Cursor controlled navigation system for aircraft

• US 5,715,163 A
• Filed: 08/22/1995
• Issued: 02/03/1998
• Est. Priority Date: 08/22/1995
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Groce, deceased, John L., Chaney, Robert E., Bang, Eric S.
• Primary Examiner(s): ZANELLI, MICHAEL J
• Application Number:
  US08/518,090
• Time in Patent Office: 896 Days
• Field of Search: 364/448, 364/424.06, 364/444.2, 340/979, 340/995, 395/143, 345/157, 345/173
• US Class Current: 701/202
• 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 aircraft navigation control system includes a flight management system control display unit (12), a navigation display unit (40), logic circuitry (60) and a cursor control input device (70). The flight management system control display unit (12) includes a keyboard (30) to allow desired route waypoint modification via keyboard entries. These entries appear on a display (20) which provides a text listing of the selected waypoints. The navigation display (40) produces a graphical depiction of the selected waypoints as provided on the flight management system control display unit (12). In addition, the user may modify or create a new desired route by movement of a cursor (4) on the navigation display (40) to thereby highlight and select various waypoints as depicted on the display (40). By use of this graphical interface via a cursor control device (70) and the cursor (74) on the navigation display (40), a user may create, by a connect the dot approach, a new desired navigation route. Changes so entered on the navigation display (40) by the cursor control device (70) correspondingly create changes in the text display of the control display unit (12).

Claims

1. An aircraft cursor controlled navigation system comprising:

a navigation display for graphically displaying to the flight crew a sequence of waypoints defining a desired aircraft route and said navigation display also depicting a movable cursor;

a manual input cursor control device suited for receiving manual inputs to control the position of said cursor on said navigational display;

a control display unit including a keypad for allowing the typed entry of sequential waypoints to define a desired aircraft route and a text display of said typed entries; and

a logic means for directing aircraft flight in accordance with a flight crew input desired route, said logic means including logic for allowing the flight crew to select a new or revised desired route by manually selecting waypoints via the cursor control device with said newly selected waypoints automatically forming the desired route on both said navigation display and as a new or revised text display on said control display unit, said logic means including means for automatically deleting waypoints which are no longer on the desired route.

2. The aircraft cursor controlled navigation system of claim 1 wherein said logic means further includes:

means for drawing a line between a selected waypoint and the cursor position on said navigation display and calculating and displaying the relative bearing and distance from said selected waypoint to said cursor position.

3. The aircraft cursor controlled navigation system of claim 1 wherein said logic means further includes logic for:

determining if said cursor has been positioned within a predetermined position of a waypoint and, if so, highlighting said waypoint on said flight display.

4. The aircraft cursor controlled navigation system of claim 3 wherein said logic means further includes:

means for producing a text display on said control display unit of said highlighted waypoint.

5. The aircraft cursor controlled navigation system of claim 4 wherein said logic means further includes:

means permitting the flight crew to select said text display of said highlighted waypoint as a desired point on the route to thereby automatically enter said waypoint on the desired route.

6. The aircraft cursor controlled navigation system of claim 1 wherein:

said manual input cursor control device comprises a touch pad; and

said logic means responds to relative movement of a user'"'"'s finger across said touch pad to control movement of the cursor on said navigational display.

7. The aircraft cursor controlled navigation system of claim 6 wherein:

said touch pad includes hot pad areas; and

said system responds to a user activating a hot pad area to move said cursor to a predetermined position on said navigational display.

8. The aircraft cursor controlled navigation system of claim 3 wherein:

said manual input cursor control device comprises a touch pad; and

said logic means responds to relative movement of a user'"'"'s finger across said touch pad to control movement of the cursor on said navigational display.

9. The aircraft cursor controlled navigation system of claim 8 wherein:

said touch pad includes hot pad areas; and

said logic means responds to a user activating a hot pad area to move said cursor to a predetermined position on said navigational display.

10. The aircraft cursor controlled navigation system of claim 9 wherein:

said manual input cursor control device comprises a selector switch; and

said logic means responds to a user depressing said selector switch to select said highlighted waypoint as a waypoint on said desired route.

11. The aircraft cursor controlled navigation system of claim 1 wherein said logic means further includes:

means for creating images of one or more predetermined control buttons on said navigation display responsive to the system'"'"'s current mode of operation, and means for performing the operation represented by said control button image in the event a user, through the manual input cursor control device, selects said control button.

12. The aircraft cursor controlled navigation system of claim 11 wherein said logic means further includes:

means responsive to a user input to display on said navigation display a sequence of said control buttons, each control button corresponding to one of the possible waypoints within range of the display that the flight crew could select for inclusion on the desired route.

13. The aircraft cursor controlled navigation system of claim 11 wherein said logic means further includes:

means responsive to two or more waypoints being too close on said navigation display to be designated for selection, to display a sequence of said control buttons, each control button corresponding to one of said waypoints.