System and method for displaying a velocity rate-of-change indicator

• US 8,604,942 B2
• Filed: 11/08/2011
• Issued: 12/10/2013
• Est. Priority Date: 11/08/2011
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Whitlow, Stephen, Flasar, Jan, Reusser, Trent
• Primary Examiner(s): Swarthout, Brent
• Application Number:
  US13/291,299
• Publication Number:
  US 20130113635A1
• Time in Patent Office: 763 Days
• Field of Search: 340/961, 340/963, 340/969, 340/971, 340/973, 340/978, 340/980, 701/7, 701/9, 701/14, 701/120, 701/121, 701/301, 342/29, 342/30, 342/36, 342/38
• US Class Current: 340/961
• 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
• 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

Avionics display system is provided for deployment onboard an aircraft and includes an air traffic data source that provides the avionics display system with data indicative of at least position and velocity of a neighboring aircraft. The system comprises a cockpit display system, and a monitor included within the cockpit display system. The cockpit display system receives and displays position and velocity data pertaining to the neighboring aircraft on the cockpit monitor as a position symbol and a velocity vector graphic. A processor operatively coupled to the monitor is configured to generate an air traffic display on the monitor including symbology indicative of (1) the current position of the neighboring aircraft (2) a velocity of the neighboring aircraft, and (3) the rate-of-change of the velocity of the neighboring aircraft.

Claims

1. A method for displaying the velocity rate-of-change (VROC) of at least one neighboring aircraft on a cockpit monitor included within a cockpit display system of a host aircraft, the cockpit display system receiving and displaying position and velocity data pertaining to the neighboring aircraft on the cockpit monitor as a position symbol and a velocity vector graphic, respectively, the method comprising:

determining the VROC of the neighboring aircraft;

generating a marker on the velocity vector that separates a first region on the velocity vector that visually represents a positive VROC from a second region on the velocity vector that visually represents a negative VROC;

generating VROC symbology on the cockpit display at a location along the velocity vector that is indicative of the neighboring aircraft'"'"'s VROC, wherein the VROC symbology comprises a plurality of symbols, the number and location of which visually represent a discreet range of VROC.

2. A method according to claim 1 wherein the marker visually represents a substantially zero VROC.

3. A method according to claim 1 wherein the VROC symbology is a bar extending from the position symbol and along the velocity vector, the location of the end of the bar on the velocity vector visually representing the VROC of the neighboring aircraft.

4. A method according to claim 1 wherein the VROC symbology comprises at least one line that intersects the velocity vector at a location that visually represents the VROC of the neighboring aircraft.

5. A method according to claim 1 wherein the VROC symbology comprises at least one chevron on the velocity vector that usually represents the VROC of the neighboring aircraft.

6. A method according to claim 1 further comprising generating VROC symbology substantially adjacent to the velocity vector.

7. A method carried out by a cockpit display system including a cockpit monitor, the method comprising:

receiving air traffic data from at least one traffic data source indicative of the position and velocity of at least one neighboring aircraft;

determining the velocity rate of change (VROC) of the neighboring aircraft from the air traffic data;

generating an air traffic display on the cockpit monitor including symbology indicative of (1) the current position of the neighboring aircraft, (2) the velocity vector of the neighboring aircraft, and (3) a marker on the velocity vector that separates a first region on the velocity vector that visually represents a positive VROC from a second region on the velocity vector that visually represents a negative VROC; and

generating VROC symbology on the cockpit display at a location along the velocity vector that is indicative of the neighboring aircraft'"'"'s VROC, wherein the VROC symbology comprises a plurality of symbols, the number and location of which visually represent a discreet range of VROC.

8. A method according to claim 7 wherein the marker visually represents a substantially zero VROC.

9. A method according to claim 8 wherein the VROC symbology is a bar extending from the position symbol and along the velocity vector, the location of the end of the bar on the velocity visually representing the VROC of the neighboring aircraft.

10. An avionics display system for deployment onboard an aircraft including an air traffic data source that provides the avionics display system with data indicative of at least position and velocity of a neighboring aircraft, the system comprising:

a cockpit display system;

a monitor included within the cockpit display system, the cockpit display system receiving and displaying position and velocity data pertaining to the neighboring aircraft on the cockpit monitor as a position symbol and a velocity vector graphic; and

a processor operatively coupled to the monitor and configured to generate an air traffic display on the monitor including symbology indicative of (1) the current position of the neighboring aircraft, (2) the velocity of the neighboring aircraft, (3) a marker on the velocity vector that separates a first region on the velocity vector that visually represents a positive VROC from a second region on the velocity vector that visually represents a negative VROC, and (4) VROC symbology at a location along the velocity vector that is indicative of the neighboring aircraft'"'"'s VROC, wherein the VROC symbology comprises a plurality of symbols, the number and location of which visually represent a discreet range of VROC.