Multi-segment head-up display for aircraft

• US 4,147,056 A
• Filed: 09/23/1977
• Issued: 04/03/1979
• Est. Priority Date: 09/23/1977
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Original Assignee: Sundstrand Data Control, Inc.
• Inventors: Muller, Hans R.
• Primary Examiner(s): Woodiel, Donald O.
• Application Number:
  US05/836,012
• Time in Patent Office: 557 Days
• Field of Search: 73/178 T, 73/178 R, 340/27 AT, 244/187, 244/137 R
• US Class Current: 73/178.00T
• CPC Class Codes: G02B 2027/0187 slaved to motion of at least a part of the body of the user, e.g. head, eye
• CPC Class Codes: G02B 27/01 Head-up displays
• 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 head-up visual approach instrument having a display of flight guidance information for a two-segment approach to touchdown. The display includes flight path indicia which the pilot aligns with an outside world aiming point, as the touchdown zone of a runway. During the first segment the flight path indicia is positioned as a function of aircraft altitude to define the changing sight angle to the target.

Claims

1. In 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 a pitch stabilized reference indicia, flight path indicia movable vertically on the screen representing the flight path of the aircraft, for alignment with a pilot-selected outside world aiming point by manipulation of the attitude and speed of the aircraft, to follow an approach path to the point of initiation of a flare maneuver, said approach path having two successive straight line segments, the first being at a steeper angle than the second, and the second being directed toward said aiming point, an improved means for positioning said flight path indicia, comprising:

means for establishing the angles of said approach path segments;

means for measuring the aircraft altitude;

means for positioning said flight path indicia on the screen during the first segment of the approach in accordance with a first approach path command which is a function of the aircraft altitude and the selected angles of the approach path segments, for the flight path of the aircraft to follow the first approach path segment as the pilot maintains said indicia in alignment with said aiming point; and

means for positioning said flight path indicia on the screen during the second approach segment in accordance with a second approach path command which is a function of the angle of the second approach segment for the aircraft to follow the second approach path segment as the pilot maintains said indicia in alignment with said aiming point.

2. The instrument of claim 1 wherein said means for positioning the flight path indicia during the first segment of the approach is actuated by a command represented by the expression ##EQU6## where γ

₁ is the angle of the first approach path segment, γ

₂ is the angle of the second approach path segment, h is the altitude of the aircraft above the ground and Δ

h is the altitude at which the first segment intersects the second segment.

3. The instrument of claim 2 wherein said indicia positioning means for the first segment of the approach provides a command signal proportional to the equation and includes:

means for dividing Δ

h by h to provide Δ

h/h;

means for subtracting γ

₂ from γ

₁ to provide (γ

₁ -γ

₂);

means for multiplying (γ

₁ -γ

₂) by Δ

h/h to provide Δ

h/h(γ

₁ -γ

₂);

means for adding γ

₂ to Δ

h/h(γ

₁ -γ

₂) to provide Δ

h/h(γ

₁ -γ

₂)+γ

₂ ;

means for multiplying γ

₁ by γ

₂ to provide γ

₁ ·

γ

₂ ; and

means for dividing γ

₁ ·

γ

₂ by (Δ

h/h(γ

₁ -γ

₂)+γ

₂ to provide the command signal.

4. The instrument of claim 2 wherein said means for positioning the flight path indicia during the first segment of the approach is actuated by a command represented by the expression ##EQU7## where θ

* is the pitch angle of the aircraft.

5. The instrument of claim 4 wherein a circuit provides a command signal for the flight path indicia along said first segment and includes:

a source of signal representing θ

*;

a source of signal representing;

##EQU8## and means for subtracting ##EQU9## from θ

* during said first approach segment.

6. The instrument of claim 4 further including:

a source of signal representing the actual flight path γ

; and

means for summing a signal representing a function of the actual flight path angle with ##STR1## during said first approach segment.

7. The instrument of claim 2 further including:

means for vertically displacing said flight path indicia indicia in accordance with the difference between the actual flight angle γ and

-γ

₁ during flight along the first approach segment and then in accordance with the difference between the actual flight path angle γ and

angle γ

₂ during flight along the second approach segment.

8. The instrument of claim 1 including means for pilot-selection of γ

₁, γ

₂ and Δ

h.

9. The instrument of claim 1 wherein the angles of the first and second approach path segment are of the order of -6°

and -3°

, respectively.

10. In an aircraft instrument having a head-up display in which pilot guidance information is viewed against a background of the outside world, the pilot guidance information including flight path indicia for alignment with an outside world target, and improved indicia command signal source to position the indicia to guide the pilot along a flight path at an angle to the line of sight from the pilot to the outside world target, comprising:

a source of signal representing the flight path angle;

a source of signal representing altitude of the aircraft above the ground; and

means operable as a function of the flight path angle and the aircraft altitude to position the flight path indicia on the line of sight of the pilot to the target and to move the indicia to maintain the sight line of the pilot to the target as the aircraft altitude changes.