Dynamic primary flight displays for unusual attitude conditions

• US 20070085705A1
• Filed: 10/13/2005
• Published: 04/19/2007
• Est. Priority Date: 10/13/2005
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Wilson, Blake, Engels, Jary, Gannon, Aaron, Feyereisen, Thea, Wyatt, Ivan, He, Gang
• Granted Patent: US 7,403,133 B2
• Time in Patent Office: Days
• US Class Current: 340/967
• 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

Embodiments of the present invention provide a method of dynamically transitioning into a distinct display format during unusual attitude conditions. In one embodiment, the method includes collecting attitude data, comparing current attitude to a first set attitude angle, and fading a distinct display format into a display for unusual attitude conditions when current attitude is at least equal to the first set attitude angle.

Claims

1. A method of dynamically transitioning into a distinct display format during unusual attitude conditions, the method comprising:

collecting attitude data;

comparing current attitude to a first set attitude angle; and

fading a distinct display format into a display for unusual attitude conditions when current attitude is at least equal to the first set attitude angle.

2. The method of claim 1, wherein fading a distinct display format onto a display includes one of:

displaying substantially simultaneously the distinct display format and a normal attitude display format with varied degrees of prominence on the display based on the craft attitude angle; and

displaying the distinct display format substantially independently of the display of the normal attitude display format.

3. The method of claim 1, wherein fading a distinct display format onto a display includes one of:

fading a distinct display format onto a display at a substantially uniform rate over a set period of time; and

fading a distinct display format onto a display at a rate based on the rate at which the craft attitude angle deviates from the first set attitude angle.

4. The method of claim 1, wherein fading a distinct display format into a display includes one or more of:

aligning gradually a zero-pitch reference line with a display horizon line and maintaining the zero-pitch reference line aligned with the display horizon during unusual attitude conditions;

changing gradually the size of flight symbology relevant to attitude correction;

changing the appearance of a zero-pitch reference line;

fading out perspective view graphics; and

fading in a two color overlay wherein the color above a zero-pitch reference line is different from the color below zero-pitch reference line.

5. The method of claim 1, wherein fading a distinct display format onto a display comprises:

dividing the number of degrees between the first set attitude angle and a second set attitude angle into N increments;

assigning each of N increments to a percentage of fading; and

fading in the distinct display format the assigned percentage of fading as current attitude reaches each of N increments, such that when current attitude reaches the second set attitude the distinct display format is substantially finished fading into the display and when current attitude returns to the first set attitude the distinct display format is substantially finished fading out of the display.

6. The method of claim 1, wherein fading a distinct display format onto a display comprises:

dividing the number of degrees between the first set attitude angle and a second set attitude angle into N increments;

dividing the number of degrees between a third set attitude angle and a fourth set attitude angle into M increments;

assigning each of N increments to a percentage of fading the distinct display format into the display;

assigning each of M increments to a percentage of fading the distinct display format out of the display;

fading in the distinct display format the assigned percentage of fading as current attitude reaches each of N increments; and

fading out the distinct display format the assigned percentage of fading as current attitude returns to each of M increments.

7. The method of claim 1, wherein fading a distinct display format onto a display comprises one of:

fading in the distinct display format as a continuous function of the craft attitude angle between a first set attitude angle and a second set attitude angle such that the first attitude angle corresponds substantially to 100 percent display of a normal attitude display format and the second set attitude angle corresponds substantially to 100 percent display of the distinct display format; and

fading in the distinct display format as a continuous function of the craft attitude angle between a first set attitude angle and a second set attitude angle and fading out the distinct display format as a continuous function of the craft attitude angle between a third set attitude angle and a fourth set attitude angle such that the second set attitude angle corresponds substantially to 100 percent display of the distinct display format and the fourth set attitude angle correspons substantially to 100 percent display of a normal attitude display format.

8. The method of claim 7, wherein fading out the distinct display format as a continuous function of the craft attitude angle between a third set attitude angle and a fourth set attitude angle includes:

setting the third attitude angle such that perspective view terrain features are substantially faded out of the display at the third attitude angle; and

setting the fourth attitude angle such that perspective view terrain features substantially cover the entire display at the fourth attitude angle.

9. The method of claim 1, further comprising:

fading a distinct display format out of the display once attitude returns to normal.

10. The method of claim 9, wherein fading a distinct display format out of the display includes one of:

delaying for a period of time after attitude is no longer in unusual attitude conditions before fading a distinct display format out of the display; and

fixing a zero-pitch reference line at a selected position during the process of fading a distinct display format out of the display.

