Apparatus and method for coupling satellite navigation signals to a VOR system

• US 5,801,659 A
• Filed: 12/17/1996
• Issued: 09/01/1998
• Est. Priority Date: 12/17/1996
• Status: Expired due to Fees

• Current Assignee: Dytech Corporation Ltd. (Dyson Group Plc)
• Original Assignee: Dytech Corporation Ltd. (Dyson Group Plc)
• Inventors: Helfrick, Albert
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US08/768,819
• Time in Patent Office: 623 Days
• Field of Search: 342/49, 342/401, 342/404, 342/46, 342/357
• US Class Current: 342/357.4
• CPC Class Codes: G01S 1/026 of associated receivers
• CPC Class Codes: G01S 19/15 Aircraft landing systems

Abstract

A navigation and control apparatus having a link to a GPS device for receiving positional and navigational data therefrom, a converter to convert the GPS signals into a VOR format, and a VOR signal generator to transmit the converted signals to a VOR receiver aboard the aircraft.

Claims

1. An onboard aircraft navigation apparatus for coupling signals received by a Global Navigation Satellite System (GNSS) device to a conventional VOR receiver aboard said aircraft, said navigation apparatus comprising:

(a) signal linking means to said GNSS device for receiving GNSS signals therefrom;

(b) converting means for converting said GNSS signals into VOR signals; and

(c) a VOR signal generator for transmitting said VOR signals to said conventional VOR receiver.

2. The aircraft navigation apparatus as claimed in claim 1, wherein said GNSS signals are from a Global Satellite Positioning System.

3. The aircraft navigation apparatus as claimed in claim 1, wherein said GNSS signals are in RTCM format.

4. The aircraft navigation apparatus as claimed in claim 1, wherein said signal linking means is a serial data line.

5. The aircraft navigation apparatus as claimed in claim 4, wherein said serial data line receives said GNSS signals at a rate from about 1200 to about 9600 baud.

6. The aircraft navigation apparatus as claimed in claim 1, wherein said converting means comprises a microprocessor.

7. The aircraft navigation apparatus as claimed in claim 1, wherein said converting means comprises a shift register and decoder.

8. The aircraft navigation apparatus as claimed in claim 1, wherein said VOR signal generator comprises an antenna.

9. The aircraft navigation apparatus as claimed in claim 1, wherein said VOR signal generator transmits said VOR signals at a VOR test frequency.

10. The aircraft navigation apparatus as claimed in claim 9, wherein said VOR test frequency is about 108.00 MHz.

11. The aircraft navigation apparatus as claimed in claim 9, wherein said VOR test frequency is about 108.05 MHz.

12. The aircraft navigation apparatus as claimed in claim 6, wherein said converting means further comprises:

(d) a digital phase shifter for phase shifting an output signal from said microprocessor; and

(e) a modulating means for modulating a first sine function shifted by said digital phase shifter and an unshifted second sine function into a modulated signal.

13. The aircraft navigation apparatus as claimed in claim 12, wherein said second sine function frequency modulates a subcarrier.

14. The aircraft navigation apparatus as claimed in claim 12, wherein said converting means further comprises summation circuitry to sum said first and second sine functions.

15. The aircraft navigation apparatus as claimed in claim 12, wherein said converting means further comprises an amplitude modulator for generating a signal at a VOR test frequency.

16. The aircraft navigation apparatus as claimed in claim 12, wherein said VOR signal generator comprises an antenna which transmits said modulated signal while said microprocessor receives said GNSS signals through said signal linking means, and said antenna transmits an error message when said microprocessor does not receive said GNSS signals.

17. The aircraft navigation apparatus as claimed in claim 1, wherein said converting means comprises:

(d) processing means for receiving said GNSS signals and converting said GNSS signals into a plurality of VOR signals;

(e) a digital phase shifter;

(f) a sine generator at a first modulation frequency, a first sine function therefrom being phase shifted by said digital phase shifter, and a second sine function therefrom being unshifted;

(g) a frequency modulated oscillator having a subcarrier frequency modulated by said second sine function at said first modulation frequency;

(h) an analog summation circuit for summing said first and said second sine functions;

(i) an amplitude modulator driven by the output from said analog summation circuit; and

(j) a carrier frequency generator, said carrier frequency modulated by the output from said analog summation circuit.

18. An onboard aircraft navigation apparatus for converting digital Global Navigation Satellite System (GNSS) signals to VOR signals for receipt by a conventional VOR receiver aboard said aircraft, said navigation apparatus comprising:

(a) a GNSS receiver for receiving said GNSS signals;

(b) converting means for converting said GNSS signals into VOR signals; and

(c) a VOR signal generator for transmitting said VOR signals to said conventional VOR receiver.

19. The aircraft navigation apparatus as claimed in claim 18, wherein said GNSS receiver is a Global Satellite Positioning System (GPS) device.

20. A method for onboard coupling of digital signals from a Global Navigation Satellite System (GNSS) device to a conventional VOR receiver via a VOR signal, said method comprising the following steps:

(1) receiving a plurality of GNSS signals from said GNSS device;

(2) decoding at least one command within said plurality of GNSS signals;

(3) converting said at least one command to at least one corresponding VOR signal; and

(4) transmitting said at least one VOR signal to said conventional VOR receiver.