Method and apparatus for display of an image to a pilot of an aircraft

• US 10,088,848 B2
• Filed: 08/25/2015
• Issued: 10/02/2018
• Est. Priority Date: 08/29/2014
• Status: Active Grant

• Current Assignee: BAE Systems Plc
• Original Assignee: BAE Systems Plc
• Inventors: Hodge, Steven James
• Primary Examiner(s): Goldman, Richard A
• Application Number:
  US15/506,929
• Publication Number:
  US 20170277199A1
• Time in Patent Office: 1,134 Days
• Field of Search: 701 16, 701 14, 701 3, 701 10, 701436, 701523, 701538, 73178 T, 940973, 940972, 940980, 244183
• CPC Class Codes: G01C 23/005 Flight directors indicating arrangements specially adapted for rotary gyroscopes G01C19/32
• CPC Class Codes: G02B 2027/0141 characterised by the informative content of the display
• CPC Class Codes: G02B 2027/0181 Adaptation to the pilot/driver
• CPC Class Codes: G02B 2027/0183 Adaptation to parameters characterising the motion of the vehicle
• CPC Class Codes: G02B 27/017 Head mounted
• 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 method for displaying an image to a pilot (20) of an aircraft (2). The method comprises, using a first value of the velocity of the aircraft (2) relative to a runway (4), displaying, on a HMD (24), an indication of a first position for an image component (e.g. a FPM) (36), the first position being the position, from the pilot'"'"'s point of view, that the image component (36) would occupy if the aircraft (2) was established on a predefined glideslope (16); using a second value different to the first value, displaying, on the HMD (24), an indication of a second position for the image component (36), the second position being the position, from the pilot'"'"'s point of view, that the image component (36) would occupy if the aircraft (2) was established on a different glideslope.

Claims

1. A method for displaying an image to a pilot of an aircraft, the method comprising:

acquiring, by one or more processors operatively linked to a helmet mounted display, a first value, the first value being a measurement of the velocity of the aircraft relative to a runway upon which the aircraft is to be landed;

displaying, by the helmet mounted display, to the pilot of the aircraft, a first image component, the position of the first image component on the helmet mounted display being dependent upon the first value, said position of the first image component being a horizontal position relative to the helmet mounted display;

displaying, by the helmet mounted display, to the pilot, a second image component, the second image component being such that, if, from the pilot'"'"'s point of view, the first image component and the second image component are in a pre-specified configuration on the helmet mounted display, the aircraft is established on a predefined glide slope;

displaying, by the helmet mounted display, to the pilot, a third image component, the position of the third image component on the helmet mounted display being dependent upon the position on the helmet mounted display of the second image component;

displaying, by the helmet mounted display, to the pilot, a fourth image component, the fourth image component indicating a first position on the helmet mounted display, the first position being such that if, from the pilot'"'"'s point of view, the third image component is located at the first position, the first image component and the second image component would be in the pre-specified configuration on the helmet mounted display from the pilot'"'"'s point of view;

acquiring, by the one or more processors, a second value, the second value being a value for the velocity of the aircraft relative to the runway, the second value being different to the first value; and

displaying, by the helmet mounted display, to the pilot, a fifth image component, the fifth image component indicating a second position on the helmet mounted display, the second position being such that if, from the pilot'"'"'s point of view, the third image component is located at the second position, the second image component would be located at a position on the helmet mounted display that it would have if the first image component was calculated using the second value instead of the first value, and, from the pilot'"'"'s point of view, the first image component and the second image component were in the pre-specified configuration on the helmet mounted display.

2. A method according to claim 1, the method further comprising controlling, by the pilot, the aircraft such that, from the pilot'"'"'s point of view, the third image component is located at the second position thereby providing that, from the pilot'"'"'s point of view, the second image component is located at the position on the helmet mounted display that it would have if the first image component was calculated using the second value instead of the first value and, from the pilot'"'"'s point of view, the first image component and the second image component were in the pre-specified configuration on the helmet mounted display, thereby the establishing the aircraft on a different glide slope.

3. A method according to claim 1, wherein the first image component is a Ship Reference Velocity Vector scale for aiding the pilot to land the aircraft.

4. A method according to claim 1, wherein the first image component is a linear object that extends horizontally across at least part of the helmet mounted display.