11. A graphical display system comprising:

one or more sensors for collecting attitude data;

a display element for displaying flight data; and

at least one processor coupled to the one or more sensors and the display element for processing data collected by the one or more sensors, wherein the at least one processor sends signals to the display element instructing the display element to fade in a distinct display format when a current attitude angle reaches a first set attitude angle.

12. The graphical display system of claim 11, wherein the at least one processor:

divides the number of degrees between the first set attitude angle and a second set attitude angle into N equally spaced increments;

assigns each of the N increments to a percentage of fading; and

sends a signal to the display element to fade in the distinct display format the assigned percentage of fading when a current attitude angle reaches each of the N increments.

13. The graphical display system of claim 11, wherein the at least one processor:

divides the number of degrees between the first set attitude angle and a second set attitude angle into N equally spaced increments;

divides the number of degrees between a third set attitude angle and a fourth set attitude angle into M equally spaced increments;

assigns each of N increments to a percentage of fading the distinct display format into the display;

assigns each of M increments to a percentage of fading the distinct display format out of the display;

sends a signal to the display element to fade in the distinct display format the assigned percentage of fading when a current attitude angle reaches each of the N increments; and

sends a signal to the display element to fade out the distinct display format the assigned percentage of fading when a current attitude angle returns to each of the M increments.

14. The graphical display system of claim 11, wherein the signals to the display element instructing the display element to fade in a distinct display format include one of:

signals instructing the display element to fade out perspective view graphics;

signals instructing the display element to fade a distinct display format onto a display at a substantially uniform rate over a set period of time when a current attitude angle reaches the first set attitude angle

15. The graphical display system of claim 11, wherein:

the at least one processor sends signals to a display element instructing the display element to fade a distinct display format out of the display when attitude conditions are no longer unusual.

16. The graphical display system of claim 11, further comprising:

a user input element for receiving a user input which suspends performance of the instructions for fading a distinct display format into a display.

17. A computer readable medium having computer-executable instructions for performing a method of dynamically transitioning into a distinct display format during unusual attitude conditions, the method comprising:

measuring at least one of a plurality of attitude angles, wherein the plurality of attitude angles define a craft'"'"'s attitude;

comparing the at least one of a plurality of attitude angles to a corresponding first set attitude angle; and

sending a signal to a display element instructing the display element to gradually fade in a distinct display format once at least one of the plurality of attitude angles equals the corresponding first set attitude angle.

18. The computer readable medium of claim 18, wherein sending a signal to gradually fade in a distinct display format includes:

sending a signal to gradually align a zero-pitch reference line with a display horizon line and maintain the zero-pitch reference line aligned with the display horizon during unusual attitude conditions;

sending a signal to fade in a distinct display format onto a display at a substantially uniform rate over a set period of time;

sending a signal to fade out perspective view graphics.

19. The computer readable medium of claim 18, further comprising:

determining a rate at which to fade in a distinct display format.

20. The computer readable medium of claim 22, wherein determining a rate at which to fade in a distinct display format includes:

dividing the number of degrees between the first set attitude angle and a corresponding second set attitude angle into N equally spaced increments;

assigning each of N increments to a percentage of fading; and

fading the distinct display format the assigned percentage of fading as a measured attitude angle of the plurality of attitude angles reaches each of the N increments.

21. The computer readable medium of claim 18, wherein determining a rate at which to fade in a distinct display format includes:

dividing the number of degrees between the first set attitude angle and a second set attitude angle into N equally spaced increments;

dividing the number of degrees between a third set attitude angle and a fourth set attitude angle into M equally spaced increments;

assigning each of N increments to a percentage of fading the distinct display format into the display;

assigning each of M increments to a percentage of fading the distinct display format out of the display;

fading in the distinct display format the assigned percentage of fading as a measured attitude angle of the plurality of attitude angles reaches each of the N increments; and

fading out the distinct display format the assigned percentage of fading as a measured attitude angle of the plurality of attitude angles returns to each of the M increments.

22. The computer readable medium of claim 18, further comprising;

sending a signal to a display element to fade a distinct display format out of the display once attitude is no longer in unusual attitude conditions.

23. The computer readable medium of claim 26, wherein sending a signal to a display element to fade a distinct display format out of the display includes:

delaying for a period of time after attitude is no longer in unusual attitude conditions before sending a signal to fade a distinct display format out of the display.

24. A graphical display system, comprising:

means for collecting attitude data;

means for executing instructions for fading in a distinct display format when a current attitude angle reaches a first set attitude angle; and

means for displaying the distinct display format.