Integrated vertical situation display for aircraft

• US 6,154,151 A
• Filed: 06/16/1998
• Issued: 11/28/2000
• Est. Priority Date: 06/16/1998
• 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: Pingsterhaus, Scott A., McElreath, Kenneth W.
• Primary Examiner(s): SWARTHOUT, BRENT
• Application Number:
  US09/097,631
• Time in Patent Office: 896 Days
• Field of Search: 340/971, 340/972, 340/973, 340/974, 340/975, 340/980, 340/961, 340/970, 340/968, 340/976, 340/977, 340/963, 701/14, 701/18, 701/9, 701/120
• US Class Current: 340/970
• 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

Abstract

An integrated vertical situation display (IVSD) for an aircraft, and method of displaying vertical situation information, are disclosed herein. The IVSD includes an electronic display for displaying the vertical situation of the aircraft, input interfaces for receiving vertical profile information signals, and a processing circuit for reading the information signals and generating display signals applied to the display therefrom. The display has a vertical profile view area to display the vertical situation in front of, above, and below the aircraft. The information sources may include a flight management system, traffic alert and collision avoidance system (TCAS) and a ground proximity warning system. Vertical situations are displayed by visual indicia representing, for example, aircraft position, path angle, flight path, waypoints, TCAS targets, altitude preselect, decision height, runway, ground contour, and vertical speed. The integrated display minimizes the cognitive workload of the operator in assessing the total vertical situation.

Claims

1. An avionics system for an aircraft, the aircraft having a plurality of vertical profile information sources, comprising:

an integrated vertical situation display (IVSD) for displaying a vertical situation of the aircraft wherein the IVSD further comprises;

a free format line view area for displaying free format messages from the vertical profile information sources;

an altitude/vertical speed view area for displaying vertical profile information from the vertical profile information sources; and

a vertical profile view area for displaying the vertical situation of the aircraft in response to the vertical profile information sources; and

a control panel for providing integrated display management of the IVSD wherein the control panel comprises operator-actuatable input devices.

2. The avionics system of claim 1 wherein the IVSD further comprises:

a plurality of input interfaces for receiving vertical profile information signals from the plurality of vertical profile information sources;

a processing circuit coupled to the plurality of input interfaces for reading the vertical profile information signals and generating display signals; and

an electronic display for displaying the display signals.

3. The avionics system of claim 2 wherein the display signals cause the display to generate a plurality of visible indicia representative of the plurality of vertical profile information signals.

4. The avionics system of claim 1 wherein the vertical profile view area displays the vertical situation for distances in front of, above, and below the aircraft thereby defining a profile window.

5. The avionics system of claim 1 wherein the vertical profile information sources are al least two selected from the group consisting of a flight management system (FMS), an air data computer (ADC) a traffic alert and collision avoidance system (TCAS), and a ground proximity warning system (GPWS).

6. The avionics system of claim 1 wherein the vertical profile view area displays an aircraft symbol representing the position of the aircraft and when mapped within the profile window, a flight path line, a TCAS target symbol, an altitude preselect line, an indication of decision height, a ground contour line, and a runway symbol.

7. The avionics system of claim 1 wherein the free format line displays a free format message from a flight management system.

8. The avionics system of claim 1 wherein the altitude/vertical speed view area displays vertical profile information including a decision height indicator, a radio altitude indicator, a baroset indicator, a barometric altitude indicator, and a vertical speed indicator.

9. The avionics system of claim 1 wherein the control panel operator-actuatable input devices further comprise:

an altitude preselector device to select a desired altitude preselect for display on the IVSD;

a baroset device to select a desired baroset for display on the IVSD;

a decision height device to select a desired decision height for display on the IVSD; and

a vertical speed device to select a desired vertical speed for display on the IVSD.

10. An avionics system with an integrated vertical situation display (IVSD) for an aircraft, the aircraft having a plurality of vertical profile information sources, the IVSD further comprising:

a plurality of input interfaces for receiving vertical profile information signals from the plurality of vertical profile information sources;

a processing circuit coupled to the plurality of input interfaces for reading the vertical profile information signals and generating display signals; and

an electronic display for displaying the display signals wherein the electronic display further comprises;

an altitude/vertical speed view area for displaying vertical profile information; and

a vertical profile view area for displaying the vertical situation of the aircraft in response to the display signals; and

wherein the electronic display further comprises a free format line view area for displaying free format messages in response to the display signals.

11. The avionics system of claim 10 further comprising a control panel wherein said control panel further comprises:

an altitude preselector device to select a desired altitude preselect for display on the IVSD;

a baroset device to select a desired baroset for display on the IVSD;

a decision height device to select a desired decision height for display on the IVSD; and

a vertical speed device to select a desired vertical speed for display on the IVSD.

12. The avionics system of claim 10 wherein the display signals cause the display to generate a plurality of visible indicia representative of the plurality of vertical profile information signals.

13. The avionics system of claim 10, wherein the vertical profile view area displays the vertical situation for distances in front of, above, and below the aircraft thereby defining a profile window.

14. The avionics system of claim 10, wherein the vertical profile information signals are received from at least two vertical profile information sources selected from the group consisting of a flight management system (FMS), air data computer (ADC), a traffic alert and collision avoidance system (TCAS), and a ground proximity warning system (GPWS).

15. The avionics system of claim 13, wherein the visible indicia generated on the display includes an aircraft symbol representing the aircraft.

16. The avionics system of claim 15, wherein the visible indicia includes a path angle line extending from the aircraft symbol at an angle with respect to horizontal which represents a profile path angle of the aircraft.

17. The avionics system of claim 12, wherein the IVSD displays the desired altitude preselect as an altitude preselect indicator line and a digital altitude indicator on the vertical profile display area and a digital altitude preselect indicator of the altitude/vertical speed view area.

18. The avionics system of claim 12, wherein the IVSD displays the desired baroset as digital baroset indicator on the altitude/vertical speed view area.

19. The avionics system of claim 12, wherein the IVSD displays the desired decision height as a digital decision height indicator on the altitude/vertical speed view area and a digital decision height indictor and a decision height line intersecting a flight path line on the vertical profile display area.

20. The avionics system of claim 12, wherein the IVSD displays the desired vertical speed (VS) as a VS set indicator on a VS scale on the altitude/vertical speed view area.

21. The avionics system of claim 10 wherein the altitude/vertical speed view area displays a digital radio altitude indicator and tape radio altitude indicator.

22. The avionics system of claim 10 wherein the altitude/vertical speed view area displays a round dial barometric altitude indicator and a digital readout barometric altitude indicator.

23. The avionics system of claim 10 wherein the altitude/vertical speed view area displays a vertical speed indicator.

24. An avionics system with an integrated vertical situation display (IVSD) for an aircraft, the aircraft having a plurality of vertical profile information sources, the IVSD further comprising:

a free format line view area for displaying free format messages from the vertical profile information sources;

an altitude/vertical speed view area for displaying vertical profile information from the vertical profile information sources; and

a vertical profile view area for displaying the vertical situation of the aircraft in response to the vertical profile information sources.

25. The avionics system of claim 24 further comprising a control panel wherein said control panel further comprises:

an altitude preselector device to select a desired altitude preselect for display on the IVSD;

a baroset device to select a desired baroset for display on the IVSD;

a decision height device to select a desired decision height for display on the IVSD; and

a vertical speed device to select a desired vertical speed for display on the IVSD.