Taxiing method and apparatus

Patent metadata

Field	Value
Publication number	US-12573306-B2
Application number	US-202017753646-A
Country	US
Kind code	B2
Filing date	Sep 10, 2020
Priority date	Sep 17, 2019
Publication date	Mar 10, 2026
Grant date	Mar 10, 2026

Abstract

A method for assisting a pilot to navigate an aircraft when taxiing is disclosed. A centre line of a route, conformal to outside scenery, is displayed on an eyes out screen associated with the pilot. A pictorial indication of the alignment of the undercarriage with the centre line is displayed on the eyes out screen. Further graphical information related to the navigation is displayed on the eyes out screen.

First claim

The invention claimed is:

1 . A method for assisting a pilot to navigate an aircraft when taxiing, the method comprising:
displaying, conformal to outside scenery, a centre line of a route assigned to the aircraft on an eyes out screen associated with the pilot; displaying, on the eyes out screen, a pictorial indication of an alignment of an undercarriage of the aircraft with the centre line and a stop or hold bar; displaying, on the eyes out screen, graphical information related to navigation of the aircraft, the graphical information comprising (i) a speed indicator, (ii) a throttle indicator, (iii) an acceleration indicator, and (iv) a bearing/heading indicator; and providing, via an active stick, a variable tactile feedback to the pilot based on a deviation of the alignment of the undercarriage of the aircraft from the route assigned to the aircraft, the variable tactile feedback requiring more force to move the active stick to a position that would deviate the undercarriage of the aircraft from the route compared to a movement of the active stick that would keep the undercarriage of the aircraft on the route.

2 . The method according to claim 1 , wherein the graphical information further comprises at least one of: a distance to turn indicator, a traffic indicator, or a time indicator, wherein the time indicator comprises at least one of an indication of time remaining to a destination of the aircraft, or an indication of the estimated time of arrival to the destination of the aircraft.

3 . The method according to claim 1 , comprising displaying, on the eyes out screen, a warning in response to at least one measure being more or less than a threshold, wherein the at least one measure includes one or more of a speed, a power setting, a distance to turn, and/or distance to traffic.

4 . The method according claim 1 , wherein displaying the centre line includes displaying mandatory stop bars.

5 . The method according to claim 1 , wherein the variable tactile feedback is in a direction that would correct the deviation and provided to the active stick used to steer a nosewheel.

6 . The method according to claim 1 , wherein the variable tactile feedback comprises a nudge.

7 . The method according to claim 1 , wherein the variable tactile feedback is synchronized with one or both of (1) a visual indication based on the deviation from the centre line route and (2) an aural indication based on the deviation from the centre line route.

8 . A non-transitory computer readable storage medium comprising instructions, that when executed by one or more processors, cause a process to be carried out for assisting a pilot to navigate an aircraft when taxiing, the process comprising:
causing display of, conformal to outside scenery, a centre line of a route on an eyes out screen associated with the pilot; causing display of, on the eyes out screen, a pictorial indication of an alignment of an undercarriage of the aircraft with the centre line and a stop or hold bar; causing display of, on the eyes out screen, graphical information related to navigation of the aircraft, the graphical information comprising a throttle indicator and an overhead map showing at least the route assigned to the aircraft, the position of the aircraft, and the stop or hold bar; and providing, via an active stick, a variable tactile feedback to the pilot based on a deviation of the alignment of the undercarriage of the aircraft from a path, the variable tactile feedback requiring more force to move the active stick to a position that would deviate the undercarriage of the aircraft from the path compared to a movement of the active stick that would keep the undercarriage of the aircraft on the path.

9 . A navigation system comprising a processor, an eyes out screen operatively coupled to the processor, and an active stick operatively coupled to the processor, the processor configured to assist a pilot to navigate an aircraft when taxiing, by causing:
display of, conformal to outside scenery, a centre line of a route on the eyes out screen associated with the pilot; display of, on the eyes out screen, a pictorial indication of an alignment of an undercarriage of the aircraft with the centre line and a stop or hold bar; display of, on the eyes out screen, graphical information related to navigation of the aircraft, the graphical information comprising an overhead map showing at least the route assigned to the aircraft, the position of the aircraft, and the stop or hold bar, the graphical information further comprising at least one of (i) a speed indicator, (ii) a throttle indicator, (iii) an acceleration indicator, and (iv) a bearing/heading indicator; and a variable tactile feedback to the pilot via an active stick based on a deviation of the alignment of the undercarriage of the aircraft from a path, the variable tactile feedback requiring more force to move the active stick to a position that would deviate the undercarriage of the aircraft from the path compared to a movement of the active stick that would keep the undercarriage of the aircraft on the path.

10 . The system according to claim 9 , wherein the variable tactile feedback is provided to the active stick used to steer a nosewheel and in a direction that would correct the deviation.

11 . The system according to claim 10 , wherein the variable tactile feedback comprises a nudge.

12 . The system according to claim 9 , wherein the variable tactile feedback is synchronized with one or both of (1) a visual indication based on the deviation from the centre line route and (2) an aural indication based on the deviation from the centre line route.

13 . The system according to claim 11 , wherein the graphical information related to the navigation includes any one or more of: an aircraft location indicator, a time to destination indicator, a distance to turn indicator, and a groundspeed indicator.

14 . The non-transitory computer readable storage medium according to claim 8 , wherein the variable tactile feedback is provided to the active stick used to steer a nosewheel and in a direction that would correct the deviation.

15 . The non-transitory computer readable storage medium according to claim 8 , wherein the variable tactile feedback is synchronized with one or both of (1) a visual indication based on the deviation from the centre line route and (2) an aural indication based on the deviation from the centre line route.

16 . The non-transitory computer readable storage medium according to claim 8 , wherein the graphical information related to the navigation includes any one or more of: an aircraft location indicator, a time to destination indicator, a distance to turn indicator, and a groundspeed indicator.

Assignees

• Bae Systems Plc

Inventors

• Lamb Philip
• Harrison James
• Kershaw Antony

Classifications

• G08G5/723

  from the aircraft · CPC title

• G08G5/55

  for a single aircraft · CPC title

• G08G5/50

  Navigation or guidance aids · CPC title

• G08G5/21

  located onboard the aircraft · CPC title

• G08B7/06

  using electric transmission {, e.g. involving audible and visible signalling through the use of sound and light sources} · CPC title