Current: 342/367
• CPC Class Codes: G01S 19/071 DGPS corrections
• CPC Class Codes: H04B 1/1081 Reduction of multipath noise by equalising H04B7/005
• CPC Class Codes: H04B 7/12 Frequency diversity

Abstract

An apparatus and a method for transmitting and receiving a signal having multiple tones for obviating destructive interference between a groundwave and a skywave of the signal. The multiple tones have a frequency offset that is calculated so that the destructive interference nulls for each of the tones occurs at different range distances from the transmitter thereby extending the distance over which at least one of the tones can be reliably received.

Claims

1. A method for obviating destructive interference between a groundwave and a skywave of a signal, comprising steps of:

transmitting a first signal having a first carrier frequency propagating from a transmitter as a first signal groundwave and a first signal skywave;

transmitting a second signal having a second carrier frequency having a frequency offset from said first carrier frequency, said second carrier frequency propagating from said transmitter as a second signal groundwave and a second signal skywave; and

using an ionospheric height for calculating said frequency offset for staggering first distances where destructive interference of said first signal groundwave and said first signal skywave occur from second distances where destructive interference between said second signal groundwave and said second signal skywave occur.

2. The method of claim 1, wherein:

the step of calculating said frequency offset includes a step of calculating said frequency offset for extending a range where said first and said second distances are staggered, said range beginning from said transmitter and continuous through an extended range.

3. The method of claim 2, wherein:

said frequency offset is approximately 2.9 kilohertz for providing said extended range for covering approximately between 150 and 600 kilometers from said transmitter.

4. The method of claim 1, wherein:

the step of calculating said frequency offset includes calculating said ionospheric height based upon a time of day.

5. The method of claim 1, wherein:

the step of transmitting said first signal includes a step of transmitting differential global positioning (DGPS) corrections with said first signal; and

the step of transmitting said second signal includes a step of transmitting said DGPS corrections with said second signal.

6. The method of claim 5, further including steps of:

receiving a GPS satellite signal in a GPS receiver having a GPS antenna; and

calculating said DGPS corrections based upon a difference between a known location of said GPS antenna and a GPS-derived location of said GPS antenna determined from information in said GPS satellite signal.

7. The method of claim 1, wherein:

said first signal includes a first DGPS beacon signal; and

said second signal includes a second DGPS beacon signal.

8. The method of claim 7, wherein:

said first DGPS beacon signal is a standard DGPS beacon signal.

9. A transmitter station for transmitting at least two signals for obviating destructive interference between a groundwave and a skywave of a signal for extending a selected range from the transmitter station, comprising:

a transmitter for transmitting a first signal and a second signal, said first signal propagating as a first signal groundwave and a first signal skywave and said second signal propagating as a second signal groundwave and a second signal skywave;

a first signal generator connected to the transmitter for providing said first signal having a first carrier frequency; and

a second signal generator connected to the transmitter for providing said second signal having a second carrier frequency differing from said first signal carrier frequency by a frequency offset, said frequency offset calculated from an ionospheric height for staggering first distances where destructive interference of said first signal groundwave and said first signal skywave occurs from second distances where destructive interference between said second signal groundwave and said second signal skywave occurs.

10. The transmitter station of claim 9, further including:

calculation means for calculating said ionospheric height and said frequency offset.

11. The transmitter station of claim 10, wherein:

the calculation means includes means for calculating said ionospheric height and said frequency offset based upon a time of day.

12. The transmitter station of claim 9, wherein:

said first signal includes differential global positioning (DGPS) corrections; and

said second signal includes said DGPS corrections.

13. The transmitter station of claim 12, further including:

a DGPS reference receiver having a known location for receiving a GPS satellite signal and providing said DGPS corrections.

14. The transmitter station of claim 9, wherein:

said first signal includes a first DGPS beacon signal; and

said second signal includes a second DGPS beacon signal.

15. The transmitter station of claim 14, wherein:

said first DGPS beacon signal is a standard DGPS beacon signal.

16. The transmitter station of claim 9, wherein:

said frequency offset is approximately 2.9 kilohertz for extending said selected range for covering approximately between 150 to 600 kilometers from the transmitter station.

17. A method for obviating destructive interference by receiving a multi-tone signal, comprising steps of:

receiving a first signal having information modulated onto a first carrier frequency, said first signal propagating from a transmitter as a first signal groundwave and a first signal skywave;

receiving a second signal having said information modulated onto a second carrier frequency, said second signal propagating from said transmitter as a second signal groundwave and a second signal skywave, said second carrier frequency differing from said first carrier frequency by a frequency offset calculated from an ionospheric height for staggering first distances from said transmitter where destructive interference of said first signal groundwave and said first signal skywave occur from second distances where destructive interference between said second signal groundwave and said second signal skywave occur; and

processing said first and said second signals for recovering said information from at least one of said first signal and said second signal.

