Method for validating at least one predetermined position data stored in an aircraft database, associated computer program and device

US11789927B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11789927-B2
Application numberUS-202016935960-A
CountryUS
Kind codeB2
Filing dateJul 22, 2020
Priority dateJul 24, 2019
Publication dateOct 17, 2023
Grant dateOct 17, 2023

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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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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The invention relates to a method for validating at least one position stored in a database of an aircraft comprising a satellite positioning system, the database containing at least one radionavigation beacon position, a runway threshold position, and a displaced runway threshold position on a runway, on which the aircraft is intended to land, the validation of said at least one position comprising a consistency check between at least:a signal received by the aircraft from a radionavigation beacon associated with said at least one position, andthe position of the aircraft provided by the satellite positioning system, andthe value of the position stored in the database.

First claim

Opening claim text (preview).

The invention claimed is: 1. Method for validating at least one predetermined position data item stored in a database of an aircraft, the aircraft comprising a satellite positioning system, the database containing at least one radionavigation beacon position, a runway threshold position, and a displaced runway threshold position, of a runway on which the aircraft is intended to land, the validation method being implemented by an electronic validation device on board the aircraft and configured to access the database, the validation of said at least one predetermined position data item comprising a consistency check between at least: a signal received by the aircraft from a radionavigation beacon associated with said at least one predetermined position data item, and the position of the aircraft provided by the satellite positioning system, and the value of the predetermined position data item stored in the database, wherein said at least one predetermined position data item stored in the database corresponds to an element belonging to the group comprising at least: a position of a runway alignment radio beacon associated with said runway, a position of a glide path alignment radio beacon associated with said runway, a position of Distance Measuring Equipment associated with said runway, a position of the runway threshold, a position of the displaced runway threshold, and wherein, when said at least one predetermined position data item stored in the database corresponds to the position of the runway alignment radio beacon, the verification of consistency comprises, prior to interception by the aircraft of the runway axis, when the value of the signal received by the aircraft from the runway alignment radio beacon lies between two first predetermined signal values where the signal has a linear variation: the determination of a virtual point located on the perpendicular to the runway axis passing through the runway threshold, the distance on the ground from this virtual point to the center of the runway threshold being proportional to the value of the signal received by the aircraft from the runway alignment radio beacon, the calculation of an estimated position of the runway alignment radio beacon corresponding to the intersection of the first straight line passing through the virtual point and the position of the aircraft, with the second straight line passing through the runway threshold and the displaced runway threshold, the determination of a distance between the estimated position of the runway alignment radio beacon and the orthogonal projection on the runway longitudinal axis of the position of the runway alignment radio beacon stored in the database, the validation of the orthogonal projection, on the runway longitudinal axis, of the position of the runway alignment radio beacon stored in the database, if the distance is less than a first predetermined distance value. 2. Validation method according to claim 1 , wherein the calculation of the distance between the estimated position of the runway alignment radio beacon and the orthogonal projection on the runway longitudinal axis of the position of the runway alignment radio beacon stored in the database, is cyclically reiterated. 3. Validation method according to claim 1 , wherein when said at least one predetermined position data item stored in the database corresponds to: a position of the runway alignment radio beacon, and a position of the runway threshold, and a position of the displaced runway threshold, the consistency check comprises, as of the position of the aircraft, and after interception by the aircraft of the runway axis when the value of the signal received by the aircraft from the runway alignment radio beacon is equal to zero up to a first predetermined uncertainty factor, at least one calculation of the bearing of the aircraft with respect to: the runway threshold, the displaced runway threshold, the runway alignment radio beacon. 4. Validation method according to claim 3 , wherein the consistency check further comprises: the validation, within a first predetermined margin of error, of the position, laterally to the runway axis, of the runway alignment radio beacon, and the position, laterally to the runway axis, of the runway threshold, and of the position, laterally to the runway axis, of the displaced runway threshold stored in the database, in the event of equality of: the true runway heading, obtained from the runway threshold and the displaced runway threshold, with the bearings of the aircraft with respect to the runway threshold, to the displaced runway threshold, to the runway alignment radio beacon, and/or the validation, within a second predetermined margin of error, of the position, laterally to the runway axis, of the alignment radio beacon, and of the position, laterally to the runway axis, of the runway threshold, and of the position, laterally to the runway axis, of the displaced runway threshold stored in the database, in the event of equality of: the heading of a path followed by the aircraft provided by the satellite positioning system when the aircraft is previously established and stabilized at the center of the beam of the runway alignment radio beacon, with the bearings of the aircraft with respect to the runway threshold, to the displaced runway threshold, and to the runway alignment radio beacon. 5. Validation method according to claim 1 , wherein when said at least one position data item corresponds to: a position of the glide path alignment radio beacon, and/or a position of the Distance Measuring Equipment, the consistency check comprises, after interception by the aircraft of the runway axis when the value of the signal received by the aircraft from the alignment radio beacon is equal to zero up to a second predetermined uncertainty factor, and when the value of the signal received by the aircraft from the glide path beacon is equal to zero up to a third predetermined uncertainty factor, one or more calculations for distinct positions of the aircraft: a first distance on the ground between the aircraft and the glide path alignment radio beacon and/or the Distance Measuring Equipment respectively, by using a distance supplied by the Distance Measuring Equipment and a predetermined aircraft approach slope value or by using: the altitude of the aircraft provided by the positioning system, an altitude of the glide path alignment radio beacon and/or Distance Measuring Equipment stored in the database, a predetermined aircraft approach slope value, and a second distance on the ground between the aircraft and the glide path alignment radio beacon and/or the Distance Measuring Equipment, respectively, from: latitude and longitude coordinates of the glide path alignment radio beacon and/or the Distance Measuring Equipment stored in the database, the position of the aircraft, and the validation of the position, longitudinally to the runway axis, of the glide path alignment radio beacon and/or the Distance Measuring Equipment respectively, stored in the database, when the difference, or the average difference, between the first distance on the ground and the second distance on the ground associated with the same position of the aircraft, is less than a second predetermined distance value. 6. Validation method according to claim 5 , in which the consistency verification further comprises the preliminary calculation of the longitudinal distance on the runway axis between the runway threshold and the glide path alignment radio beacon, from the latitude and longitude coordinates of the runway threshold and from the glide path alignment radio beacon stored in the database, and, in case of validation of the position, longitudinally to the runway axis, of the g

Assignees

Inventors

Classifications

  • Ensuring data consistency and integrity · CPC title

  • Landing aids; Safety measures to prevent collision with earth's surface · CPC title

  • Aircraft landing systems · CPC title

  • Geographical information databases · CPC title

  • G01S1/14Primary

    using amplitude comparison of signals transmitted simultaneously from antennas or antenna systems having differently oriented overlapping directivity-characteristics · CPC title

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What does patent US11789927B2 cover?
The invention relates to a method for validating at least one position stored in a database of an aircraft comprising a satellite positioning system, the database containing at least one radionavigation beacon position, a runway threshold position, and a displaced runway threshold position on a runway, on which the aircraft is intended to land, the validation of said at least one position compr…
Who is the assignee on this patent?
Thales Sa
What technology area does this patent fall under?
Primary CPC classification G06F16/2365. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Oct 17 2023 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 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).