Mobile multilateration systems and related methods

US2016309291A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016309291-A1
Application numberUS-201615098118-A
CountryUS
Kind codeA1
Filing dateApr 13, 2016
Priority dateApr 20, 2015
Publication dateOct 20, 2016
Grant date

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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.

Mobile multilateration systems and related methods are disclosed. An example method includes accessing multilateration data relating to a first aircraft using a time-difference-of-arrival determiner of a second aircraft; processing the multilateration data at the second aircraft to determine a calculated position of the first aircraft; comparing the calculated position of the first aircraft to an asserted position of the first aircraft stored at the second aircraft; and in response to the comparison, determining if the calculated position and the asserted position are within a threshold of one another using the time-difference-of-arrival determiner of the second aircraft to determine an authenticity of the first aircraft.

First claim

Opening claim text (preview).

What is claimed is: 1 . A method, comprising: accessing multilateration data relating to a first aircraft using a time-difference-of-arrival determiner of a second aircraft; processing the multilateration data at the second aircraft to determine a calculated position of the first aircraft; comparing the calculated position of the first aircraft to an asserted position of the first aircraft stored at the second aircraft; and in response to the comparison, determining if the calculated position and the asserted position are within a threshold of one another using the time-difference-of-arrival determiner of the second aircraft to determine an authenticity of the first aircraft. 2 . The method of claim 1 , further including, prior to accessing the multilateration data, determining at the second aircraft if a quantity of the multilateration data satisfies a threshold. 3 . The method of claim 2 , further including, in response to the quantity of the multilateration data not satisfying the threshold, transmitting a multilateration data request from the second aircraft to aircraft within a range of the second aircraft, where the range includes the first aircraft. 4 . The method of claim 3 , wherein the multilateration data request is a first multilateration data request, and prior to transmitting the first multilateration data request, waiting for a time period to deter the first multilateration data request from interfering with a second multilateration data request. 5 . The method of claim 3 , wherein the multilateration data includes first multilateration data, and further including receiving a response from a third aircraft including second multilateration data. 6 . The method of claim 5 , wherein the first and second multilateration data correspond to a time window. 7 . The method of claim 5 , wherein the processing of the multilateration data at the second aircraft includes processing the first and second multilateration data to determine the calculated position of the first aircraft. 8 . The method of claim 1 , wherein the multilateration data includes first multilateration data, and further including: receiving transmitted data from the first aircraft at the second aircraft, the transmitted data including an aircraft identification and positional information; and time stamping the transmitted data at the second aircraft to form second multilateration data. 9 . The method of claim 8 , wherein the processing of the multilateration data at the second aircraft includes processing the first and second multilateration data to determine the calculated position of the first aircraft. 10 . The method of claim 1 , further including identifying the first aircraft as being authenticate in response to determining that the calculated position is within the threshold of the asserted position. 11 . The method of claim 1 , further including identifying the first aircraft as not being authenticate in response to determining that the calculated position is outside of the threshold of the asserted position. 12 . The method of claim 1 , further including receiving a multilateration data request at the second aircraft from the first aircraft, and transmitting the multilateration data in response to the multilateration data request. 13 . An apparatus, comprising: a database of a first aircraft storing multilateration data, the multilateration data associated with a second aircraft; a processor to access the multilateration data, the processor to: process the multilateration data using a time-difference-of-arrival determiner of the processor to determine a calculated position of the second aircraft; compare the calculated position of the second aircraft to an asserted position of the second aircraft; and in response to the comparison, determine if the calculated position is within a threshold of the asserted position to determine an authenticity of the second aircraft. 14 . The apparatus of claim 13 , wherein the processor is to determine if a quantity of the multilateration data satisfies a threshold to determine the authenticity of the second aircraft. 15 . The apparatus of claim 14 , further including a requester to transmit a multilateration data request from the first aircraft to aircraft within a range of the first aircraft in response to the quantity of the multilateration data not satisfying the threshold. 16 . The apparatus of claim 15 , wherein the multilateration data request is a first multilateration data request, and further including a random request delayer to delay the transmission of the multilateration data request for a time period to deter the first multilateration data request from interfering with a second multilateration data request. 17 . The apparatus of claim 15 , wherein the multilateration data includes first multilateration data, further including a receiver to receive a response from a third aircraft including second multilateration data. 18 . The apparatus of claim 17 , wherein the processor is to process the first multilateration data and the second multilateration data using the time-difference-of-arrival determiner to determine the calculated position of the second aircraft. 19 . An article of manufacture comprising instructions that, when executed, cause a machine to at least: access multilateration data relating to a first aircraft at a second aircraft; process the multilateration data at the second aircraft to determine a calculated position of the first aircraft; compare the calculated position of the first aircraft to an asserted position of the first aircraft stored at the second aircraft; and in response to the comparison, determine if the calculated position and the asserted position are within a threshold of one another to determine an authenticity of the first aircraft. 20 . A method, comprising: receiving a message from a first aircraft at a second aircraft, the message including an aircraft identification of the first aircraft and an asserted position of the first aircraft; time stamping the message to form first multilateration data associated with the first aircraft; storing the first multilateration data in a database at the second aircraft; receiving second multilateration data from a third aircraft in response to transmitting a multilateration data request; storing the second multilateration data in the database at the second aircraft; associating the first multilateration data and the second multilateration data in response to the first and second multilateration data being associated with a time period and the first aircraft; determining a calculated position of the first aircraft at the second aircraft based on the first multilateration data and the second multilateration data; and identifying the first aircraft as not being authenticate in response to the asserted position and the calculated position being outside of a threshold.

Assignees

Inventors

Classifications

  • Airborne · CPC title

  • Transmission of traffic-related information between aircraft · CPC title

  • Communications with or from aircraft, i.e. aeronautical mobile service · CPC title

  • Selective distribution of broadcast services, e.g. multimedia broadcast multicast service [MBMS]; Services to user groups; One-way selective calling services · CPC title

  • H04W4/021Primary

    Services related to particular areas, e.g. point of interest [POI] services, venue services or geofences · CPC title

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What does patent US2016309291A1 cover?
Mobile multilateration systems and related methods are disclosed. An example method includes accessing multilateration data relating to a first aircraft using a time-difference-of-arrival determiner of a second aircraft; processing the multilateration data at the second aircraft to determine a calculated position of the first aircraft; comparing the calculated position of the first aircraft to …
Who is the assignee on this patent?
Boeing Co
What technology area does this patent fall under?
Primary CPC classification H04W4/021. Mapped technology areas include Electricity.
When was this patent published?
Publication date Thu Oct 20 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). 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).