Aircraft operating and position information display system and method

Patent metadata

Field	Value
Publication number	US-9296490-B2
Application number	US-201414467275-A
Country	US
Kind code	B2
Filing date	Aug 25, 2014
Priority date	Aug 25, 2014
Publication date	Mar 29, 2016
Grant date	Mar 29, 2016

Abstract

A method of displaying aircraft operating and position information with an electronic display unit comprises determining a position of a first aircraft at an airport; determining an optimum speed range of the first aircraft; determining a first aircraft speed of the first aircraft; displaying on a screen of the display unit a map of at least part of the airport; displaying a first aircraft symbol on the map, the first aircraft symbol displayed in a position on the map indicative of position of the first aircraft; and displaying an optimum speed range symbol having a lower bound end and a higher bound end in a position on the map such that the first aircraft symbol is between the lower bound end and the higher bound end when the first aircraft speed is within the optimum speed range.

First claim

We claim:

1. A method of displaying aircraft operating and position information with an electronic display unit, comprising:
determining a position of a first aircraft at an airport; determining a ground optimum speed range of the first aircraft, with a performance model;
determining a first aircraft ground speed of the first aircraft with a speed sensor;
generating display signals as a function of the first aircraft position, the first aircraft ground optimum speed, and the first aircraft ground speed;
displaying on a screen of the display unit a map of the airport, including geographic locations and dimensions of runways and taxiways, from map data in an airport database;
displaying a first aircraft symbol on the map, the first aircraft symbol displayed in a position on the map indicative of position of the first aircraft; and
displaying an optimum speed range symbol, the optimum speed range symbol having a lower bound end and a higher bound end, on the map; and
wherein the optimum speed range symbol is displayed in a position on the map such that the first aircraft symbol is between the lower bound end and the higher bound end when the first aircraft speed is within the optimum speed range.

2. The method of claim 1 , wherein the optimum speed range symbol is placed in a position on the map such that the first aircraft symbol is on a lower bound side of the optimum speed range symbol when the first aircraft speed is less than the optimum speed range; and
the optimum speed range symbol is placed in a position on the map such that the first aircraft symbol is on a higher bound side of the optimum speed range symbol when the first aircraft speed is greater than the optimum speed range.

3. The method of claim 1 , further comprising displaying a first intended route on the map indicative of a first intended route of the first aircraft.

4. The method of claim 3 , further comprising;
displaying a speed vector symbol along the first intended route, the speed vector symbol having a first end and a second end, the speed vector displayed with the first end at the first aircraft map position and the second end at a current speed predicted position on the map, the current speed predicted position indicative of a predicted position of the first aircraft if the first aircraft maintains the current speed of the first aircraft for a first time period; and
displaying a maximum speed vector symbol along the current intended route, the maximum speed vector symbol having a first end and a second end, the maximum speed vector displayed with the first end at the first aircraft map position and the second end at a maximum speed predicted position on the map, the maximum speed predicted position indicative of a predicted position of the first aircraft if the first aircraft maintains the maximum possible speed of the first aircraft for a first time period.

5. The method of claim 3 , further comprising; displaying a deceleration point symbol on the map in a deceleration point position indicative of a position on the first intended route where the first aircraft must begin decelerating to follow the first intended route.

6. The method of claim 3 , further comprising;
displaying an emergency stop symbol on the map in an emergency stop position on the first intended route indicative of a stop position of the first aircraft if full braking power is applied to the first aircraft until the first aircraft has come to a stop; and
displaying a coast stop symbol on the map in a coast stop position on the first intended route indicative of a stop position of the first aircraft if the first aircraft is put in a coast mode until the first aircraft has come to a stop.

7. The method of claim 1 , further comprising;
displaying the map, the first aircraft symbol, and the optimum speed range symbol in a first display scheme when the current speed of the first aircraft is within or less than the optimum speed range;
displaying the map, the first aircraft symbol, and the optimum speed range symbol in a second display scheme when the current speed of the first aircraft is greater than the optimum speed range, the second display scheme different than the first display scheme; and
displaying the map, the first aircraft symbol, and the optimum speed range symbol in a third display scheme when the current speed of the first aircraft is greater than a speed necessary for the first aircraft to follow a first intended route, the third display scheme different than the first display scheme and the second display scheme.

8. The method of claim 1 , further comprising;
determining a second aircraft position of a second aircraft; and
displaying a second aircraft symbol on the map, the second aircraft symbol displayed in a position on the map indicative of the second aircraft position.

9. The method of claim 8 , further comprising; displaying a second intended route on the map indicative of an intended route of the second aircraft.

10. The method of claim 8 , further comprising; displaying the map, the first aircraft symbol, and the optimum speed range symbol in a third display scheme when there is a danger of collision between the first aircraft and the second aircraft.

11. An aircraft operating and position information display system, comprising:
an aircraft speed sensor configured to generate a first aircraft ground speed signal indicative of the speed of a first aircraft;
a GPS system configured to generate a first aircraft position signal indicative of a geographic position of the first aircraft at an airport;
a controller including an aircraft performance model configured to predict a ground optimum speed range for the first aircraft; and an airport database including map data of the airport, the map data including geographic locations and dimensions of runways and taxiways, and wherein the controller is configured to generate display signals as a function of the first aircraft ground speed signal, the first aircraft position signal, the ground optimum speed range, and the map data; and
a first display unit configured to display as a function of the display signals;
a map of at least part of the airport, including runways and taxiways, from map data in an airport database;
a first aircraft symbol on the map, the first aircraft symbol displayed in a position on the map indicative of position of the first aircraft; and
an optimum speed range symbol, the optimum speed range symbol having a lower bound end and a higher bound end, on the map; and
wherein the optimum speed range symbol is displayed in a position on the map such that the first aircraft symbol is between the lower bound end and the higher bound end when the first aircraft speed is within the optimum speed range.

12. The system of claim 11 , wherein the first display unit is located in the flight deck of the first aircraft.

13. The system of claim 11 , further comprising a receiver configured to receive a second aircraft position signal from a second aircraft at the airport; and
wherein the controller is configured to generate the display signals as a function of the first aircraft speed signal, the first aircraft position signal, the optimum taxi speed range, the map data, and the second aircraft position signal; and
wherein the display unit is configured to display a second aircraft symbol on the map in a position on the map indicative of a position of the second aircraft as a function of the display signals.

14. The system of claim 11 , further comprising at least one first aircraft operating parameter sensor configured to generate an operating parameter signal indicative of an operating parameter

Assignees

• Honeywell Int Inc

Inventors

• Olofinboba Olukayode
• Nutaro Joseph
• Pepitone David
• Jackson Patrick

Classifications

• G08G5/80

  Anti-collision systems · CPC title

• G08G5/723

  from the aircraft · CPC title

• G08G5/51

  for control when on the ground, e.g. taxiing or rolling · CPC title

• G08G5/26

  Transmission of traffic-related information between aircraft and ground stations · CPC title

• G08G5/25

  Transmission of traffic-related information between aircraft · CPC title