Method and apparatus for providing an indication as to whether an aircraft can safely glide to a selected destination

• US 5,142,480 A
• Filed: 02/27/1990
• Issued: 08/25/1992
• Est. Priority Date: 02/27/1990
• Status: Expired due to Fees

• Current Assignee: UPS Aviation Technologies, Inc. (Garmin Limited)
• Original Assignee: II Morrow, Inc.
• Inventors: Morrow, James
• Primary Examiner(s): Lall, Parshotam S.
• Assistant Examiner(s): Zanelli, Michael
• Application Number:
  US07/485,616
• Time in Patent Office: 910 Days
• Field of Search: 364/428, 364/430, 364/433, 364/446, 364/452, 364/444, 73/178 T, 244/185, 244/186
• US Class Current: 701/219
• CPC Class Codes: G01C 23/005 Flight directors indicating arrangements specially adapted for rotary gyroscopes G01C19/32
• CPC Class Codes: G05D 1/105 specially adapted for unpowered flight, e.g. glider, parachuting, forced landing parachutes per se B64D17/00

Abstract

A method and apparatus for providing an indication as to whether an aircraft can safely glide to a selected location. An electronic processor is provided with a manual data input, a Loran navigation system input, or electronic altimeter input, a memory, a display, and a processor program. Data representing the identity, location, and other features of a set of possible airport landing sites are stored in the memory. Data representing the aircraft flight performance parameters is entered manually. Based on the airport data, aircraft performance data, Loran data, and altimeter data, the program causes the processor to determine and display a predetermined number of nearest airports, the altitude required to glide to those airports from the aircraft'"'"'s current location, or the difference between the distance to the airports and the distance the aircraft can glide from its current altitude, and whether the aircraft can safely glide to a selected airport.

Claims

1. An on-board aircraft system for providing an indication as to whether said aircraft can safely glide to a selected destination, comprising:

(a) a radio navigation instrument on board said aircraft which provides data in the form of an electrical signal representing the current location of said aircraft;

(b) first source means on board said aircraft for providing in the form of an electrical signal data representing the current altitude of said aircraft;

(c) second source means on board said aircraft for providing data in the form of an electrical signal representing the flight a performance characteristics of said aircraft; and

(d) electronic data processor means, on board said aircraft and responsive to said data from said radio navigation instrument, said first source means, said second source means and said third source means, for producing, based on said current location of said aircraft, said altitude of said aircraft, said position of said selected target destination, and said flight performance data, an indication of whether said aircraft can glide to said selected target destination.

2. The system of claim 1 further comprising means responsive to said first source means for determining whether or not said electrical signal representing current altitude is reliable.

3. The system of claim 1 wherein said second source means comprises an electronic data storage device.

4. The system of claim 1 wherein said third source means comprises an electronical data storage device.

5. The system of claim 1, further comprising display means for providing a visual indication of whether said aircraft can safely glide to said target destination.

6. The system of claim 1, further comprising display means for providing a visual indication of the difference between the distance to said target destination and the distance that said aircraft can glide at its current altitude.

7. The system of claim 1, further comprising display means for providing a visual indication of the minimum altitude required for said aircraft to glide to said target destination from its current location.

8. The system of claim 1, further comprising display means for providing a visual indication of a predetermined number of nearest landing sites from among a set of possible landing sites.

9. The system of claim 1 wherein said processor means comprises programmed electronic digital data processor.

10. The system of claim 1 wherein said data processor means is adapted to determine the difference between the distance to said target destination and the distance that said aircraft can glide at its current altitude.

11. The system of claim 1, wherein said data processor means is adapted to determine the minimum altitude required for said aircraft to glide to said target destination from its current location.

12. The system of claim 1, wherein said data processor means is adapted to select as target destinations a predetermined number of nearest landing sites from among a set of possible landing sites.

13. The system of claim 1, wherein said radio navigation instrument comprises a Loran device.

14. The system of claim 1, wherein said first source means comprises an altimeter.

15. A method for determining on board an aircraft whether said aircraft can safely glide to a selected target destination, comprising:

(a) providing from a radio navigation instrument on board said aircraft to an electronic data processor on board said aircraft an electrical data signal representing the current location of said aircraft;

(b) providing from a first source on board said aircraft to said electronic data processor an electrical data signal representing the current altitude of said aircraft;

(c) providing from a second source on board said aircraft to said electronic data processor an electrical data signal representing the current position of said selected target destination;

(d) providing from a third source on board said aircraft to said electronic data processor an electrical data signal representing the flight performance characteristics of said aircraft; and

(e) causing said electronic data processor to produce, based on said current location, said current altitude, said selected target destination, and said flight performance data, an indication of whether said aircraft can glide to said selected target destination.

16. The method of claim 15, further comprising determining whether said altitude data is valid and, if not, displaying the altitude required to glide to said target location.

17. The method of claim 15, further comprising providing a visual display as to whether said aircraft can safely glide to said target destination.

18. The method of claim 15, further comprising providing a visual display of the difference between the distance to said target destination and the distance that said aircraft can glide at its current altitude.

