FR2901363B1 - Dispositif de navigation aerienne a capteurs inertiels et recepteurs de radionavigation et procede de navigation aerienne utilisant de tels elements - Google Patents

Dispositif de navigation aerienne a capteurs inertiels et recepteurs de radionavigation et procede de navigation aerienne utilisant de tels elements

Info

Publication number
FR2901363B1
FR2901363B1 FR0604508A FR0604508A FR2901363B1 FR 2901363 B1 FR2901363 B1 FR 2901363B1 FR 0604508 A FR0604508 A FR 0604508A FR 0604508 A FR0604508 A FR 0604508A FR 2901363 B1 FR2901363 B1 FR 2901363B1
Authority
FR
France
Prior art keywords
elements
inertial sensors
aerial
navigation device
radionavigation receivers
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
FR0604508A
Other languages
English (en)
Other versions
FR2901363A1 (fr
Inventor
Jacques Coatantiec
Charles Dussurgey
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Thales SA
Original Assignee
Thales SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Thales SA filed Critical Thales SA
Priority to FR0604508A priority Critical patent/FR2901363B1/fr
Priority to CA002653123A priority patent/CA2653123A1/fr
Priority to US12/301,342 priority patent/US20120004846A1/en
Priority to PCT/EP2007/054858 priority patent/WO2007135115A1/fr
Priority to RU2008150349/09A priority patent/RU2434248C2/ru
Priority to EP07729302A priority patent/EP2021822A1/fr
Publication of FR2901363A1 publication Critical patent/FR2901363A1/fr
Application granted granted Critical
Publication of FR2901363B1 publication Critical patent/FR2901363B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/13—Receivers
    • G01S19/33—Multimode operation in different systems which transmit time stamped messages, e.g. GPS/GLONASS
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/165—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation combined with non-inertial navigation instruments
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/42—Determining position
    • G01S19/45—Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement
    • G01S19/47—Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Automation & Control Theory (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Navigation (AREA)
FR0604508A 2006-05-19 2006-05-19 Dispositif de navigation aerienne a capteurs inertiels et recepteurs de radionavigation et procede de navigation aerienne utilisant de tels elements Expired - Fee Related FR2901363B1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR0604508A FR2901363B1 (fr) 2006-05-19 2006-05-19 Dispositif de navigation aerienne a capteurs inertiels et recepteurs de radionavigation et procede de navigation aerienne utilisant de tels elements
CA002653123A CA2653123A1 (fr) 2006-05-19 2007-05-21 Dispositif de navigation aerienne a capteurs inertiels et recepteurs de radionavigation et procede de navigation aerienne utilisant de tels elements
US12/301,342 US20120004846A1 (en) 2006-05-19 2007-05-21 Air navigation device with inertial sensor units, radio navigation receivers, and air navigation technique using such elements
PCT/EP2007/054858 WO2007135115A1 (fr) 2006-05-19 2007-05-21 Dispositif de navigation aerienne a capteurs inertiels et recepteurs de radionavigation et procede de navigation aerienne utilisant de tels elements
RU2008150349/09A RU2434248C2 (ru) 2006-05-19 2007-05-21 Аэронавигационное устройство с инерционными датчиками и радионавигационными приемниками и способ аэронавигации, использующий такие элементы
EP07729302A EP2021822A1 (fr) 2006-05-19 2007-05-21 Dispositif de navigation aerienne a capteurs inertiels et recepteurs de radionavigation et procede de navigation aerienne utilisant de tels elements

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0604508A FR2901363B1 (fr) 2006-05-19 2006-05-19 Dispositif de navigation aerienne a capteurs inertiels et recepteurs de radionavigation et procede de navigation aerienne utilisant de tels elements

Publications (2)

Publication Number Publication Date
FR2901363A1 FR2901363A1 (fr) 2007-11-23
FR2901363B1 true FR2901363B1 (fr) 2010-04-23

Family

ID=37744271

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0604508A Expired - Fee Related FR2901363B1 (fr) 2006-05-19 2006-05-19 Dispositif de navigation aerienne a capteurs inertiels et recepteurs de radionavigation et procede de navigation aerienne utilisant de tels elements

Country Status (6)

