Method for determining an offset lateral trajectory for an aircraft

US9410807B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9410807-B2
Application numberUS-201313936034-A
CountryUS
Kind codeB2
Filing dateJul 5, 2013
Priority dateJul 6, 2012
Publication dateAug 9, 2016
Grant dateAug 9, 2016

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

In the field of the definition of a flight plan for an aircraft, a method is provided for determining an offset lateral trajectory from an initial lateral trajectory comprising a set of initial waypoints. The initial lateral trajectory and the offset lateral trajectory have two junction points in common, namely a point of entry and a point of exit. At least one of the junction points is distinct from the initial waypoints and from the current position of the aircraft. This first junction point can notably be defined so that the flight duration or the flight distance between the first and second junction points corresponds to a defined value.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method of determining and forwarding an offset lateral trajectory for an aircraft from an initial lateral trajectory comprising initial waypoints, the method being executed by a flight management system comprising at leak one processor and a storage device storing a navigation database storing waypoints, the offset lateral trajectory rejoining the initial lateral trajectory at first and second junction points, the method comprising: determining the first junction point within the initial lateral trajectory, the first junction point being different from the initial waypoints and from a current position of the aircraft, the first junction point being determined based on: a predetermined direction and a defined offset distance from said initial lateral trajectory, a predetermined flight duration on said offset lateral trajectory with an associated tolerance, or a predetermined flight distance on said offset lateral trajectory with associated tolerance, and a predetermined second junction point within the initial lateral trajectory; determining, and storing in the navigation database, an offset waypoint for each initial waypoint situated between the first and second junction points; defining a portion of the offset lateral trajectory passing through the offset waypoints, such that the portion of the offset lateral trajectory is the same offset distance from a corresponding portion of the initial lateral trajectory in the predetermined direction; and forwarding the determined offset lateral trajectory from the flight management system to an autopilot system of the aircraft to guide the aircraft along the determined offset lateral trajectory, wherein the first junction point is determined such that: a flight duration between the first and second junction points along the offset lateral trajectory or along said portion of the offset lateral trajectory is equal to the predetermined flight duration taking into account the associated tolerance, or a flight distance between the first and second junction points along the offset lateral trajectory or along said portion of the offset lateral trajectory is equal to the predetermined flight distance taking into account the associated tolerance. 2. The method according to claim 1 , wherein the first junction point forms a point of exit from the offset lateral trajectory. 3. The method according to claim 1 , wherein the first junction point forms a point of entry to the offset lateral trajectory.

Assignees

Inventors

Classifications

  • located onboard the aircraft · CPC title

  • G08G5/34Primary

    for flight plan modification · CPC title

  • Physics · mapped topic

  • G01C21/00Primary

    Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 (measuring distance traversed on the ground by a vehicle G01C22/00; control of position, course, altitude or attitude of vehicles G05D1/00; traffic control systems for road vehicles involving transmission of navigation instructions to the vehicle G08G1/0968) · CPC title

  • Physics · mapped topic

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What does patent US9410807B2 cover?
In the field of the definition of a flight plan for an aircraft, a method is provided for determining an offset lateral trajectory from an initial lateral trajectory comprising a set of initial waypoints. The initial lateral trajectory and the offset lateral trajectory have two junction points in common, namely a point of entry and a point of exit. At least one of the junction points is distinc…
Who is the assignee on this patent?
Thales Sa
What technology area does this patent fall under?
Primary CPC classification G08G5/34. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Aug 09 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).