19. The method of claim 15, wherein said radio navigation instrument comprises a Loran device.

20. The method of claim 15, wherein said first source comprises an altimeter.

21. The method of claim 15, wherein said second source comprises an electronic data storage device.

22. The method of claim 15, wherein said third source comprises an electronic data storage device.

23. The method of claim 15, further comprising causing said electronic data processor to select as target destinations a predetermined number of nearest landing sites from among a set of possible landing sites.

24. An on-board aircraft system for providing an indication as to whether said aircraft can safely glide to a selected destination, comprising:

(a) first source means on board said aircraft for providing data in the form of an electrical signal representing the current location of said aircraft;

(b) an altimeter on board said aircraft for providing in the form of an electrical signal data representing the current altitude of said aircraft;

(c) second source means on board said aircraft for providing data in the form of an electrical signal representing the position of a selected target destination;

(d) third source means on board said aircraft for providing data in the form of an electrical signal representing the flight performance characteristics of said aircraft; and

(e) electronic data processor means, on board said aircraft and responsive to said data from said first source means, said altimeter, said second source means, and said third source means, for producing, based on said current location of said aircraft, said altitude of said aircraft, said position of said selected target destination, and said flight performance data, an indication of whether said aircraft can glide to said selected target destination.

25. An on-board aircraft system for providing an indication as to whether said aircraft can safely guide to a selected destination, comprising:

(a) first source means on board said aircraft for providing data in the form of an electrical signal representing the current location of said aircraft;

(b) second source means on board said aircraft for providing in the form of an electrical signal data representing the current altitude of said aircraft;

(c) an electronic data memory on board said aircraft for providing data in the form of an electrical signal representing the position of a selected target destination;

(d) third source means on board said aircraft for providing data in the form of an electrical signal representing the flight performance characteristics of said aircraft; and

(e) electronic data processor means, on board said aircraft and responsive to said first source means, said second source means, said electronic data memory, and said third source means, for producing, based on said current location of said aircraft, said altitude of said aircraft, said position of said selected target destination, and said flight performance data, an indication of whether said aircraft can glide to said selected target destination.

26. An on-board aircraft system for providing an indication as to whether said aircraft can safely glide to a selected destination, comprising:

(a) first source means on board said aircraft for providing data in the form of an electrical signal representing the current location of said aircraft;

(b) second source means on board said aircraft for providing in the form of an electrical signal data representing the current altitude of said aircraft;

(c) third source means on board said aircraft for providing data in the form of an electrical signal representing the position of a selected target destination;

(d) an electronic data memory on board said aircraft for providing data in the form of an electrical signal representing the flight performance characteristics of said aircraft; and

(e) electronic data processor means, on board said aircraft and responsive to said data from said first source means, said second source means, said third source means, and said electronic data memory for producing, based on said current location of said aircraft, said altitude of said aircraft, said position of said selected target destination, and said flight performance data, an indication of whether said aircraft can glide to said selected target destination.

27. A method for determining on board an aircraft whether said aircraft can safely glide to a selected target destination, comprising:

(a) providing from a first source on board said aircraft to an electronic data processor on board said aircraft an electrical data signal representing the current location of said aircraft;

(b) providing from an altimeter on board said aircraft to said electronic data processor an electrical data signal representing the current altitude of said aircraft;

(c) providing from a second source on board said aircraft to said electronic data processor an electrical data signal representing the current position of said target destination;

(d) providing from a third source on board said aircraft to said electronic data processor an electrical data signal representing the flight performance characteristics of said aircraft; and

(e) causing said electronic data processor to produce, based on said current location, said current altitude, said target destination, and said flight performance data, an indication of whether said aircraft can glide to said selected target destination.

28. A method for determining on board an aircraft whether said aircraft can safely glide to a selected target destination, comprising:

(a) providing from a first source on board said aircraft to an electronic data processor on board said aircraft an electrical data signal representing the current location of said aircraft;

(b) providing from a second source on board said aircraft to said electronic data processor an electrical data signal representing the current altitude of said aircraft;

(c) providing from an electronic data memory on board said aircraft to said electronic data processor an electrical data signal representing the current position of said target destination;

(d) providing from a third source on board said aircraft to said electronic data processor an electrical data signal representing the flight performance characteristics of said aircraft; and

(e) causing said electronic data processor to produce, based on said current location, said current altitude, said target destination, and said flight performance data, an indication of whether said aircraft can glide to said selected target destination.

29. A method for determining on board an aircraft whether said aircraft can safely glide to a selected target destination, comprising:

(a) providing from a first source on board said aircraft to an electronic data processor on board said aircraft an electrical data signal representing the current location of said aircraft;

(b) providing from a second source on board said aircraft to said electronic data processor an electrical data signal representing the current altitude of said aircraft;

(c) providing from a third source on board said aircraft to said electronic data processor an electrical data signal representing the current position of said target destination;

(d) providing from an electronic data memory on board said aircraft to said electronic data processor an electrical data signal representing the flight performance characteristics of said aircraft; and

(e) causing said electronic data processor to produce, based on said current location, said current altitude, said target destination, and said flight performance data, an indication of whether said aircraft can glide to said target destination.