Country Link
US (1) US20120004846A1 (fr)
EP (1) EP2021822A1 (fr)
CA (1) CA2653123A1 (fr)
FR (1) FR2901363B1 (fr)
RU (1) RU2434248C2 (fr)
WO (1) WO2007135115A1 (fr)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2866423B1 (fr) * 2004-02-13 2006-05-05 Thales Sa Dispositif de surveillance de l'integrite des informations delivrees par un systeme hybride ins/gnss
FR2949866B1 (fr) * 2009-09-10 2011-09-30 Thales Sa Systeme hybride et dispositif de calcul d'une position et de surveillance de son integrite.
FR2953013B1 (fr) * 2009-11-20 2012-05-25 Sagem Defense Securite Systeme de navigation inertie/gnss
EP2585852A1 (fr) * 2010-06-25 2013-05-01 Trusted Positioning Inc. Correcteur de portée d'ins de plateforme mobile (mpirc)
FR2977314B1 (fr) * 2011-06-29 2013-07-12 Ixblue Dispositif et procede de navigation integrant plusieurs systemes inertiels de navigation hybrides
FR2989174B1 (fr) * 2012-04-06 2016-12-09 Thales Sa Dispositif pour la determination d'informations de localisation et de references primaires inertielles pour un aeronef
US8949027B2 (en) * 2012-07-10 2015-02-03 Honeywell International Inc. Multiple truth reference system and method
FR2998958B1 (fr) * 2012-12-05 2019-10-18 Thales Procede de gestion de donnees air (air data) d'un aeronef
FR3004826B1 (fr) * 2013-04-18 2015-05-08 Sagem Defense Securite Procede de controle d'integrite et dispositif de fusion-consolidation comprenant un pluralite de modules de traitement
FR3008818B1 (fr) * 2013-07-22 2015-08-14 Airbus Operations Sas Dispositif et procede de prediction au sol de la precision, l'integrite et la disponibilite de la position d'un aeronef le long d'une trajectoire.
FR3020469B1 (fr) * 2014-04-28 2016-05-13 Sagem Defense Securite Procede et dispositif de controle d'integrite a double niveau de consolidation
DE102014217196A1 (de) * 2014-08-28 2016-03-03 Meteomatics Gmbh Sicherheitsvorrichtung und Sicherheitsverfahren für ein Fluggerät, und Fluggerät mit der Sicherheitsvorrichtung
FR3026495B1 (fr) * 2014-09-25 2019-05-31 Thales Procede et dispositif de verification d'integrite d'informations de position obtenues par au moins deux dispositifs de geolocalisation par satellite
FR3030058B1 (fr) 2014-12-11 2016-12-09 Airbus Helicopters Dispositif redondant de capteurs de pilotage pour aeronef a voiture tournante
FR3038048B1 (fr) 2015-06-23 2017-07-07 Sagem Defense Securite Systeme inertiel de mesure pour aeronef
US10514260B2 (en) 2015-10-16 2019-12-24 Safran Electronics & Defense Integrity control method and merging/consolidation device comprising a plurality of processing modules
DE102016201980A1 (de) 2015-11-12 2017-05-18 Continental Teves Ag & Co. Ohg System zum Plausibilisieren von Satellitensignalen globaler Navigationssysteme
CN106289251A (zh) * 2016-08-24 2017-01-04 中船重工西安东仪科工集团有限公司 一种微小型惯性传感器组合结构
RU2646957C1 (ru) * 2016-11-03 2018-03-12 Открытое акционерное общество Московский научно-производственный комплекс "Авионика" имени О.В. Успенского (ОАО МНПК "Авионика") Комплексный способ навигации летательных аппаратов
CN107656300B (zh) * 2017-08-15 2020-10-02 东南大学 基于北斗/gps双模软件接收机的卫星/惯性超紧组合方法
FR3075356B1 (fr) * 2017-12-14 2020-07-17 Safran Electronics & Defense Systeme de navigation adapte pour mettre en oeuvre un traitement de fusion ou de consolidation
EP3998453A1 (fr) * 2021-03-12 2022-05-18 Lilium eAircraft GmbH Procédé et ensemble permettant de surveiller l'intégrité des mesures de position et de vitesse inertielles d'un aéronef
CN114279311A (zh) * 2021-12-27 2022-04-05 深圳供电局有限公司 一种基于惯性的gnss变形监测方法与***

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6317688B1 (en) * 2000-01-31 2001-11-13 Rockwell Collins Method and apparatus for achieving sole means navigation from global navigation satelite systems
US6424914B1 (en) * 2000-12-26 2002-07-23 American Gnc Corporation Fully-coupled vehicle positioning method and system thereof
FR2830320B1 (fr) * 2001-09-28 2003-11-28 Thales Sa Centrale de navigation inertielle hybryde a integrite amelioree
US6654685B2 (en) * 2002-01-04 2003-11-25 The Boeing Company Apparatus and method for navigation of an aircraft
US20030135327A1 (en) * 2002-01-11 2003-07-17 Seymour Levine Low cost inertial navigator
SE0300303D0 (sv) * 2003-02-06 2003-02-06 Nordnav Technologies Ab A navigation Method and Apparatus
US7248964B2 (en) * 2003-12-05 2007-07-24 Honeywell International Inc. System and method for using multiple aiding sensors in a deeply integrated navigation system
US7107833B2 (en) * 2003-12-23 2006-09-19 Honeywell International Inc. Inertial reference unit with internal backup attitude heading reference system
FR2866423B1 (fr) * 2004-02-13 2006-05-05 Thales Sa Dispositif de surveillance de l'integrite des informations delivrees par un systeme hybride ins/gnss
IL169408A (en) * 2004-06-28 2010-02-17 Northrop Grumman Corp System for navigation redundancy
FR2878953B1 (fr) * 2004-12-03 2007-01-26 Thales Sa Architecture d'un systeme embarque d'aide au pilotage d'un aeronef
US7328104B2 (en) * 2006-05-17 2008-02-05 Honeywell International Inc. Systems and methods for improved inertial navigation
FR2906893B1 (fr) * 2006-10-06 2009-01-16 Thales Sa Procede et dispositif de surveillance de l'integrite des informations delivrees par un systeme hybride ins/gnss
FR2949866B1 (fr) * 2009-09-10 2011-09-30 Thales Sa Systeme hybride et dispositif de calcul d'une position et de surveillance de son integrite.
FR2953013B1 (fr) * 2009-11-20 2012-05-25 Sagem Defense Securite Systeme de navigation inertie/gnss

Also Published As

Publication number Publication date
EP2021822A1 (fr) 2009-02-11
US20120004846A1 (en) 2012-01-05
RU2434248C2 (ru) 2011-11-20
RU2008150349A (ru) 2010-06-27
FR2901363A1 (fr) 2007-11-23
WO2007135115A1 (fr) 2007-11-29
CA2653123A1 (fr) 2007-11-29

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