Radio navigation emulating GPS system

• US 5,957,995 A
• Filed: 06/17/1996
• Issued: 09/28/1999
• Est. Priority Date: 06/17/1996
• Status: Expired due to Term

• Current Assignee: Trimble Navigation Limited (Trimble Inc.)
• Original Assignee: Trimble Navigation Limited (Trimble Inc.)
• Inventors: Beckmann, Martin, Gunderson, Charles M.
• Primary Examiner(s): MARQUIS, LISSI MOJICA
• Application Number:
  US08/665,318
• Time in Patent Office: 1,198 Days
• Field of Search: 701/200, 701/213, 73/178 R, 395/500
• US Class Current: 701/213
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration

Abstract

The present invention provides a radio navigation emulating GPS device. In one embodiment, the radio navigation emulating GPS device receives an identifier associated with a conventional radio navaid. The present radio navigation emulating GPS device then retrieves latitude and longitude information corresponding to the received conventional radio navaid from a database. A satellite based position information system generates position information for the aircraft on which the present radio navigation emulating GPS device is disposed. The present radio navigation emulating GPS device then generates navigation information for the aircraft using the retrieved latitude and longitude information and the satellite based position information for the aircraft. The present radio navigation emulating GPS device then presents the navigation information in a manner which emulates the presentation of navigation information generated by a conventional radio navigation device. The entire emulation process is transparent to the user of the present radio navigation emulating GPS device.

Claims

1. A conventional radio navigation emulating aircraft navigation apparatus comprising:

a satellite based position determining system;

a data storage unit for storing latitude and longitude information corresponding to conventional navaids;

a processor coupled to said satellite based position determining system and said data storage unit, said processor for calculating position and navigation information for an aircraft using said latitude and longitude information corresponding to said conventional navaids and position information derived from said satellite based position determining system; and

a radio navaid emulating user interface coupled to said processor, said radio navaid emulating user interface for enabling a user to select a desired one of said conventional navaids.

3. The conventional radio navigation emulating aircraft navigation apparatus of claim 1 wherein said radio navaid emulating user interface includes user controls, said user controls substantially similar to user controls of a conventional radio signal based aircraft navigation system.

4. The conventional radio navigation emulating aircraft navigation apparatus of claim 1 wherein said radio navaid emulating user interface includes a display, said display adapted to display navigation data in a manner substantially similar to the manner in which navigation data is displayed in a conventional radio signal based aircraft navigation system.

5. The conventional radio navigation emulating apparatus of claim 1 wherein said radio navaid emulating user interface emulates a conventional radio signal based aircraft navigation system.

6. The conventional radio navigation emulating apparatus of claim 5 wherein said radio navaid emulating user interface emulates a VOR aircraft navigation system.

7. The conventional radio navigation emulating apparatus of claim 5 wherein said radio navaid emulating user interface emulates a DME aircraft navigation system.

8. The conventional radio navigation emulating apparatus of claim 5 wherein said radio navaid emulating user interface emulates a TACAN aircraft navigation system.

9. The conventional radio navigation emulating apparatus of claim 5 wherein said radio navaid emulating user interface emulates an NDB aircraft navigation system.

10. The conventional radio navigation emulating apparatus of claim 1 wherein said apparatus is adapted to receive a portable memory device such that additional data can be accessed by said processor.

2. A computer system comprising:

a processor;

an address/data bus coupled to said processor;

a satellite based position determining system coupled to communicate with said processor;

a computer readable memory coupled to communicate with said processor, said processor for performing steps of;

receiving at a conventional radio navigation emulating apparatus an identifier associated with a conventional navaid;

retrieving latitude and longitude information corresponding to said received conventional navaid, said latitude and longitude information retrieved from a data storage unit of said conventional radio navigation emulating apparatus;

generating satellite based position information for an aircraft coupled to said conventional radio navigation emulating apparatus;

generating navigation information for said aircraft using said retrieved latitude and longitude information and said satellite based position information for said aircraft; and

presenting said navigation information in a manner which emulates the presentation of navigation information generated by a conventional radio navigation device such that said navigation information is of use to a user familiar with a conventional radio navigation system.

