Method and system for automatically modifying a lateral flight plan of an aircraft

Patent metadata

Field	Value
Publication number	US-9261369-B2
Application number	US-201414250562-A
Country	US
Kind code	B2
Filing date	Apr 11, 2014
Priority date	Apr 15, 2013
Publication date	Feb 16, 2016
Grant date	Feb 16, 2016

Abstract

A system for automatically modifying a lateral flight plan of an aircraft includes modifying means adapted to modify the flight plan by an action to chosen among the following actions: deleting, adding and moving at least one waypoint of an initial flight plan (T 1 ). The modified flight plan (T 3 ) includes one downstream waypoint (P 6 ) defined as the waypoint on which the aircraft gets back to the initial flight plan (T 1 ), and one upstream waypoint (P 4 ) preceding the downstream waypoint (P 6 ). By defining an intermediate point (P 5′ ) between the upstream (P 4 ) and downstream (P 6 ) waypoints, the coordinates are calculated in order to allow the aircraft to reach the downstream waypoint (P 6 ) with the same course as the initial flight plan (T 1 ).

First claim

The invention claimed is:

1. A method for automatically modifying a lateral flight plan of an aircraft, said flight plan being defined by a sequence of waypoints that the aircraft is to fly over and flight-path portions connecting the successive waypoints, wherein, for modifying a flight plan referred to as initial to become a modified flight plan, the method comprises:
performing, by a modification device, an action to be selected from the following actions: adding, deleting or moving at least one waypoint of the initial flight plan, said modified flight plan comprising a downstream waypoint defined as the waypoint at which the aircraft returns to the initial flight plan, and an upstream waypoint preceding the downstream waypoint, and
defining, by the modification device, an intermediate point between said upstream and downstream waypoints, of which the coordinates are calculated to allow the aircraft to arrive at said downstream waypoint on the same course as that provided by the initial flight plan,
wherein for defining the intermediate point, said method comprises:
defining, by the modification device, a first upstream circle having a first predetermined radius, passing through a crossing point of the aircraft located after the upstream waypoint and positioned such that the direction of the aircraft at said crossing point is tangential to said first circle;
defining, by the modification device, a second downstream circle having a second predetermined radius, passing through said downstream waypoint and positioned such that the flight path corresponding to the initial flight plan of the aircraft at said downstream waypoint is tangential to said second circle;
defining, by the modification device, a straight line tangential to said first and second circles, said tangential straight line being tangential to the first circle at a first point of intersection and to the second circle at a second point of intersection; and
defining, by the modification device, said intermediate point on said tangential straight line between said first and second points of intersection.

2. The method according to claim 1 , wherein said intermediate point is located at a distance from the second point of intersection corresponding to a predetermined straight-line-flight distance between the waypoints.

3. The method according to claim 1 , wherein said first and second radii of said first and second circles, respectively, are equal.

4. The method according to claim 1 , wherein said crossing point is positioned at a distance from the upstream waypoint corresponding to a predetermined straight-line-flight distance between the waypoints.

5. The method according to claim 1 , wherein the part of the lateral flight path corresponding to the modified flight plan of the aircraft up to the downstream waypoint follows in this order:
a first arc of said first circle, the first arc being defined between the crossing point and the first point of intersection;
the tangential straight line between the first point of intersection and the second point of intersection, passing through said intermediate point; and
a second arc of the second circle, the second arc being defined between said second point of intersection and said downstream waypoint.

6. The method according to claim 1 , wherein the flight plan is modified for a low-altitude section of flight.

7. A device for modifying a lateral flight plan of an aircraft, the flight plan being defined by a sequence of waypoints that the aircraft is to fly over and flight-path portions connecting the waypoints, the device comprising:
modification means configured to modify the flight plan by an action to be selected from the following actions:
deleting, adding and moving at least one waypoint of the initial flight plan, said modified flight plan comprising a downstream waypoint defined as the waypoint at which the aircraft returns to the initial flight plan, and
an upstream waypoint preceding the downstream waypoint, and by defining a new intermediate point between said upstream and downstream waypoints, of which the coordinates are calculated to allow the aircraft to arrive at said downstream waypoint on the same course as that of the initial flight plan,
wherein the modification means comprise elements for respectively: defining a first upstream circle having a first predetermined radius, passing through a crossing point of the aircraft located after the upstream waypoint and positioned such that the direction of the aircraft at said crossing point is tangential to said first circle;
defining a second downstream circle having a second predetermined radius, passing through said downstream waypoint and positioned such that the flight path corresponding to the initial flight plan of the aircraft at said downstream waypoint is tangential to said second circle;
defining a straight line tangential to said first and second circles, said tangential straight line being tangential to the first circle at a first point of intersection and to the second circle at a second point of intersection; and
defining said intermediate point on said tangential straight line, between said first and second points of intersection.

8. The device according to claim 7 , further comprising:
means for triggering the modification of the flight plan; and
means for transmitting the modified flight plan.

9. A flight management system comprising:
a device for modifying a lateral flight plan of an aircraft, the flight plan being defined by a sequence of waypoints that the aircraft is to fly over and flight-path portions connecting the waypoints, the device comprising:
modification means configured to modify the flight plan by an action to be selected from the following actions:
deleting, adding and moving at least one waypoint of the initial flight plan, said modified flight plan comprising a downstream waypoint defined as the waypoint at which the aircraft returns to the initial flight plan, and an upstream waypoint preceding the downstream waypoint, and
by defining a new intermediate point between said upstream and downstream waypoints, of which the coordinates are calculated to allow the aircraft to arrive at said downstream waypoint on the same course as that of the initial flight plan,
wherein the modification means comprise elements for respectively:
defining a first upstream circle having a first predetermined radius, passing through a crossing point of the aircraft located after the upstream waypoint and positioned such that the direction of the aircraft at said crossing point is tangential to said first circle;
defining a second downstream circle having a second predetermined radius, passing through said downstream waypoint and positioned such that the flight path corresponding to the initial flight plan of the aircraft at said downstream waypoint is tangential to said second circle;
defining a straight line tangential to said first and second circles, said tangential straight line being tangential to the first circle at a first point of intersection and to the second circle at a second point of intersection; and
defining said intermediate point on said tangential straight line, between said first and second points of intersection.

Assignees

• Airbus Operations Sas

Inventors

• Albert Nicolas
• Kozlow Boris
• Wachenheim Maxime

Classifications

• G01C21/20 Primary

  Instruments for performing navigational calculations (G01C21/24, G01C21/26 take precedence) · CPC title

• G08G5/21

  located onboard the aircraft · CPC title

• G08G5/34 Primary

  for flight plan modification · CPC title

• G08G5/0021

  Physics · mapped topic

• G08G5/0039

  Physics · mapped topic