Automatic reconfiguration of electronic landing display

• US 4,999,780 A
• Filed: 03/03/1989
• Issued: 03/12/1991
• Est. Priority Date: 03/03/1989
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Mitchell, James E.
• Primary Examiner(s): Lall, Parshotam S.
• Assistant Examiner(s): PIPALA, EDWARD J
• Application Number:
  US07/319,383
• Time in Patent Office: 739 Days
• Field of Search: 364/428-430, 364/424.01, 364/424.06, 340/945, 340/947, 340/951, 340/954, 340/959, 340/980, 340/972, 340/973, 340/976, 358/103, 358/104, 434/38, 434/42-44, 434/50, 73/178 R, 73/178 T
• US Class Current: 701/16
• 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
• CPC Class Codes: G05D 1/0676 specially adapted for landing

Abstract

Automatically reconfiguring an electronic landing display that includes a flight path vector (FPV) symbol and a rising runway symbol combined with a digital altitude value that merge at low aircraft altitudes is disclosed. During approach, when the aircraft descends below a predetermined minimum altitude, e.g., 200 feet, the FPV symbol is removed. When the aircraft is on the ground and during takeoff, the rising runway symbol is removed. Removing one or the other of the merging symbols prevents the symbols from overlapping. Thus, the potential for pilot error due to one of the merging symbols occluding the other is avoided.

Claims

1. In an electronic flight instrument system that includes:

(i) an electronic landing display that includes a flight path vector (FPV) symbol and a runway symbol that merge toward one another when an aircraft incorporating the electronic flight instrument system descends below a first predetermined altitude above a runway during a landing maneuver; and

(ii) a programmable controller for controlling the position and orientation of said FPV and runway symbols of said electronic landing display, the improvement comprising;

means for automatically reconfiguring the electronic landing display by removing said FPV symbol prior to said merging FPV and runway symbols overlapping and occluding one another by programming said programmable controller to remove said FPV symbol from said display when the altitude of said aircraft above said runway drops below a second predetermined value, said second predetermined value being chosen such that said FPV and runway symbols do not overlap when the altitude of said aircraft above said runway drops below said second predetermined value.

2. The improvement claimed in claim 1 including a radar altitude value associated with said runway symbol such that said radar altitude value would be occluded by said FPV symbol if said FPV symbol were allowed to overlap said runway symbol and said radar altitude value.

3. The improvement claimed in claim 2 wherein said runway symbol and said radar altitude value rise toward said FPV symbol when the altitude of said aircraft above said runway drops below said first predetermined value.

4. The improvement claimed in claim 3, wherein said runway signal and said radar altitude value are removed from said display when said aircraft is on the ground.

5. The improvement claimed in claim 4, wherein said runway symbol and said radar altitude value are also removed from said display when the speed of said aircraft is below a predetermined value.

6. The improvement claimed in claim 2, wherein said runway symbol and said radar altitude value are removed from said display when said aircraft is on the ground and at takeoff thrust.

7. The improvement claimed in claim 6, wherein said runway symbol and said radar altitude value are also removed from said display when said aircraft is on the ground and at a speed below 80 knots.

8. The improvement claimed in claim 2, wherein said flight path vector symbol is removed from said display when said aircraft is airborne and said radar altitude value is less than 200 feet.

9. The improvement claimed in claim 8, wherein said flight path vector symbol is removed from said display when said rising runway symbol is being displayed, said aircraft is airborne and said radar altitude value is less than 200 feet.