Apparatus for indicating air traffic and terrain collision threat to an aircraft

• US 6,538,581 B2
• Filed: 08/26/1999
• Issued: 03/25/2003
• Est. Priority Date: 02/26/1997
• Status: Expired due to Fees

• Current Assignee: Atlantic Inertial Systems Incorporated (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: BAE Systems Plc
• Inventors: Cowie, Mark
• Primary Examiner(s): SWARTHOUT, BRENT
• Application Number:
  US09/383,403
• Publication Number:
  US 20010013836A1
• Time in Patent Office: 1,307 Days
• Field of Search: 340/961, 340/970, 340/963, 342/29, 342/65, 701/4, 701/9, 701/14, 701/301
• US Class Current: 340/961
• CPC Class Codes: G08G 5/0078 for monitoring traffic from the aircraft radar or analogous systems specially adapted for traffic control G01S13/91
• CPC Class Codes: G08G 5/0086 for monitoring terrain radar or analogous systems specially adapted for terrain avoidance G01S13/935

Abstract

Includes means for monitoring the position and behavior of air traffic in the vicinity of the aircraft and generating a warning or avoidance signal for air traffic predicted to be on a collision course. The apparatus also includes means for monitoring the position and behavior of the aircraft relative to terrain in the vicinity of the aircraft flight path to generate a warning or avoidance signal for terrain features predicted to provide a collision threat. Means are provided for receiving the traffic warning signals and terrain warning signals comparing the signals and generating a combined warning or advisory signal which indicates an action for the aircraft which avoids both air traffic and terrain collisions.

Claims

1. An apparatus for indicating air traffic and terrain collision threats to an aircraft, comprising:

traffic advisory means for monitoring the position and behavior of air traffic in the vicinity of an aircraft provided with the apparatus and for generating a traffic signal regarding air traffic predicted to be on a collision course with the aircraft provided with the apparatus;

terrain advisory means for monitoring the position and behavior of the aircraft provided with the apparatus relative to terrain in the vicinity of the aircraft flight path and for generating a terrain signal for terrain features predicted to provide a collision threat to the aircraft flight path,

wherein terrain information sent from the terrain advisory means to the traffic advisory means is used in the generating of the traffic signal and air traffic information sent from the traffic advisory means to the terrain advisory means is used in the generating of the terrain signal; and

interactive means for receiving the traffic signal from the traffic advisory means and the terrain signal from the terrain advisory means, for comparing the traffic signal and terrain signal and for calculating a new signal from the traffic signal and the terrain signal which indicates an action for the aircraft to avoid both air traffic and terrain collisions.

2. The apparatus of claim 1, wherein the traffic signal is a warning signal.

3. The apparatus of claim 1, wherein the traffic signal is an avoidance signal.

4. The apparatus of claim 1, wherein the terrain signal is a warning signal.

5. The apparatus of claim 1, wherein the terrain signal is an avoidance signal.

6. The apparatus of claim 1, wherein the new signal is a warning signal.

7. The apparatus of claim 1, wherein the new signal is an avoidance signal.

8. The apparatus according to claim 1, wherein the traffic advisory means comprises:

a transponder for receiving position signals relating to the position of air traffic in the vicinity of the aircraft provided with the apparatus; and

a traffic signal generator operable to receive output signals from the transponder, to calculate and monitor the position and behavior of air traffic in the vicinity of the aircraft and to generate the traffic signal.

9. The apparatus according to claim 8, wherein the traffic signal generator is connectable to a flight management system of the aircraft provided with the apparatus to receive aircraft operating information therefrom.

10. The apparatus according to claim 1, wherein the terrain advisory means comprises:

a store of representations of terrain and obstacles in and around the flight path of the aircraft provided with the apparatus;

a search logic device for retrieving data from the store within a predetermined latitudinal and longitudinal envelope defined relative to the aircraft position and velocity; and

a terrain signal generator operable to receive, from a navigation system of the aircraft, signals representative of the latitude, longitude and altitude of the aircraft, calculate the predicted aircraft ground flight path, and generate the terrain signal.

11. The apparatus according to claim 8, wherein the terrain advisory means comprises:

a store of representations of terrain and obstacles in and around the flight path of the aircraft provided with the apparatus;

a search logic device for retrieving data from the store within a predetermined latitudinal and longitudinal envelope defined relative to the aircraft position and velocity; and

a terrain signal generator operable to receive, from a navigation system of the aircraft, signals representative of the latitude, longitude and altitude of the aircraft, calculate the predicted aircraft ground flight path, and generate the terrain signal.

12. The apparatus according to claim 10, wherein the terrain generator includes a comparator for comparing the predicted aircraft ground flight path with a predetermined worst case terrain profile so that the terrain signal is issued upon occurrence of a predetermined condition.

13. The apparatus according to claim 11, wherein the terrain generator includes a comparator for comparing the predicted aircraft ground flight path with a predetermined worst case terrain profile so that the terrain signal is issued upon occurrence of a predetermined condition.

14. The apparatus according to claim 12, wherein the predetermined condition is the predicted aircraft altitude falling below a predetermined minimum clearance height at any point along the predicted ground flight path.

15. The apparatus according to claim 12, wherein the predetermined condition is when intersection with the terrain is predicted to be less than a predetermined time to impact.

16. The apparatus according to claim 13, wherein the predetermined condition is the predicted aircraft altitude falling below a predetermined minimum clearance height at any point along the predicted ground flight path.

17. The apparatus according to claim 13, wherein the predetermined condition is when intersection with the terrain is predicted to be less than a predetermined time to impact.

18. The apparatus according to claim 10, wherein the interactive means interlinks and forms part of the traffic signal generator and the terrain signal generator and wherein the new signal includes an electrical signal.

