Frequency estimator for aeronautical communication

US9859958B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9859958-B2
Application numberUS-201514699353-A
CountryUS
Kind codeB2
Filing dateApr 29, 2015
Priority dateApr 30, 2014
Publication dateJan 2, 2018
Grant dateJan 2, 2018

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

A method and device are provided suited to estimating a frequency value for aeronautical communication between a first station and an airborne system moving in relation to the first station, the data being transmitted in the form of a succession of frames, a frame comprising at least one first header field of known data followed by one or more fields of unknown data, and having at least the following steps: Step 1: performance of a supervised correlation on the known data ( 300 ) of the header, and estimation of a first frequency range centered on a frequency ; Step 2: production of a blind correlation on at least all of the unknown data of a field of data, by looking for a correlation peak over the frequency range +/− , as determined in step 1, and by retaining of the frequency corresponding to the correlation peak.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method for estimating a frequency value for aeronautical communication between a first station and an airborne system moving in relation to the first station, data being transmitted in a form of a succession of frames, a frame comprising at least one first header field of known data followed by one or more fields of unknown data, at least one of the first station and the airborne system comprising a radiocommunication receiver, the method comprising at least the following steps being executed by the radiocommunication receiver: Step 1: performance of a supervised correlation on the known data of the header by the radiocommunication receiver, and estimation of a first frequency range centered on an estimated frequency having a precision of +/− by the radiocommunication receiver, and Step 2: production of a blind correlation on at least all of the unknown data of a field of data by the radiocommunication receiver, by looking for a correlation peak over the range centered on the frequency +/− , as determined in step 1, and by retaining the frequency corresponding to the correlation peak, said retained frequency being used for transmitting data between the first station and the airborne system, wherein the frame is modulated with a modulation by change of phase comprising a field of pilots ( 302 1 ) that is arranged before a field of data and in that it has at least the following steps: Step 1: performance of a supervised correlation by Fourier transform on the field of pilots ( 302 1 ), in order to obtain a range centered on an estimated frequency having a precision of +/− , and Step 2: use of the symbols of the modulated frame and use of the Fourier transform from the modulated symbols of the short frame, corresponding to the range centered on the frequency +/− defined in step 1, determination of the frequency corresponding to the maximum of the norm of the Fourier transform and deduction of the value of the Doppler effect therefrom. 2. The method according to claim 1 , wherein the frame is a frame of DVB-S2 type using a DVB-S2 QPSK type modulation t. 3. The method according to claim 2 , wherein it comprises at least the following steps: Step 1: estimation of the frequency , = MaxIndex ⁡ (  DFT ⁡ ( R ⁡ ( k ) * conj ⁡ ( Ref ⁡ ( k ) ) + BABG ⁡ ( k ) )  2 ) = MaxIndex ⁡ (  DFT ⁡ ( ⅇ ⅈ * 2 * π * Δ f * t * rect 90 ⁡ ( t ) + BABG ⁡ ( t ) )  2 ) = MaxIndex ⁡ (  sinc 90 * π ⁡ ( f - Δ f ) +

Assignees

Inventors

Classifications

  • detecting errors in frequency or phase · CPC title

  • Transmission in a satellite or space-based system · CPC title

  • using blind estimation · CPC title

  • H04B7/01Primary

    Reducing phase shift · CPC title

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

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US9859958B2 cover?
A method and device are provided suited to estimating a frequency value for aeronautical communication between a first station and an airborne system moving in relation to the first station, the data being transmitted in the form of a succession of frames, a frame comprising at least one first header field of known data followed by one or more fields of unknown data, and having at least the fol…
Who is the assignee on this patent?
Thales Sa
What technology area does this patent fall under?
Primary CPC classification H04W56/0035. Mapped technology areas include Electricity.
When was this patent published?
Publication date Tue Jan 02 2018 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).