AIRCRAFT AVIONIC SYSTEM HAVING A PILOT USER INTERFACE WITH CONTEXT DEPENDENT INPUT DEVICES

• US 20080184166A1
• Filed: 12/03/2007
• Published: 07/31/2008
• Est. Priority Date: 06/02/2005
• Status: Abandoned Application

• Current Assignee: L-3 Communications Avionics Systems Incorporated (L3Harris Technologies, Inc.)
• Original Assignee: L-3 Communications Avionics Systems Incorporated (L3Harris Technologies, Inc.)
• Inventors: Getson, Blake R., Brust, Clifford S.
• Application Number:
  US11/949,492
• Publication Number:
  US 20080184166A1
• Time in Patent Office: Days
• US Class Current: 715/810
• CPC Class Codes: G01C 23/005 Flight directors indicating arrangements specially adapted for rotary gyroscopes G01C19/32

Abstract

An avionics system having a pilot user interface, and method of interfacing with a pilot, includes providing a display screen and a video processor driving the display screen. A plurality of context dependent input devices is provided. Operation of at least one of the input devices may cause the processor to display a rotary selection list on the display screen. The rotary selection list includes multiple potential selections, each capable of effecting a change in the avionic system when highlighted. At least one of the input devices may be made up of at least one rotary knob. The processor displays a context dependent label for the rotary knob.

Claims

1. An aircraft avionic system having a pilot user interface, said system comprising:

a display screen;

a video processor driving said display screen; and

a plurality of context dependent input devices, wherein operation of one of said input devices causes said processor to display a rotary selection list on said display screen, said rotary selection list including a menu of selectable options, each capable of effecting a change in said avionic system when highlighted and wherein subsequent operation of said one of said input devices causes a different one of said selectable options to be highlighted.

2. The system as claimed in claim 1 wherein said input devices comprise at least one selected from push buttons and a touch screen.

3. The system as claimed in claim 1 or claim 2 wherein said processor is adapted to drive said display screen to display a parameter associated with the highlighted one of said selections.

4. The system as claimed in claim 3 wherein at least one of said input devices comprising at least one rotary knob, said processor adapted to drive said display screen to display a context dependent label for said at least one rotary knob and wherein rotation of said at least one rotary knob edits at least a portion of said parameter.

5. The system as claimed in any of the preceding claims wherein said rotary selection menu remains hidden until operation of said one of said input devices.

6. The system as claimed in claim 5 wherein said rotary selection list becomes displayed upon actuation of said one of said input devices with one of said options highlighted.

7. The system as claimed in any of the preceding claims wherein said one of said input devices comprises a soft key.

8. The system as claimed in any of the preceding claims wherein said rotary selection list includes at least one inhibited option that is inhibited from effecting a change in said avionic system under particular context of said aircraft avionic system.

9. An aircraft avionic system having a pilot user interface, said system comprising:

a display screen;

a video processor driving said display screen; and

a plurality of context dependent input devices, at least one of said input devices comprising at least one rotary knob, said processor adapted to drive said display screen to display a context dependent label for said at least one rotary knob and said processor adapted to drive said display screen to display a parameter of said avionic system, wherein rotation of said at least one rotary knob edits at least a portion of said parameter.

10. The system as claimed in claim 9 wherein said at least one rotary knob comprises a large rotary knob and a small rotary knob that is smaller than and concentric with said large rotary knob.

11. The system as claimed in claim 10 wherein rotation of said large rotary knob edits a most significant portion of said parameter and rotation of said small rotary knob edits a least significant portion of said parameter.

12. The system as claimed in claim 10 or claim 11 wherein said processor is adapted to drive said display to display a plurality of parameters of said avionic system and wherein rotation of said large rotary knob causes said processor to drive said display to highlight different ones of said parameters.

13. The system as claimed in any of claims 10 through 12 wherein rotation of said small knob edits the one of said parameters that are highlighted.

14. The system as claimed in any of claims 9 through 13 wherein said processor is adapted to display context dependent labels for said large and small rotary knobs.

15. The system as claimed in claim 14 wherein said processor is adapted to separately highlight each of said context dependent labels to identify which of said knobs have active functions associated with corresponding controls.

16. The system as claimed in any of claims 10 through 15 wherein said small rotary knob rotates about an axis of rotation and wherein said small rotary knob is adapted to be actuated in a direction of said axis of rotation.

17. The system as claimed in claim 16 wherein said processor is adapted to display context dependent labels for said large and small rotary knobs and said actuation of said small rotary knob in said direction of said axis of rotation.