ATE557301T1 - Hybrides system und vorrichtung zur berechnung der position und zur überwachung der integrität - Google Patents

Hybrides system und vorrichtung zur berechnung der position und zur überwachung der integrität

Info

Publication number
ATE557301T1
ATE557301T1 AT10176028T AT10176028T ATE557301T1 AT E557301 T1 ATE557301 T1 AT E557301T1 AT 10176028 T AT10176028 T AT 10176028T AT 10176028 T AT10176028 T AT 10176028T AT E557301 T1 ATE557301 T1 AT E557301T1
Authority
AT
Austria
Prior art keywords
extended
preset
hybrid system
probability
hybrid solution
Prior art date
Application number
AT10176028T
Other languages
English (en)
Inventor
Jacques Coatantiec
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
Application granted granted Critical
Publication of ATE557301T1 publication Critical patent/ATE557301T1/de

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
    • G01S19/38—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
    • 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
    • G01S19/20—Integrity monitoring, fault detection or fault isolation of space segment
    • 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
    • G01S19/01—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

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)
  • Computer Security & Cryptography (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Navigation (AREA)
  • Emergency Protection Circuit Devices (AREA)
AT10176028T 2009-09-10 2010-09-09 Hybrides system und vorrichtung zur berechnung der position und zur überwachung der integrität ATE557301T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0904328A FR2949866B1 (fr) 2009-09-10 2009-09-10 Systeme hybride et dispositif de calcul d'une position et de surveillance de son integrite.

Publications (1)

Publication Number Publication Date
ATE557301T1 true ATE557301T1 (de) 2012-05-15

Family

ID=42238287

Family Applications (1)

Application Number Title Priority Date Filing Date
AT10176028T ATE557301T1 (de) 2009-09-10 2010-09-09 Hybrides system und vorrichtung zur berechnung der position und zur überwachung der integrität

Country Status (5)

Country Link
US (1) US9146322B2 (de)
EP (1) EP2299287B1 (de)
AT (1) ATE557301T1 (de)
CA (1) CA2714822C (de)
FR (1) FR2949866B1 (de)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2901363B1 (fr) * 2006-05-19 2010-04-23 Thales Sa Dispositif de navigation aerienne a capteurs inertiels et recepteurs de radionavigation et procede de navigation aerienne utilisant de tels elements
FR2947901B1 (fr) * 2009-07-10 2012-03-23 Sagem Defense Securite Procede de determination de parametres de navigation d'un porteur et dispositif d'hybridation
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
US9560619B2 (en) * 2012-06-28 2017-01-31 Koninklijke Philips N.V. Method of estimating the position of a device and an apparatus implementing the same
US8949027B2 (en) * 2012-07-10 2015-02-03 Honeywell International Inc. Multiple truth reference system and method
US9547086B2 (en) 2013-03-26 2017-01-17 Honeywell International Inc. Selected aspects of advanced receiver autonomous integrity monitoring application to kalman filter based navigation filter
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.
FR3012619B1 (fr) * 2013-10-31 2016-01-22 Sagem Defense Securite Procede de controle d'integrite de mesures satellites
US9784844B2 (en) 2013-11-27 2017-10-10 Honeywell International Inc. Architectures for high integrity multi-constellation solution separation
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
FR3028310A1 (fr) * 2014-11-07 2016-05-13 Thales Sa Procede de dertemination d'un rayon de protection associe a un parametre de navigation d'un systeme hybride de navigation inertielle, et systeme associe
FR3030058B1 (fr) 2014-12-11 2016-12-09 Airbus Helicopters Dispositif redondant de capteurs de pilotage pour aeronef a voiture tournante
US10889302B2 (en) 2018-06-27 2021-01-12 Honeywell International Inc. Methods for monitoring the output performance of state estimators in navigation systems
US11168986B2 (en) * 2019-02-13 2021-11-09 Rockwell Collins, Inc. Navigation system and method
US11320540B2 (en) * 2019-04-10 2022-05-03 Honeywell International Inc. Integrity monitoring of primary and derived parameters
CN110068840B (zh) * 2019-05-15 2020-12-29 北京航空航天大学 一种基于伪距测量特征值提取的araim故障检测方法
FR3114164B1 (fr) * 2020-09-17 2022-08-12 Thales Sa Procede de controle d'integrite du recalage sur une pluralite d'amers, produit programme d'ordinateur et dispositif de controle d'integrite associes
US12442936B2 (en) * 2021-06-14 2025-10-14 Honeywell International Inc. Inertial coasting position and velocity solution separation
CN114692465B (zh) * 2022-04-15 2023-09-08 石家庄铁道大学 桥梁损伤位置的无损识别方法、存储介质及设备
CN116244955B (zh) * 2023-03-10 2026-03-24 中国人民解放军海军工程大学 一种惯性平台加速度计故障注入模拟方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5702070A (en) * 1995-09-20 1997-12-30 E-Systems, Inc. Apparatus and method using relative GPS positioning for aircraft precision approach and landing
US6570531B1 (en) * 2000-04-27 2003-05-27 Rockwell Collins, Inc. Satellite navigation receiver designed for compatibility with aircraft automatic landing systems
US7328104B2 (en) * 2006-05-17 2008-02-05 Honeywell International Inc. Systems and methods for improved inertial navigation
FR2901363B1 (fr) * 2006-05-19 2010-04-23 Thales Sa Dispositif de navigation aerienne a capteurs inertiels et recepteurs de radionavigation et procede de navigation aerienne utilisant de tels elements
US7702460B2 (en) * 2006-06-17 2010-04-20 Northrop Grumman Guidance And Electronics Company, Inc. Estimate of relative position between navigation units
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

Also Published As

Publication number Publication date
EP2299287B1 (de) 2012-05-09
US9146322B2 (en) 2015-09-29
FR2949866A1 (fr) 2011-03-11
FR2949866B1 (fr) 2011-09-30
US20110084874A1 (en) 2011-04-14
CA2714822C (en) 2018-01-02
EP2299287A1 (de) 2011-03-23
CA2714822A1 (en) 2011-03-10

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