17. The computer system of claim 2 wherein said processor further performs the steps of:

driving conventional radio navigation displays using said generated navigation information.

18. The computer system of claim 2 wherein said processor further performs the steps of:

calculating the distance of said aircraft from said received conventional navaid.

19. The computer system of claim 2 wherein said processor further performs the steps of:

retrieving said latitude and longitude information corresponding to said received conventional navaid from a portable memory device.

20. The computer system of claim 2 wherein said processor further performs the steps of:

calculating the bearing of said aircraft with respect to said received conventional navaid.

11. In a computer system, a method of emulating a conventional radio navigation system while using satellite based position information, said method comprising the computer implemented steps of:

receiving at a conventional radio navigation emulating apparatus an identifier associated with a conventional navaid;

retrieving latitude and longitude information corresponding to said received conventional navaid, said latitude and longitude information retrieved from a data storage unit of said conventional radio navigation emulating apparatus;

generating satellite based position information for an aircraft coupled to said conventional radio navigation emulating apparatus;

generating navigation information for said aircraft using said retrieved latitude and longitude information and said satellite based position information for said aircraft; and

presenting said navigation information in a manner which emulates the presentation of navigation information generated by a conventional radio navigation device such that said navigation information is of use to a user familiar with a conventional radio navigation system.

13. The method as recited in claim 11 further comprising the computer implemented steps of:

retrieving said latitude and longitude information corresponding to said received conventional navaid from a portable memory device.

14. The method as recited in claim 11 wherein said computer implemented step of generating navigation information for said aircraft using said retrieved latitude and longitude information and said satellite based position information for said aircraft further comprises the step of:

calculating the bearing of said aircraft with respect to said received conventional navaid.

15. The method as recited in claim 11 wherein said computer implemented step of generating navigation information for said aircraft using said retrieved latitude and longitude information and said satellite based position information for said aircraft further comprises the step of:

calculating the distance of said aircraft from said received conventional navaid.

16. The method as recited in claim 11 wherein said computer implemented step of presenting said navigation information in a manner which emulates the presentation of navigation information generated by a conventional radio navigation device further comprises the step of:

driving conventional radio navigation displays using said generated navigation information.

12. A computer-usable medium having computer-readable program code embodied therein for causing a computer to perform the steps of:

receiving at a conventional radio navigation emulating apparatus an identifier associated with a conventional navaid;

retrieving latitude and longitude information corresponding to said received conventional navaid, said latitude and longitude information retrieved from a data storage unit of said conventional radio navigation emulating apparatus;

generating satellite based position information for an aircraft coupled to said conventional radio navigation emulating apparatus;

generating navigation information for said aircraft using said retrieved latitude and longitude information and said satellite based position information for said aircraft; and

presenting said navigation information in a manner which emulates the presentation of navigation information generated by a conventional radio navigation device such that said navigation information is of use to a user familiar with a conventional radio navigation system.

21. The computer-usable medium of claim 12 further having computer-readable program code embodied therein for causing a computer to perform the steps of:

retrieving said latitude and longitude information corresponding to said received conventional navaid from a portable memory device.

22. The computer-usable medium of claim 12 further having computer-readable program code embodied therein for causing a computer to perform the steps of:

calculating the bearing of said aircraft with respect to said received conventional navaid.

23. The computer-usable medium of claim 12 further having computer-readable program code embodied therein for causing a computer to perform the steps of:

calculating the distance of said aircraft from said received conventional navaid.

24. The computer-usable medium of claim 12 further having computer-readable program code embodied therein for causing a computer to perform the steps of:

driving conventional radio navigation displays using said generated navigation information.