5. A method according to claim 1, wherein the second image component is a Ship Reference Velocity Vector for aiding the pilot to land the aircraft.

6. A method according to claim 1, wherein the second value and the first value differ, and wherein a determination of difference is made when the predetermined interval difference is met or exceeded.

7. A method according to claim 1, wherein the step of displaying the first image component comprises:

providing a measurement, to the one or more processors, of a velocity of the aircraft relative to the Earth;

providing a measurement, to the one or more processors, of a velocity of the runway relative to the Earth; and

using the provided measurements, determining, by the one or more processors, a specification for the first image component; and

using the determined specification, displaying, by the helmet mounted display, to the pilot, the first image component.

8. A method according to claim 1, wherein the step of displaying the fifth image component comprises:

providing, to the one or more processors, an indication that the first value is incorrect;

establishing, by the one or more processors, a specification for the fifth image component; and

in response to the one or more processors receiving the indication, using the established specification, displaying, by the helmet mounted display, to the pilot, the fifth image component.

9. A method according to claim 8 wherein the step of displaying the first image component comprises:

providing a measurement, to the one or more processors, of a velocity of the aircraft relative to the Earth;

providing a measurement, to the one or more processors, of a velocity of the runway relative to the Earth; and

using the provided measurements, determining, by the one or more processors, a specification for the first image component; and

using the determined specification, displaying, by the helmet mounted display, to the pilot, the first image component,

and

wherein the step of establishing, by the one or more processors, the specification for the fifth image component comprises;

modifying, by the one or more processors, the value of the velocity of the runway relative to the Earth; and

using the value of the velocity of the aircraft relative to the Earth and the modified value of the velocity of the runway relative to the Earth, establishing, by the one or more processors, the specification for the fifth image component.

10. A method according to claim 8, wherein the step of providing, to the one or more processors, the indication that the first value is incorrect comprises:

controlling, by the pilot, the aircraft such that, from the pilot'"'"'s point of view, the first image component and the second image component are in the pre-specified configuration on the helmet mounted display, thereby establishing the aircraft on the certain glide slope;

determining, by the pilot, that, while the aircraft is established on the certain glide slope, from the pilot'"'"'s point of view, the first image component moves with respect to one or more objects or features external to the aircraft; and

subsequently providing, to the one or more processors, the indication that the first value is incorrect.

11. A method according to claim 1, wherein the pre-specified configuration is that, from the pilot'"'"'s point of view, the first image component and the second image component are coincident on the helmet mounted display.

14. A program or plurality of programs arranged such that when executed by a computer system or one or more processors it/they cause the computer system or the one or more processors to operate in accordance with the method of claim 1.

15. A machine readable storage medium storing said program or at least one of the plurality of programs according to claim 14.

12. Apparatus for displaying an image to a pilot of an aircraft, the apparatus comprising:

one or more processors configured to determine respective specifications for a first image component, a second image component, a third component, a fourth component, and a fifth component; and

a helmet mounted display operatively coupled to the one or more processors and configured to display, to the pilot, the first image component, the second image component, the third component, the fourth component, and the fifth component in accordance with the determined specifications;

wherein

the position of the first image component on the helmet mounted display is dependent upon a first value for the velocity of the aircraft relative to a runway upon which the aircraft is to be landed, said position of the first image component being a horizontal position relative to the helmet mounted display;

the second image component is such that, if, from the pilot'"'"'s point of view, the first image component and the second image component are in a pre-specified configuration on the helmet mounted display, the aircraft is established on a certain glide slope;

the third image component is such that the position of the third image component on the helmet mounted display is dependent upon the position on the helmet mounted display of the second image component;

the fourth image component indicates a first position on the helmet mounted display, the first position being such that if, from the pilot'"'"'s point of view, the third image component is located at the first position, the first image component and the second image component would be in the pre-specified configuration on the helmet mounted display from the pilot'"'"'s point of view;

the fifth image component indicates a second position on the helmet mounted display, the second position being such that if, from the pilot'"'"'s point of view, the third image component is located at the second position, the second image component would be located at a position on the helmet mounted display that it would have if the first image component was calculated using a second value of the velocity of the aircraft relative to the runway instead of the first value, and, from the pilot'"'"'s point of view, the first image component and the second image component were in the pre-specified configuration on the helmet mounted display; and

the second value is different to the first value.

13. An aircraft comprising apparatus according to claim 12.