Method and device for aiding the airport navigation

• US 8,346,464 B2
• Filed: 04/20/2009
• Issued: 01/01/2013
• Est. Priority Date: 04/22/2008
• Status: Expired due to Fees

• Current Assignee: Airbus Operations SAS (Airbus SE)
• Original Assignee: Airbus Operations SAS (Airbus SE)
• Inventors: Albert, Eric, Gauffriau, Adrien
• Primary Examiner(s): Joerger, Kaitlin
• Assistant Examiner(s): SUAREZ, ERNESTO A
• Application Number:
  US12/426,814
• Publication Number:
  US 20090265089A1
• Time in Patent Office: 1,352 Days
• Field of Search: 701/117, 701/120, 701/409, 701/431, 701/437, 701/439, 701/454
• US Class Current: 701/120
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/065 Navigation or guidance aids, e.g. for taxiing or rolling

Abstract

Disclosed is a method and device for aiding ground navigation of an aircraft on an airport in which a current position and current heading of the aircraft are determined by a set of information sources. A first determination unit determines, according to the determined current position and current heading, and according to information obtained from an airport database, a current traffic lane on which the aircraft is situated, and parameters relating to a next intersection of the current traffic lane. Parameters relating to the next intersection include the position of the next intersection; and the distance between the next intersection and the current position of the aircraft. A head-up display unit overlays, on an environment in front of the aircraft, a first symbol illustrating the determined current traffic lane and a set of second symbols illustrating the determined parameters of the next intersection.

Claims

1. A method for aiding ground navigation of an aircraft on an airport, the method comprising:

a) determining, by a set of information sources, current position and current heading of the aircraft;

b) determining, by a first determination unit, according to said determined current position and said determined current heading, and according to information obtained from an airport database, a current traffic lane of the airport on which the aircraft is situated, and parameters relating to a next intersection of the current traffic lane, wherein said parameters relating to the next intersection include the following;

position of the next intersection; and

distance between the next intersection and the current position of the aircraft; and

c) overlaying, by a head-up display unit, on an environment in front of the aircraft, a first symbol illustrating said determined current traffic lane, and a set of second symbols illustrating the determined parameters of the next intersection,

wherein;

the following parameters relating to the next intersection of the current traffic lane are determined by the first determination unit;

characteristics of traffic lanes that cross the current traffic lane at the next intersection; and

angles between the crossing traffic lanes and said current traffic lane; and

the following steps are carried out by the first determination unit;

α

) determining, according to the current traffic lane and the information of said airport database, a set of intersections on the current traffic lane;

β

) selecting from among the set of intersections, an intersection closest to the front of the aircraft, according to the determined current heading and the determined current position of the aircraft, obtained from the information of said airport database; and

γ

) determining, according to information of the airport database (3);

characteristics of the crossing traffic lanes at the selected closest intersection; and

angles between the crossing traffic lanes and the current traffic lane.

2. The method as claimed in claim 1,

wherein the traffic lanes and set of intersections of the airport are overlaid as an oriented graph, wherein the oriented graph includes vertices representing the traffic lanes and oriented arcs representing the set of intersections, with each arc being associated a name of the intersection, a geographical position of the intersection and angle between the traffic lanes.

3. The method as claimed in claim 2,

wherein, a definition of an intersection object is added to a database to obtain the oriented graph.

4. The method as claimed in claim 1,

wherein in said first symbol and said set of second symbols are overlaid at a fixed position on a transparent screen of said head-up display system.

5. The method as claimed in claim 1,

wherein in said first symbol and said set of second symbols are overlaid as a conformal representation in which said symbols are overlaid on the environment in front of the airplane at positions representative of actual positions on the airport.

6. The method as claimed in claim 1, wherein:

the current position of the aircraft is monitored and an alert signal is emitted when the aircraft is situated in proximity to a runway; and

when the alert signal is emitted, a third symbol indicating the alert signal is overlaid by said head-up display system on the environment in front of the aircraft.

7. The method as claimed in claim 1,

wherein auxiliary symbols illustrating respectively:

a current heading of the aircraft;

a current ground speed of the aircraft; and

an information cue relating to the acceleration or deceleration of the aircraft,

are determined and presented overlaid by said head-up display system on the environment in front of the aircraft.

8. A device for aiding ground navigation of an aircraft on an airport, said device comprising:

a set of information sources configured to determine current position and current heading of the aircraft;

an airport database, which comprises airport installation information;

a first determination unit configured to determine, according to said determined current position and said determined current heading, and according to said information from said airport database, a current traffic lane of the airport on which the aircraft is situated, and parameters relating to a next intersection of the current traffic lane, wherein said parameters relating to the next intersection include the following;

position of the next intersection; and

distance between the next intersection and the current position of the aircraft; and

a head-up display system configured to overlay, on an environment in front of the aircraft, a first symbol illustrating said current traffic lane determined by said first determination unit, and a set of second symbols illustrating the parameters of the next intersection determined by said first determination unit, wherein;

said first determination unit is further configured to determine the following parameters relating to the next intersection of the current traffic lane;

characteristics of traffic lanes that cross the current traffic lane at the next intersection, and

angles between the crossing traffic lanes and said current traffic lane; and

said first determination unit is additionally configured to carry out the following steps;

α

) determine, according to the current traffic lane and the information of said airport database, a set of intersections on the current traffic lane;

β

) select, from the set of intersections, an intersection closest to the front of the aircraft, according to the determined current heading and the determined current position of the aircraft, a position of each intersection in the set of intersections, obtained from the information from said airport database; and

said first determination unit is further configured to determine, according to information of the airport database;

characteristics of the crossing traffic lanes at the selected closest intersection; and

angles between the crossing traffic lanes and the current traffic lane.

9. The device as claimed in claim 8,

wherein said first determination unit forms a part of an onboard system for aiding ground navigation.

10. The device as claimed in claim 8,

wherein said head-up display system comprises a calculation unit, a projection unit and a transparent screen, and said first determination unit is integrated into said calculation unit of said head-up display system (7).