Electronic flight instrument design and evaluation tool

• US 4,573,925 A
• Filed: 09/14/1982
• Issued: 03/04/1986
• Est. Priority Date: 09/14/1982
• Status: Expired due to Term

• Current Assignee: Rockwell International Corporation
• Original Assignee: Rockwell International Corporation
• Inventors: Styers, C. James
• Primary Examiner(s): Pinkham, Richard C.
• Assistant Examiner(s): Picard, Leo P.
• Application Number:
  US06/418,105
• Time in Patent Office: 1,267 Days
• Field of Search: 434/43, 434/239, 434/49, 340/720, 340/724, 340/973
• US Class Current: 434/49
• CPC Class Codes: G09B 9/16 Ambient or aircraft conditions simulated or indicated by instrument or alarm

Abstract

A design and evaluation system is disclosed which enables the computer generation of graphic displays and symbology used in the design of electronic instrument displays. The graphics and symbology may be positioned, rearranged, altered, and replaced with other graphics or symbology representative of that used in the intended instrument. The display may then be dynamically tested in accordance with programmed or selected manual inputs to determine the aesthetic and functional interactions between symbols or groups of symbols and to evaluate their acceptability in their intended environment. The proposed display may be repeatedly updated, altered and modified during testing until a final version has been selected for the instrument display.

Claims

1. A process for generating and evaluating instrument displays comprising:

generating a plurality of display items representing parts of an instrument display;

selecting and arranging individual ones of said display items in a configuration forming an instrument display;

generating a plurality of individual control signals wherein each control signal represents a changing parameter visually displayed by said instrument display; and

altering individual display items in response to selected ones of said individual control signals to dynamically change the visual appearance of said instrument display in response to said changing parameters.

2. The process of claim 1 wherein each of said display items are coupled for control by a single control signal to reflect one changing parameter.

3. The process of claim 1 wherein said step of generating display items comprises forming a display menu library of multiple display items with a predetermined number of display items forming a page of menu, and selecting individual display items from said pages of menu.

4. The process of claim 1 wherein said step of generating control signals representing changing parameters comprises simulating the operation of a device and providing control signals representing said changing parameters produced as a result of that simulation.

5. The process of claim 4 further comprising the step of providing manual changes in said simulation to effect changes in said parameters.

6. The process of claim 4 further comprising the step of providing automatic changes in said simulation to effect changes in said parameters.

7. The process of claim 4 wherein said step of simulating comprises simulating aircraft flight and changing parameters represented by aircraft flight conditions.

8. The process of claim 7 further comprising the step of providing manual changes in said simulated aircraft flight from an aircraft wheel/column control.

9. The process of claim 7 wherein said step of simulating aircraft flight comprises simulating said flight with a simulated autopilot control.

10. The process of claim 7 wherein said step of simulating further comprises simulating a plurality of aircraft types for flight simulation and selecting one of said aircraft types for providing said changing parameters in response to the simulated flight of that selected aircraft type.

11. An instrument display design and evaluation system comprising:

means for generating a plurality of control signals representing varying parameters displayed by an instrument;

means for generating a plurality of individual display items, with each display item being associated with a different one of said varying parameters and including means for forming a menu of said display items;

means for selecting and displaying individual ones of said display items in the configuration of an instrument display; and

means for altering said display items in response to said control signals to reflect the dynamic operation of the instrument display in response to said changing parameters.

12. The system of claim 11 wherein said means for generating control signals comprises a means for generating control signals responsive to simulated aircraft flight.

13. The system of claim 12 further comprising means for providing manual inputs for altering said control signals responsive to aircraft flight.

14. The system of claim 12 further comprising means for altering said control signals in response to simulated autopilot control of aircraft flight.

15. The system of claim 11 wherein said means for generating control signals includes means for generating control signals representative of the flight of a particular aircraft type.

16. The system of claim 15 wherein said means for generating control signals representing the flight of a particular aircraft type further includes means for altering the aircraft type and associated control signals for producing control signals representing the flight of a different aircraft type.

17. The system of claim 11 wherein said menu library includes a predetermined number of display items forming at least one page of menu.

18. The system of claim 11 wherein said means for selecting and displaying further includes means for electronically displaying said configuration of display items as a visual representation of said instrument display.

19. The system of claim 18 wherein said means for electronically displaying comprises a color cathode ray tube.

20. An electronic flight instrument design and evaluation system comprising:

an aircraft simulation computer having a first input responsive to an aircraft wheel/column flight control and a second input responsive to a simulated autopilot control for simulating aircraft flight and generating control signals representing changing parameters in response to said simulated aircraft flight;

means for selectively controlling the generation of said control signals in response to one of said wheel/column control and said simulated autopilot control;

an interactive graphics system having a menu library for selectively generating a plurality of individual display items, each of which represent a portion of a display of an aircraft instrument and further including means for selecting individual ones of said plurality of display items for forming a configuration of an instrument display representing an aircraft instrument;

a color display coupled to said interactive graphics system for displaying the configuration of said selected display items; and

means for coupling said aircraft simulation computer to said interactive graphics system for altering said selected display items in response to said control signals to provide dynamic simulation of said instrument display.

21. The apparatus of claim 20 wherein said aircraft simulation computer includes a means for selectively simulating the flight of different aircraft types in response to said first or second inputs and providing control signals representing the flight of a selected aircraft type.

22. The system of claim 20 wherein said color display is a stroke written cathode ray tube.

23. The system of claim 20 wherein said interactive graphics system further includes means for altering the position, size, and orientation of selected display items forming said instrument display.

24. The apparatus of claim 20 further comprising means for substituting different display items for selected ones of said selected display items to form a different configuration of instrument display.

25. A process for generating and evaluating instrument displays comprising:

generating a plurality of display items which visually represent parts of an instrument display;

generating a plurality of individual control signals wherein each control signal represents a changing parameter visually displayed by said instrument display;

selecting and arranging individual ones of said display items in a configuration forming an instrument display;

altering individual display items in response to selected ones of said individual control signals to dynamically change the visual appearance of said instrument display in response to said changing parameters;

reselecting and rearranging individual ones of said display items in response to said dynamically changing visual appearance to form a different configuration of instrument display; and

again altering individual display items in response to selected ones of said individual control signals to dynamically change the visual appearance of said instrument display in response to said changing parameters.