19. The apparatus according to claim 12, wherein the interactive means interlinks and forms part of the traffic signal generator and the terrain signal generator and wherein the new signal includes an electrical signal.

20. The apparatus according to claim 10, further comprising:

an auditory warning device and a visual avoidance display device for receiving output signals from the traffic signal generator and the terrain signal generator, the auditory warning device further configured to feed and output signals to the visual avoidance display device.

21. The apparatus according to claim 12, further comprising:

an auditory warning device and a visual avoidance display device for receiving output signals from the traffic signal generator and the terrain signal generator, the auditory warning device further configured to feed and output signals to the visual avoidance display device.

41. The apparatus according to claim 1, wherein the terrain information includes a maximum descent rate signal and a terrain left/right signal and the air traffic information includes a proximity of the air traffic in the vicinity.

22. A method of indicating air traffic and terrain collision threats to an aircraft, comprising:

monitoring the position and behavior of air traffic in the vicinity of a first aircraft;

generating a traffic signal regarding air traffic predicted to be on a collision course with the first aircraft;

monitoring the position and behavior of the first aircraft relative to terrain in the vicinity of the first aircraft flight path;

generating a terrain signal for terrain features predicted to provide a collision threat to the aircraft flight path;

using air traffic information in the generating of the terrain signal;

using terrain information in the generating of the traffic signal;

receiving the traffic signal and the terrain signal at a receiver;

comparing the traffic signal and terrain signal; and

calculating a new signal from the traffic signal and the terrain signal which indicates an action for the first aircraft to avoid both air traffic and terrain collisions.

23. The method according to claim 22, wherein the traffic signal is a warning signal.

24. The method according to claim 22, wherein the traffic signal is an avoidance signal.

25. The method according to claim 22, wherein the terrain signal is a warning signal.

26. The method according to claim 22, wherein the terrain signal is an avoidance signal.

27. The method according to claim 22, wherein the new signal is a warning signal.

28. The method according to claim 22, wherein the new signal is an avoidance signal.

29. The method according to claim 22, wherein the step of monitoring the position and behavior of air traffic comprises:

receiving position signals, at a transponder, relating to the position of air traffic in the vicinity of the first aircraft; and

receiving output signals from the transponder at a traffic signal generator;

calculating and monitoring, at the traffic signal generator, the position and behavior of air traffic in the vicinity of the first aircraft.

30. The method according to claim 29, further comprising

receiving aircraft operating information from a flight management system of the first aircraft connectable to the traffic signal generator.

31. The method according to claim 22, wherein the step of monitoring the position and behavior of the first aircraft relative to terrain:

retrieving data, from a store of representations of terrain and obstacles in and around the flight path of the aircraft provided with the apparatus, within a predetermined latitudinal and longitudinal envelope defined relative to the first aircraft position and velocity; and

receiving, from a navigation system of the first aircraft, signals representative of the latitude, longitude and altitude of the aircraft, and

calculating the predicted aircraft ground flight path.

32. The method according to claim 31, further comprising:

comparing the predicted aircraft ground flight path with a predetermined worst case terrain profile so that the terrain signal is issued upon occurrence of a predetermined condition.

33. The method according to claim 32, wherein the predetermined condition is the predicted aircraft altitude falling below a predetermined minimum clearance height at any point along the predicted ground flight path.

34. The method according to claim 32, wherein the predetermined condition is when intersection with the terrain is predicted to be less than a predetermined time to impact.

42. The method according to claim 22, wherein the terrain information includes a maximum descent rate signal and a terrain left/right signal and the air traffic information includes a proximity of the air traffic in the vicinity.

35. An apparatus for indicating air traffic and terrain collision threats to an aircraft, comprising:

traffic advisory means for monitoring the position and behavior of air traffic in the vicinity of an aircraft provided with the apparatus and for generating a traffic signal regarding air traffic predicted to be on a collision course with the aircraft provided with the apparatus; and

terrain advisory means for monitoring the position and behavior of the aircraft provided with the apparatus relative to terrain in a geographical area along a predefined complete aircraft flight path of the aircraft and for generating a terrain signal for terrain features predicted to provide a collision threat to the predefined complete aircraft flight path, the terrain advisory means including a store containing a representation of the terrain in the geographical area along the predefined complete aircraft flight path

wherein terrain information sent from the terrain advisory means to the traffic advisory means is used in the generating of the traffic signal and air traffic information sent from the traffic advisory means to the terrain advisory means is used in the generating of the terrain signal.

36. The apparatus according to claim 35, wherein the terrain information includes a maximum descent rate signal and a terrain left/right signal and the air traffic information includes a proximity of the air traffic in the vicinity.

37. The apparatus according to claim 35, further comprising:

interactive means for receiving the traffic signal from the traffic advisory means and the terrain signal from the terrain advisory means, for comparing the traffic signal and terrain signal and for calculating a new signal from the traffic signal and the terrain signal which indicates an action for the aircraft to avoid both air traffic and terrain collisions.

38. The apparatus according to claim 35, wherein the predefined complete aircraft flight path includes predefined complete diversion flight paths of the aircraft.

39. The apparatus according to claim 35, wherein the representation of the terrain includes a representation of obstacles in the geographical area along the predefined complete aircraft flight path.

40. The apparatus according to claim 35, the terrain advisory means further including:

a search logic device for retrieving data from the store within a predetermined latitudinal and longitudinal envelope defined relative to the aircraft position and velocity; and

a terrain signal generator operable to receive, from a navigation system of the aircraft, signals representative of the latitude, longitude and altitude of the aircraft, calculate the predicted aircraft ground flight path, and generate the terrain signal.