18. The method of claim 17, wherein:

the step of processing said first and said second signals includes steps of;

measuring a signal strength for said first signal;

measuring a signal strength for said second signal;

selecting a strongest of said first and said second signal; and

demodulating said strongest signal.

19. The method of claim 17, wherein:

the step of processing said first and said second signals includes steps of;

measuring data integrity for said first signal;

measuring data integrity for said second signal;

selecting from said first and second signals a signal having a best data integrity; and

demodulating said signal having said best data integrity.

20. The method of claim 17, wherein:

the step of processing said first and said second signals includes steps of;

converting said first signal to a first intermediate signal having an intermediate frequency;

converting said second signal to a second intermediate signal having said intermediate frequency;

combining said first and said second intermediate signals; and

demodulating said combined signal.

21. The method of claim 17, wherein:

the step of processing said first and said second signals includes a step of;

alternately demodulating said first signal and said second signals.

22. The method of claim 17, wherein:

said information includes differential global positioning (DGPS) corrections.

23. The method of claim 22, wherein:

the step of processing said first and said second signals includes steps of;

tuning a phase loop to a first frequency corresponding to said first carrier frequency;

determining a signal strength of said first signal;

tuning a phase lock loop to a second frequency corresponding to said second carrier frequency;

determining a signal strength of said second signal;

selecting a strongest of said first and said second signals; and

recovering said differential global positioning system (DGPS) corrections from said strongest signal.

24. The method of claim 22, wherein:

the step of processing said first and said second signals includes steps of;

tuning a phase loop to a first frequency corresponding to said first carrier frequency;

determining a data integrity of said first signal;

tuning a phase lock loop to a second frequency corresponding to said second carrier frequency;

determining a data integrity of said second signal;

selecting a signal from said first and said second signals having a best data integrity; and

recovering said differential global positioning system (DGPS) corrections from said signal having said best data integrity.

25. The method of claim 22, further including the steps of:

receiving a GPS satellite signal in a GPS receiver having a GPS antenna; and

calculating a differentially corrected GPS-based location of said GPS antenna by correcting information in said GPS satellite signal with said DGPS corrections.

26. The method of claim 17, wherein:

said first signal includes a first DGPS beacon signal; and

said second signal includes a second DGPS beacon signal.

27. The method of claim 26, wherein:

said first DGPS beacon signal is a standard DGPS beacon signal.

28. A receiver for obviating destructive interference by receiving a multi-tone signal, comprising:

a first tuner for tuning to a first signal having information modulated onto a first carrier frequency propagating from a transmitter as a first signal groundwave and a first signal skywave;

a second tuner for tuning to a second signal having said information modulated onto a second carrier frequency propagating from said transmitter as a second signal groundwave and a second signal skywave, said second carrier frequency and said first carrier frequency having a frequency offset calculated from an ionospheric height for extending the range where destructive interference of said first signal groundwave and said first signal skywave and destructive interference between said second signal groundwave and said second signal skywave do not simultaneously occur; and

selection means coupled to the first and second tuners for selecting at least one of said first and said second signals for recovering said information.

29. The receiver of claim 28, wherein:

the selection means includes a signal strength detector for measuring a signal strength representative of each of said first and said second signal and means for selecting a strongest of said first and second signals for recovering said information.

30. The receiver of claim 28, wherein:

the selection means includes a data integrity code for measuring a data integrity representative of each of said first and said second signal and means for selecting one of said first and second signals having a best data integrity for recovering said information.

31. The receiver of claim 28, wherein:

the selection means includes a combiner for receiving a first intermediate signal representative of said first signal and a second intermediate signal representative of said second signal and providing a combination of said first and said second intermediate signals in a combined signal for recovering said information.

32. The receiver of claim 28, wherein:

the selection means includes means for alternating between said first and second signals for recovering said information.

33. The receiver of claim 28, wherein:

said information includes DGPS corrections.

34. The receiver of claim 33, further including:

a GPS receiver including a GPS antenna for receiving a GPS satellite signal coupled for receiving said DGPS corrections and providing a differentially corrected GPS-based location of said GPS antenna.

35. The receiver of claim 28, wherein:

said first signal includes a DGPS beacon signal; and

said second signal includes a DGPS beacon signal.

36. The receiver of claim 35, wherein:

said first DGPS beacon signal includes a standard DGPS beacon signal.