Aircraft landing display system

• US 4,368,517 A
• Filed: 04/08/1980
• Issued: 01/11/1983
• Est. Priority Date: 03/16/1978
• Status: Expired due to Term

• Current Assignee: Contel Federal Systems Incorporated (Verizon Communications Inc.)
• Original Assignee: Bunker Ramo Corporation (Honeywell International Inc.)
• Inventors: Lovering, Peter
• Primary Examiner(s): Smith, Jerry
• Application Number:
  US06/138,560
• Time in Patent Office: 1,008 Days
• Field of Search: 364/428, 364/429, 364/430, 364/522, 358/103, 358/104, 340/24, 340/723, 340/724, 340/729, 73/178 T, 434/42, 434/43
• US Class Current: 701/16
• CPC Class Codes: G01C 23/005 Flight directors indicating arrangements specially adapted for rotary gyroscopes G01C19/32
• CPC Class Codes: G05D 1/0676 specially adapted for landing
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/025 Navigation or guidance aids radar or analogous systems specially adapted for landing purposes G01S13/913

Abstract

A landing display system for indicating to the pilot of an aircraft the relationship between his aircraft and a landing runway includes an aircraft symbol providing attitude information with respect to a reference horizon, a velocity vector indicative of the projected flight path of the aircraft, a descent profile vector indicative of the projected descent path of the aircraft, and a runway symbol in perspective to the aircraft. By reference to these displays the pilot can ascertain not only the present position of his aircraft with respect to the runway, but also the consequences of various corrective maneuvers accomplished with the aircraft.

Claims

1. A system for presenting a cockpit display providing guidance information for landing an aircraft on a runway in conditions of low visibility, comprising:

a display device visible to the pilot;

means for generating on said display device a horizons reference line having a generally fixed horizontal configuration;

means for generating an aircraft symbol on said device, said aircraft symbol having an orientation with respect to said reference line corresponding to the orientation of the aircraft with respect to the actual horizon;

means for generating on said display device a runway symbol having an orientation with respect to the aircraft symbol indicative of the orientation of the actual runway with respect to the aircraft; and

means for generating a generally V-shaped descent profile vector extending from respective sides of the display towards a location on the projected flight path of the aircraft indicative of the projected landing point of the aircraft.

2. A landing display system as described in claim 1 wherein aircraft symbol further comprises a velocity vector having a direction indicative of the course of the aircraft with respect to the center line of the runway.

3. An aircraft display system as defined in claim 2 wherein said runway symbol includes a center line projection extending across the projected flight path depicted for said aircraft symbol.

4. A blind landing display system as defined in claim 3 wherein said velocity vector includes a tip portion indicative of the rate of change of said vector.

5. A blind landing system as defined in claim 1 wherein said descent profile vector includes at a disjunctive central portion thereof a tip portion indicating rate of change of the descent profile.

6. A blind landing display system as defined in claim 1 which further includes the generally V-shaped descent profile vector extending from either end of said horizon reference line.

7. A blind landing display system for assisting the pilot of an aircraft in landing on a runway in poor visibility conditions, comprising:

a display device in view of the pilot;

means for generating on said display device a horizon reference line having a generally fixed horizontal relationship with respect to said device;

means for generating an aircraft symbol on said display device having an orientation with respect to said horizon reference line corresponding to the relationship between the aircraft and the actual horizon;

means for generating a runway symbol on said display device below the horizon reference line having an orientation with respect to said aircraft symbol generally corresponding to the visual orientation of the actual runway as viewed from the aircraft, said runway symbol including an extended center line;

means for generating a velocity vector extending from said aircraft symbol indicative of the projected flight path of the aircraft with respect to said extended center line; and

means for generating a generally disjointed V-shaped descent profile symbol extending from either side of said display to indicate the projected landing point of the aircraft with respect to said runway.

8. A blind landing display system as defined in claim 7 including means for generating an additional descent profile indicative of the desired descent path and touchdown point of the aircraft with respect to said runway.

9. A blind landing display system as defined in claim 8 wherein the slope of said descent profile symbol is less than the slope of said desired profile when said aircraft is descending along a profile shallower than the desired profile, and wherein the slope of said descent profile symbol is steeper than said desired descent profile when said aircraft is descending more steeply than said desired descent profile.

10. A blind landing display system as defined in claim 9 wherein said descent profile symbol includes a tip portion indicative of the rate of change of the rate of descent of the aircraft.

11. A blind landing display system as defined in claim 9 wherein said velocity vector includes a tip portion indicative of the lateral acceleration of the aircraft with respect to the center line of said runway.