FR3008818B1 - 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. - Google Patents

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.

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Publication number
FR3008818B1
FR3008818B1 FR1357191A FR1357191A FR3008818B1 FR 3008818 B1 FR3008818 B1 FR 3008818B1 FR 1357191 A FR1357191 A FR 1357191A FR 1357191 A FR1357191 A FR 1357191A FR 3008818 B1 FR3008818 B1 FR 3008818B1
Authority
FR
France
Prior art keywords
predicting
integrity
availability
precision
track
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.)
Active
Application number
FR1357191A
Other languages
English (en)
Other versions
FR3008818A1 (fr
Inventor
Philippe Gmerek
Jean-Damien Perrie
Alain Guillet
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1357191A priority Critical patent/FR3008818B1/fr
Priority to US14/334,812 priority patent/US9377306B2/en
Priority to CN201410427608.2A priority patent/CN104331593B/zh
Publication of FR3008818A1 publication Critical patent/FR3008818A1/fr
Application granted granted Critical
Publication of FR3008818B1 publication Critical patent/FR3008818B1/fr
Active 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
    • G01S19/14—Receivers specially adapted for specific applications
    • G01S19/15—Aircraft landing systems
    • 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
    • G01C21/20—Instruments for performing navigational calculations
    • 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
    • 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
    • G01S19/14—Receivers specially adapted for specific applications
    • G01S19/18—Military applications
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • G05D1/106—Change initiated in response to external conditions, e.g. avoidance of elevated terrain or of no-fly zones
FR1357191A 2013-07-22 2013-07-22 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. Active FR3008818B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1357191A FR3008818B1 (fr) 2013-07-22 2013-07-22 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.
US14/334,812 US9377306B2 (en) 2013-07-22 2014-07-18 Device and method for prediction on the ground of characteristics of the position of an aircraft along a path
CN201410427608.2A CN104331593B (zh) 2013-07-22 2014-07-22 用于地面预测航空器沿路径的定位的特征的设备和方法

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1357191A FR3008818B1 (fr) 2013-07-22 2013-07-22 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.

Publications (2)

Publication Number Publication Date
FR3008818A1 FR3008818A1 (fr) 2015-01-23
FR3008818B1 true FR3008818B1 (fr) 2015-08-14

Family

ID=49998321

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1357191A Active FR3008818B1 (fr) 2013-07-22 2013-07-22 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.

Country Status (3)

Country Link
US (1) US9377306B2 (fr)
CN (1) CN104331593B (fr)
FR (1) FR3008818B1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3044152A1 (fr) * 2015-11-19 2017-05-26 Direction Des Services De La Navigation Aerienne Station de reception de signaux pour un systeme de surveillance ads-b
US9922570B2 (en) * 2016-02-17 2018-03-20 Ge Aviation Systems, Llc Aircraft navigation performance prediction system
FR3053779B1 (fr) * 2016-07-07 2018-06-29 Thales Dispositif et methode de calcul de prediction de performance de navigation estimee
DE102018205430A1 (de) * 2018-04-11 2019-10-17 Robert Bosch Gmbh Verfahren zur satellitengestützten Ermittlung einer Fahrzeugposition
US11168986B2 (en) 2019-02-13 2021-11-09 Rockwell Collins, Inc. Navigation system and method
FR3099575B1 (fr) * 2019-07-31 2021-06-25 Safran Aircraft Engines Détection automatique d’une configuration hardware d’un équipement embarqué dans un aéronef
CN111780758A (zh) * 2020-07-08 2020-10-16 中国人民解放军海军工程大学 一种基于双模解算的重力稳定平台姿态确定方法及应用

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5436632A (en) * 1994-06-02 1995-07-25 Trimble Navigation Limited Integrity monitoring of differential satellite positioning system signals
US5623414A (en) * 1995-01-24 1997-04-22 Massachusetts Inst Technology Clock-aided satellite navigation receiver system for enhanced position estimation and integrity monitoring
US5923286A (en) * 1996-10-23 1999-07-13 Honeywell Inc. GPS/IRS global position determination method and apparatus with integrity loss provisions
US6711478B2 (en) * 2000-12-15 2004-03-23 Garmin At, Inc. Receiver-autonomous vertical integrity monitoring
US6804585B2 (en) * 2001-06-19 2004-10-12 John Jay Humbard Flight management system and method for providing navigational reference to emergency landing locations
FR2852683B1 (fr) * 2003-03-19 2005-05-20 Airbus France Procede et dispositif d'aide au pilotage d'un aeronef lors d'une approche de non precision pendant une phase d'atterrissage.
US7783425B1 (en) * 2005-06-29 2010-08-24 Rockwell Collins, Inc. Integrity-optimized receiver autonomous integrity monitoring (RAIM)
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
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
US7893890B2 (en) * 2007-03-05 2011-02-22 The Boeing Company Electrically dimmable combiner optics for head-up display
US7956802B1 (en) * 2007-05-21 2011-06-07 Rockwell Collins, Inc. Integrity-optimized receiver autonomous integrity monitoring (RAIM) for vertical integrity monitoring
FR2916530B1 (fr) * 2007-05-23 2009-07-10 Airbus France Sa Procede et dispositif pour surveiller une indication de position d'un aeronef.
FR2917853A1 (fr) * 2007-06-25 2008-12-26 Airbus France Sas Procede et dispositif pour determiner une position consolidee d'un mobile, en particulier d'un aeronef
FR2944888B1 (fr) 2009-04-28 2012-03-30 Thales Sa Procede d'aide a la navigation pour la determination de la trajectoire d'un aeronef
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.
CA2780675A1 (fr) * 2009-11-17 2011-05-26 Topcon Positioning Systems, Inc. Detection et correction de mesures anormales et resolution d'ambiguite dans recepteur de geolocalisation et navigation par systeme de satellites
FR2966259B1 (fr) * 2010-10-18 2012-11-30 Airbus Operations Sas Procede et dispositif d'aide a la conduite d'operations aeriennes necessitant une garantie de performance de navigation et de guidage.
CN102867073B (zh) * 2011-07-08 2014-12-24 中国民航科学技术研究院 一种基于性能导航的飞行程序设计系统及验证平台和验证方法
CN102385317B (zh) * 2011-09-01 2013-05-08 中国航空工业第六一八研究所 一种惯性导航系统的自动导航功能地面仿真试验方法
US20130138338A1 (en) * 2011-11-30 2013-05-30 Honeywell International Inc. Graphical presentation of receiver autonomous integrity monitoring outage regions on an aircraft display
DE102012007191B3 (de) * 2012-04-12 2013-06-20 Astrium Gmbh Verbesserung des Integritätskonzepts eines Satellitennavigationssystems

Also Published As

Publication number Publication date
FR3008818A1 (fr) 2015-01-23
CN104331593A (zh) 2015-02-04
US9377306B2 (en) 2016-06-28
US20150219460A1 (en) 2015-08-06
CN104331593B (zh) 2018-12-18

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