Traffic collision avoidance system

• US 6,085,150 A
• Filed: 07/22/1997
• Issued: 07/04/2000
• Est. Priority Date: 07/22/1997
• Status: Expired due to Term

• Current Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Henry, Jeff M., Suiter, James M.
• Primary Examiner(s): Cuchlinski, Jr., William A.
• Assistant Examiner(s): PIPALA, EDWARD J
• Application Number:
  US08/898,661
• Time in Patent Office: 1,078 Days
• Field of Search: 701/1, 701/3, 701/4, 701/14, 701/120, 701/300, 701/301, 701/302, 340/903, 340/945, 340/961, 342/29, 342/455
• US Class Current: 701/301
• CPC Class Codes: G08G 5/0008 with other aircraft
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0078 for monitoring traffic from the aircraft radar or analogous systems specially adapted for traffic control G01S13/91

Abstract

A traffic collision avoidance system (TCAS) for use in a first aircraft is disclosed. The TCAS includes TCAS circuitry providing output data as a function of a location of an intruder aircraft relative to a location of the first aircraft. A display device coupled to the TCAS circuitry receives the output data. The display device is adapted to provide a graphical representation of the altitude of the intruder aircraft.

Claims

1. A traffic collision avoidance system (TCAS) for use in a first aircraft, the TCAS comprising:

TCAS circuitry providing output data as a function of a location of an intruder aircraft relative to a location of the first aircraft; and

A display device coupled to the TCAS circuitry and receiving the output data, the display device being adapted to provide a graphical representation of an altitude of the intruder aircraft, wherein the display device is adapted to selectable provide both the graphical representation of the altitude of the intruder aircraft and a numeric representation of the altitude of the intruder aircraft that changes as the relative altitude between the first aircraft and the intruder aircraft changes.

2. The TCAS of claim 1, wherein the display device is also adapted to selectably provide only the numeric representation of the altitude of the intruder aircraft.

3. The TCAS of claim 1, and further comprising a display device pilot interface coupled to the display device, wherein a pilot of the first aircraft uses the display device pilot interface to select which of multiple intruder aircraft representation formats is provided by the display device to thereby optimize the situational awareness of the pilot.

4. The TCAS of claim 1, wherein the display device is adapted to provide the graphical representation of the altitude of the intruder aircraft in combination with a graphical representation of the position of the intruder aircraft relative to the first aircraft.

5. The TCAS of claim 1, wherein the graphical representation of the altitude of the intruder aircraft is a graphical representation of an altitude of the intruder aircraft relative to first reference altitude.

6. The TCAS of claim 5, wherein the first reference altitude is approximately zero feet.

7. A traffic collision avoidance system (TCAS) for use in a first aircraft, the TCAS comprising:

TCAS circuitry Providing output data as a function of a location of an intruder aircraft relative to a location of the first aircraft; and

a display device coupled to the TCAS circuitry and receiving the output data, the display device being adapted to provide a graphical representation of an altitude of the intruder aircraft in combination with a flight plan display.

8. A traffic collision avoidance system (TCAS) for use in a first aircraft, the TCAS comprising:

TCAS circuitry providing output data as a function of a location of an intruder aircraft relative to a location of the first aircraft; and

a display device coupled to the TCAS circuitry and receiving the output data, the display device being adapted to provide a graphical representation of an altitude of the intruder aircraft relative to a first reference altitude, wherein the graphical representation of the altitude of the intruder aircraft includes a first line segment extending from a graphical representation of the intruder aircraft to the first reference altitude, wherein a relative length of the first line segment is indicative of the altitude of the intruder aircraft.

9. A traffic collision avoidance system (TCAS) for use in a first aircraft, the TCAS comprising:

TCAS circuitry providing TCAS data as a function of a given location of an intruder aircraft relative to a location of the first aircraft;

a display device operationally coupled to the TCAS circuitry and receiving the TCAS data, the display device adapted to provide a plurality of different graphical representations of the given location of the intruder aircraft, wherein each of the plurality of different graphical representations of the given location of the intruder aircraft has a different viewing perspective associated therewith; and

a display device pilot interface operationally coupled to the display device, wherein a pilot of the first aircraft uses the display device pilot interface to select which of the plurality of different graphical representations of the given location of the intruder aircraft is displayed by the display device so that situational awareness of the pilot is optimized.

10. The TCAS of claim 9, wherein at least one of the plurality of different graphical representations of the location of the intruder aircraft includes a graphical representation of an altitude of the intruder aircraft relative to a first reference altitude.

11. The TCAS of claim 10, wherein the graphical representation of the altitude of the intruder aircraft relative to the first reference altitude includes a line segment extending from a graphical representation of the intruder aircraft to a representation of the first reference altitude, wherein a relative length of the line segment is representative of the altitude of the intruder aircraft.

12. The TCAS of claim 10, wherein at least one of the plurality of different graphical representations of the location of the intruder aircraft includes both a graphical representation of the altitude of the intruder aircraft relative to the first reference altitude and a numeric representation of the altitude of the intruder aircraft relative to a second reference altitude.

13. The TCAS of claim 10, wherein at least one of the plurality of different graphical representations of the location of the intruder aircraft includes a graphical representation of the altitude of the intruder aircraft relative to the first reference altitude in combination with a flight plan display.

14. A traffic collision avoidance system (TCAS) display unit for use in a first aircraft, the TCAS display unit comprising:

a display device adapted to receive TCAS data indicative of a given location of a second aircraft relative to the first aircraft and to provide a 3-dimensional representation of the location of the second aircraft relative to the first aircraft, wherein the display device is further adapted to provide a plurality of 3-dimensional representations of the given location of the second aircraft relative to the first aircraft; and

a display device interface coupled to the display device and controlling which of the plurality of 3-dimensional representations of the given location of the second aircraft are provided by the display device, wherein a pilot of the first aircraft uses the display device interface to select which of the plurality of 3-dimensional representations are provided by the display device to thereby optimize the situational awareness of the pilot.

15. The TCAS display unit of claim 14, wherein at least one of the plurality of 3-dimensional representations of the location of the second aircraft relative to the first aircraft includes a graphical representation of an altitude of the second aircraft relative to a first reference altitude.

16. The TCAS display unit of claim 15, wherein in the at least one of the plurality of 3-dimensional representations of the location of the second aircraft, the graphical representation of the altitude of the second aircraft relative to the first reference altitude includes a first line segment extending from a graphical representation of the second aircraft to a representation of the first reference altitude, wherein a relative length of the first line segment is representative of the altitude of the second aircraft.

17. The TCAS display unit of claim 16, wherein the at least one of the plurality of 3-dimensional representations of the location of the second aircraft further includes a second line segment extending from a graphical representation of the first aircraft to the representation of the first reference altitude, wherein the length of the second line segment is indicative of the altitude of the first aircraft, and wherein a length of the first line segment relative to a length of the second line segment is representative of the altitude of the second aircraft relative to the altitude of the first aircraft.

18. The TCAS display unit of claim 15, wherein at least one of plurality of 3-dimensional representations of the location of the second aircraft relative to the first aircraft includes a combination of the graphical representation of the altitude of the second aircraft relative to a first reference altitude and a numeric representation of the altitude of the second aircraft that changes as the location of the second aircraft relative to the first aircraft changes.

19. The TCAS display unit of claim 15, wherein at least one of plurality of 3-dimensional representations of the location of the second aircraft relative to the first aircraft includes a combination of the graphical representation of the altitude of the second aircraft relative to a first reference altitude and a numeric representation of the altitude of the second aircraft relative to a second reference altitude.