Aircraft proximity monitoring system

• US 4,274,096 A
• Filed: 07/09/1979
• Issued: 06/16/1981
• Est. Priority Date: 07/09/1979
• Status: Expired due to Term

• Current Assignee: Terry A. Dennison
• Original Assignee: Terry A. Dennison
• Inventors: Dennison, Terry A.
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US06/055,992
• Time in Patent Office: 708 Days
• Field of Search: 343/112 CA, 343/112 TC, 343/112 C, 340/24, 340/26
• US Class Current: 342/456
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G01S 7/003 Transmission of data between radar, sonar or lidar systems and remote stations

Abstract

An aircraft proximity monitoring method according to the invention comprises the steps of: continuously and repeatedly developing and transmitting signals corresponding to the positions relative to a first location of aircraft within a predetermined range of said first location receiving said transmitted signals at a given aircraft and transposing the signals corresponding to the positions of the others of said aircraft to said second signals corresponding to the positions of said other aircraft relative to the location of said given aircraft and producing an observable indication of the positions of said other aircraft relative to said location of said given aircraft. Apparatus according to the invention includes apparatus for performing each of the foregoing steps.

Claims

1. An aircraft proximity monitoring system comprising:

ground-based means for continuously and repeatedly deriving and transmitting signal information representative of the speeds and positions relative to a first location of each and every one of a plurality of aircraft within a predetermined range of said first location, means on at least one of said plurality aircraft within said range of said first location for receiving said signal information, means on said one aircraft for identifying the portion of said signal information corresponding to said one aircraft, means for transposing said signal information so as to form second signal information corresponding to the positions of others of said plurality of aircraft relative to the position of said one aircraft and means on said one aircraft responsive to said second signal information for aiding in the navigation of said one aircraft with respect to the positions of at least selected ones of said other aircraft relative to the position of said one aircraft.

2. An aircraft proximity monitoring system according to claim 1 wherein said developing and transmitting means further includes means for developing and transmitting as a portion of first said signal information, information corresponding to the identity of selected ones of said aircraft within said predetermined range.

3. An aircraft proximity monitoring system according to claim 1 or claim 2 wherein said developing and transmitting means further includes means for developing and transmitting as a part of said first signal information, information corresponding to the altitude of selected ones of said aircraft within said predetermined range.

4. An aircraft proximity monitoring system according to claim 3 wherein said developing and transmitting means comprises translator means for cooperating with an air traffic computer and responsive to both ground-based radar and transponders carried by selected aircraft within said predetermined range and wherein said first location comprises an air traffic control center.

5. An aircraft proximity monitoring system according to claim 1 wherein said means for aiding in navigation comprises means for providing an observable indication of the positions of at least selected ones of said other aircraft relative to said one aircraft.

6. An aircraft proximity moitoring system according to claim 5 further including means on said one aircraft for distinguishing portions of said second signal information corresponding to aircraft within a predetermined range of special concern with respect to said one aircraft, and wherein said means for producing an observable indication includes means for distinguishing the portion of the observable indication corresponding to said portions of said second signal information distinguished.

7. An aircraft proximity monitoring system according to claim 6 wherein said means for producing an observable indication comprises a CRT display and wherein said range of concern comprises a predetermined volume having an apical portion located at the position in said CRT display representing said one aircraft.

8. An aircraft proximity monitoring system according to claim 7 wherein said volume comprises a cone.

9. An aircraft proximity monitoring system according to claim 7 wherein said receiving means and said transposing means on said aircraft include an aircraft computer system including means for selectively rotating said volume of concern about said apical portion.

10. An aircraft proximity monitoring system according to claim 1 or claim 9 wherein said one aircraft carries a transponder for producing signal information corresponding to the identity of said one aircraft and wherein said transposing means includes means for correlating said signal information from said transponder with said signal information from said transmitting means for producing said observable indication of other aircraft within said given range relative to said given aircraft.

11. An aircraft proximity monitoring system according to claim 7 wherein said observable indication producing means includes means for emphasizing the representations on said CRT aircraft within said volume of concern.

12. An aircraft proximity monitoring system according to claim 7 wherein said observable indication producing means includes means for deemphasing the representations on said CRT on aircraft not within said volume of concern.

13. An aircraft proximity monitoring system according to claim 6 wherein said observable indication producing means further includes means for producing a separate indication in response to said distinguishing means and corresponding to other aircraft within said range of concern.

14. An aircraft proximity monitoring system according to claim 1 wherein said last-mentioned means further includes means for providing an observable indication corresponding to the speeds of said other aircraft.

15. An aircraft promixity monitoring method comprising the steps of:

continuously and repeatedly developing and transmitting signals at a ground station corresponding to the positions relative to a first location of each and every aircraft within a predetermined range of said first location, receiving said transmitted signals at a given aircraft and transposing the signals corresponding to the positions of the others of said aircraft to second signals corresponding to the positions of said other aircraft relative to the location of said given aircraft and producing an observable indication of the positions of said other aircraft relative to said location of said given aircraft.

16. An aircraft proximity monitoring method according to claim 15 wherein the step of developing and transmitting further includes developing and transmitting signals corresponding to the identity of each of said aircraft within said predetermined range, wherein the step of receiving includes receiving said signals corresponding to the identity of said aircraft and wherein the step of producing an observable indication includes producing an observable indication of said identity.

17. An aircraft proximity monitoring method according to claim 15 or claim 16 wherein the step of developing and transmitting includes developing and transmitting signals corresponding to the altitudes of each of said aircraft within said predetermined range, wherein the step of receiving includes receiving said signals corresponding to altitudes and the step of producing an observable indication includes producing an observable indication corresponding to said altitudes.

18. An aircraft proximity monitoring method according to claim 15 wherein the step of producing an observable indication further includes establishing a range of concern relative to said location of said given aircraft and differentiating the observable indications within said range of concern from those observable indications without said range of concern.

19. An aircraft proximity monitoring system comprising:

ground-based means for continuously and repeatedly deriving and transmitting signal information representative of the speeds and positions relative to the location of an air traffic control center of each and every one of a plurality of aircraft within a predetermined range of said location, means on at least one of said plurality aircraft within said range of said location for receiving said signal information, means on said one aircraft for identifying the portion of said first signal information corresponding to said one aircraft, means for transposing said signal information so as to form second signal information corresponding to the positions of others of said plurality of aircraft relative to said one aircraft, means on said one aircraft responsive to said second signal information for producing an observable indication of the positions of selected ones of said other aircraft relative to said one aircraft, means accessible to an air traffic controller at said air traffic control center for transmitting further signal information corresponding to a particular one of said aircraft and additional means in said indication producing means for producing a separately identifiable observable indication particularly identifying the position of said particular one of said aircraft with respect to said one aircraft.