Traffic advisory-instantaneous vertical speed display

• US 4,914,733 A
• Filed: 10/30/1987
• Issued: 04/03/1990
• Est. Priority Date: 10/30/1987
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc.
• Original Assignee: Alliedsignal Inc.
• Inventors: Gralnick, Paul E. L.
• Primary Examiner(s): Orsino, Joseph A.
• Assistant Examiner(s): SWARTHOUT, BRENT
• Application Number:
  US07/115,687
• Time in Patent Office: 886 Days
• Field of Search: 340/961, 340/963, 340/973, 340/969, 340/970, 340/977, 340/978, 364/439, 364/460, 364/461, 364/449, 364/440, 364/441, 342/29-32, 342/37, 342/38, 342/455
• 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: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G01S 7/06 Cathode-ray tube displays or other two dimensional or three-dimensional displays
• CPC Class Codes: G01S 7/062 in which different colours are used
• CPC Class Codes: G01S 7/22 Producing cursor lines and indicia by electronic means

Abstract

An electronic display for presenting to an aircraft flight crew the combined information outputs of a vertical speed sensor and a TCAS computer aboard an aircraft. TCAS traffic advisories, i.e. the locations of other aircraft in the vicinity of the protected aircraft, are presented in a first display area of an electric display panel, preferrably in PPI format, showing range, relative bearing and relative altitude, if known. Vertical speed of the protected aircraft is indicated in a second display area adjacent the first display area on the same display panel. Whenever the TCAS computer determines that a particular aircraft constitutes a collison threat and that the establishment or maintainence of a specific flight path is necessary to minimize the probability of collision, the TCAS computer issues a resolution advisory which is displayed by identifying the threatening aircraft with a characterizing symbol in the first display area and by indicating symbolically and by other distinctive visual means, such as contrasting colors, in the first and second display areas the specific flight path to be established or maintained.

Claims

1. A display for presenting symbolically to an aircraft flight crew the traffic advisory and resolution advisory information developed by a Traffic Advisory and Collision Avoidance System (TCAS) computer aboard an aircraft, comprising:

an electronic display panel

an instantaneous vertical speed sensor aboard the aircraft, said sensor providing output data containing rate of climb or descent information for the aircraft;

first means receiving output data from said TCAS computer for controlling said display panel to present thereon a first display indicating the locations of other aircraft relative to the aircraft, said other aircraft being characterized by particular symbols in accordance with their degree of collision threat to the aircraft,

second means receiving output data from said instantaneous vertical speed sensor for controlling said display panel to present thereon a second display indicating the vertical speed of the aircraft, said second display being located in an area of said panel adjacent said first display; and

third means receiving output data from said TCAS computer for controlling said display panel to cause said second display to indicate vertical speeds of the aircraft which comply with a particular resolution advisory generated by said TCAS computer,

said second display including a scale of climb and descent rates and a pointer, the information content of said sensory output data being indicated by the position of said pointer along said scale, said third means controlling said display panel to cause illumination of the backgrounds of different portions of said scale with light of contrasting colors in accordance with resolution advisories generated by said TCAS computer, wherein said first display is presented in PPI format and said second display is laid out about the outer periphery of said first display.

2. Apparatus as claimed in claim 1 wherein said display panel is of the color liquid crystal type.

3. Apparatus as claimed in claim 1 wherein said display panel is of the color cathode ray tube type.

4. Apparatus as claimed in claim 1 wherein said second display is laid out circularly about the outer periphery of said first display.

5. Apparatus as claimed in claim 1 wherein said background of said scale is illuminated with red light in the range of rates prohibited by a particular resolution advisory and is illuminated with green light in the range of rates permitted by said particular resolution advisory.

6. Apparatus as claimed in claim 1 wherein the portion of the background of the vertical speed scale covering climb or descent rates in excess of climb or descent rates permitted by a particular TCAS resolution advisory is illuminated with yellow light and the remaining portion of the background of the vertical scale in compliance with said particular TCAS resolution is illuminated by green light.

7. Apparatus as claimed in claim 1 wherein said third means controls said display means to selectively illuminate one or more portions of the background of said scale in accordance with a particular resolution advisory.

8. Apparatus as claimed in claim 7 wherein said portion of the background of said scale in the range of rates prohibited by said particular resolution advisory is illuminated with red light.

9. Apparatus as claimed in claim 8 wherein said portion of the background of said scale in the range of rates permitted by said resolution advisory is illuminated with green light.

10. Apparatus as claimed in claim 7 wherein the altitude of said other aircraft relative to the aircraft is displayed adjacent said particular symbols characterizing said other aircraft.

11. Apparatus as claimed in claim 1 further comprising:

a third display on said display panel controlled by said first means receiving output data from said TCAS computer, on which a symbol representative of the resolution advisory generated by said TCAS is displayed.

12. Apparatus as claimed in claim 1 wherein the altitude of said other aircraft relative to the aircraft, is displayed adjacent said particular symbols characterizing said other aircraft.

13. Apparatus as claimed in claim 12 wherein said relative altitude is displayed in hundreds of feet as a positive number if said other aircraft is above the aircraft or as a negative number if said other aircraft is below the aircraft.

14. A method for presenting to a aircraft flight crew traffic advisories and resolution advisories for other aircraft within a selected horizontal range of the aircraft on a single electronic display face comprising the steps of:

providing on the display face an indication of the aircraft;

displaying on the display face symbols indicative of the altitude and bearing of other aircraft within the selected horizontal range;

changing the symbols indicative of other aircraft within the selected range to highlight aircraft which constitute a collision threat;

providing around the periphery of the display face a vertical speed scale illuminated with light of a first color;

positioning an indicator with respect to the vertical speed scale to indicate the aircraft vertical speed; and

,

selectively illuminating a portion of the vertical speed scale, indicative of a range of vertical speeds which should be avoided, in a contrasting color to that of said first color, in response to a resolution advisory provided by a Traffic Advisory and Collision Avoidance System (TCAS) computer aboard the aircraft.

15. A method as claimed in claim 14, further comprising the step of:

displaying a symbol representing a particular resolution advisory.

16. A method as claimed in claim 14 further comprising:

providing around the indication of the aircraft, fixed range markings intermediate said aircraft indication and the selected horizontal range.

17. A method as claimed in claim 14 wherein the range of the vertical speeds to be avoided is illuminated red.