IP Library Granted Patent US 10,318,003
Granted Patent B2
US 10,318,003 · App. 15/095,310 · Granted Jun 11, 2019

System and method for providing aircraft autoflight capability feedback to a pilot

Inventors: Aaron Gannon (Anthem, AZ); Ivan Sandy Wyatt (Scottsdale, AZ); Steve Grothe (Cave Creek, AZ)
Assignee: HONEYWELL INTERNATIONAL INC.
G06F3/016G01C23/005G05D1/101G06F3/14G06F3/04842
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Quick Facts
Patent No.
US 10,318,003
App. No.
15/095,310
Granted
Jun 11, 2019
Kind
B2
Abstract

A system and method provides aircraft autoflight capability feedback to aircraft pilots to thereby prevent, or at least inhibit, latent errors of omission that may result in operational errors. The system and method uses graphics that communicate subtly and in the background, in a manner that naturally fits with how the visual cortex processes graphical information and how the mind makes quick, and subconscious judgments about information. The system may also use auditory and tactile feedback.

Claims (36)

1. A method for providing aircraft autoflight capability feedback to a pilot via a plurality of display devices that render images in a nominal resolution, the method comprising the steps of:

determining, in a processor, when a flight constraint value has been entered via a user interface;

determining, in the processor, which images, rendered on the plurality of display devices, are associated with the flight constraint value;

rendering, on the plurality of display devices, at least portions of the images associated with the flight constraint value in a degraded resolution, the degraded resolution being less than the nominal resolution;

determining, in the processor, if both a constraint selection function and an autoflight armed function have been enabled; and

rendering, on the plurality of the display devices, the images associated with the flight constraint value in the nominal resolution only when it is determined that both the constraint selection function and the autoflight armed function have been enabled,

wherein the step of determining if both the constraint selection function and the autoflight armed function have been enabled comprises:

determining if a first additional user interface has supplied a first enable signal representative of the constraint selection function;

determining if a second additional user interface has supplied a second enable signal representative of the autoflight armed function,

and wherein:

the first additional user interface comprises an altitude select (ASEL) function; and

the second additional user interface comprises a vertical navigation (VNAV) select function.

2. The method of claim 1 , further comprising:

generating, using the processor, feedback when a user operates the first additional user interface.

3. The method of claim 2 , wherein:

the feedback is generated at either a nominal level or a degraded level;

the degraded level less than the nominal level; and

the feedback is generated at the degraded level until it is determined that both the constraint selection function and the autoflight armed function have been enabled.

4. The method of claim 3 , wherein the feedback is one or more of audible, visual, and tactile.

5. A system for providing aircraft autoflight capability feedback to a pilot, comprising:

a plurality of display devices, each display device configured to render images in a nominal resolution and a degraded resolution, the degraded resolution less than the nominal resolution;

a first user interface configured to receive user input representative of a flight constraint value;

an altitude select (ASEL) function user interface configured to supply a first enable signal indicating a constraint selection function has been enabled;

a vertical navigation (VNAV) select function user interface configured to supply a second enable signal indicating that an autoflight armed function has been enabled; and

a processor in operable communication with the display devices, the first user interface, the ASEL function user interface, and the VNAV function user interface, the processor coupled to selectively receive the first enable signal from the ASEL function user interface indicating the ASEL function has been enabled, and the second enable signal from the VNAV function user interface indicating that the autoflight armed function has been enabled, the processor configured to:

determine when the flight constraint value has been entered via the first user interface,

determine which images rendered on the plurality of display devices are associated with the entered flight constraint value,

command the plurality of display devices to render at least portions of the images associated with the flight constraint value in the degraded resolution,

determine when both the first enable signal and the second enable signal have been received, and

command the plurality of display devices to render the images associated with the flight constraint value in the nominal resolution only when both the first enable signal and the second enable signal have been received.

6. The system of claim 5 , wherein:

the processor is further configured to generate feedback when a user operates the ASEL user interface;

the feedback is generated at either a nominal level or a degraded level;

the degraded level less than the nominal level; and

the processor generates feedback at the degraded level until both the first enable signal and the second enable signal have been received.

7. The system of claim 6 , wherein the feedback is one or more of audible, visual, and tactile.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 11, 2016
From: GANNON, AARON; WYATT, IVAN SANDY; GROTHE, STEVE
To: HONEYWELL INTERNATIONAL INC.
Reel/Frame 038242/0066 →
Continuity (1)
Related Publication 20170293358A1 · Oct 12, 2017
Cited By (11)
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