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Extract from the Register of European Patents

EP About this file: EP4285159

EP4285159 - DEVICE FOR DETERMINING THE ATTITUDE OF A CARRIER, AND ASSOCIATED SYSTEM FOR ASSISTING WITH THE PILOTING OF A CARRIER AND DETERMINATION METHOD [Right-click to bookmark this link]
StatusRequest for examination was made
Status updated on  03.11.2023
Database last updated on 11.09.2024
FormerThe international publication has been made
Status updated on  05.08.2022
Formerunknown
Status updated on  11.02.2022
Most recent event   Tooltip05.04.2024Change: Validation statespublished on 08.05.2024  [2024/19]
05.04.2024Change - extension statespublished on 08.05.2024  [2024/19]
Applicant(s)For all designated states
THALES
Tour Carpe Diem
Place des Corolles
Esplanade Nord
92400 Courbevoie / FR
[2023/49]
Inventor(s)01 / DEPRAZ, David
26000 VALENCE / FR
02 / MEHLEN, Christian
26000 VALENCE / FR
 [2023/49]
Representative(s)Lavoix
2, place d'Estienne d'Orves
75441 Paris Cedex 09 / FR
[2023/49]
Application number, filing date22702271.228.01.2022
[2023/49]
WO2022EP52005
Priority number, dateFR2021000086429.01.2021         Original published format: FR 2100864
[2023/49]
Filing languageFR
Procedural languageFR
PublicationType: A1 Application with search report
No.:WO2022162123
Date:04.08.2022
Language:FR
[2022/31]
Type: A1 Application with search report 
No.:EP4285159
Date:06.12.2023
Language:FR
The application published by WIPO in one of the EPO official languages on 04.08.2022 takes the place of the publication of the European patent application.
[2023/49]
Search report(s)International search report - published on:EP04.08.2022
ClassificationIPC:G01S19/53, G01C21/00
[2023/49]
CPC:
G01S19/53 (EP); G01S19/55 (US); G01S19/36 (EP,US);
G01C21/005 (EP)
Designated contracting statesAL,   AT,   BE,   BG,   CH,   CY,   CZ,   DE,   DK,   EE,   ES,   FI,   FR,   GB,   GR,   HR,   HU,   IE,   IS,   IT,   LI,   LT,   LU,   LV,   MC,   MK,   MT,   NL,   NO,   PL,   PT,   RO,   RS,   SE,   SI,   SK,   SM,   TR [2023/49]
TitleGerman:VORRICHTUNG ZUR BESTIMMUNG DER LAGE EINES TRÄGERS UND ZUGEHÖRIGES SYSTEM ZUR UNTERSTÜTZUNG DER FÜHRUNG EINES TRÄGERS UND BESTIMMUNGSVERFAHREN[2023/49]
English:DEVICE FOR DETERMINING THE ATTITUDE OF A CARRIER, AND ASSOCIATED SYSTEM FOR ASSISTING WITH THE PILOTING OF A CARRIER AND DETERMINATION METHOD[2023/49]
French:DISPOSITIF DE DÉTERMINATION DE L'ATTITUDE D'UN PORTEUR, ET SYSTÈME D'AIDE AU PILOTAGE D'UN PORTEUR ET PROCÉDÉ DE DÉTERMINATION ASSOCIÉS[2023/49]
Entry into regional phase27.07.2023National basic fee paid 
27.07.2023Designation fee(s) paid 
27.07.2023Examination fee paid 
Examination procedure27.07.2023Examination requested  [2023/49]
27.07.2023Date on which the examining division has become responsible
07.12.2023Amendment by applicant (claims and/or description)
Fees paidRenewal fee
26.12.2023Renewal fee patent year 03
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Cited inInternational search[A]WO9628747  (INTERVAL RESEARCH CORP [US]) [A] 1-13 * abstract * * figures 1-9b * * page 1, line 5 - page 4, line 9 * * page 13, line 28 - page 16, line 25 *;
 [A]EP1775599  (LOCATA CORP [US]) [A] 1-13 * abstract * * figures 1-10 * * paragraphs [0001] - [0022] - [0024] - [0025] - [0028] , [0034] - [0037] * * claims 1-28 *;
 [I]EP2674783  (THALES SA [FR]) [I] 1-13 * abstract * * figures 1-7 * * paragraphs [0001] , [0008] , [0012] , [0013] , [0016] , [0021] , [0023] , [0028] - [0032] - [0050] , [0069] , [0076] * * claims 1-6 *;
 [A]EP2758805  (NOVATEL INC [CA]) [A] 1-13 * abstract * * figures 1-4 * * paragraphs [0001] - [0014] - [0 26] - [0029] * * claims 1-22 *;
 [A]  - BELOKONOV I V ET AL, "Estimation of the nanosatellite attitude and angular rate by analyzing the navigation spacecraft geometrical visibility using the controllable pattern of navigation antenna", 2017 24TH SAINT PETERSBURG INTERNATIONAL CONFERENCE ON INTEGRATED NAVIGATION SYSTEMS (ICINS), CONCERN CSRI ELEKTROPRIBOR, JSC, (20170529), doi:10.23919/ICINS.2017.7995676, pages 1 - 4, XP033133487 [A] 1-13 * abstract * * I. Introduction * * II. Mathematical statement of problem of the nanosatellite monoaxial attitude determination * * III. Algorithm of the nanosatellite monoaxial attitude determination according to the analysis of the NS geometrical visibility *

DOI:   http://dx.doi.org/10.23919/ICINS.2017.7995676
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