Low altitude head up display for aircraft

• US 4,057,782 A
• Filed: 04/05/1976
• Issued: 11/08/1977
• Est. Priority Date: 04/05/1976
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc.
• Original Assignee: Sundstrand Data Control, Inc.
• Inventors: Muller, Hans Rudolf
• Primary Examiner(s): Habecker, Thomas B.
• Application Number:
  US05/673,794
• Time in Patent Office: 582 Days
• Field of Search: 340/27 AT, 244/187, 244/137
• US Class Current: 340/972
• CPC Class Codes: G01C 23/005 Flight directors indicating arrangements specially adapted for rotary gyroscopes G01C19/32
• CPC Class Codes: G02B 27/01 Head-up displays
• CPC Class Codes: G05D 1/0676 specially adapted for landing

Abstract

An aircraft instrument with a reflective screen on which the pilot views a collimated head up display of flight guidance information against a background of the outside world, for low altitude maneuvers. The guidance information includes a pitch stabilized reference indicia and a flight path indicia. The pitch reference and flight path indicia are positioned on the screen in accordance with aircraft operating parameters and pilot inputs to provide for a flare maneuver to touchdown or to direct the pilot in a path parallel with the surface of the ground, as for ejecting cargo.

Claims

1. A head up visual approach aircraft instrument, having a screen on which the pilot of an aircraft views a collimated display of flight guidance information against a background of the outside world, the display including first indicia movable vertically on the screen as a target for the pilot, second indicia movable vertically on the screen representing the flight path of the aircraft, for alignment of both indicia with an outside world aiming point by manipulation of the aircraft altitude and speed, wherein said instrument comprises:

means for positioning said first indicia on said screen successively in accordance with an approach path to said outside world aiming point, then along a transition path from said approach path and then in alignment with the horizon to define a path above and generally parallel with the ground; and

means for positioning said second indicia successively in accordance with an approach path command, and then with a transition path command, manipulation of the aircraft by the pilot to align said second indicia with said first indicia causing said aircraft to follow said approach and transition paths and to continue in a path above and generally parallel with the ground, as for ejection of cargo from the aircraft while airborne.

2. The aircraft instrument of claim 1 in which said second indicia transition path command is the sum of a signal representing the rate of change of altitude of the aircraft and a signal representing the difference between the altitude above ground and the altitude of said path above ground.

3. The aircraft instrument of claim 1 in which the altitude of said flight path parallel with the ground altitude is selected by the pilot.

4. The aircraft instrument of claim 1 including:

means operable by the pilot for selecting an instrument operating mode directing a flight guidance display for a low altitude path above ground; and

means for displaying operating mode indicia on said screen which indicates to the pilot that a low altitude path above ground has been selected.

5. The aircraft instrument of claim 1 including means for initiating the transition path display of said first and second indicia at an altitude above the ground which is a function of the altitude of the parallel path above ground.

6. The aircraft instrument of claim 1 including means for displaying on said screen indicia indicating to the pilot that the aircraft has descended to and is following the path above and parallel with the ground.