DE602005014441D1 - Architektur eines Bordsystems zur Unterstützung der Steuerung von Luftschiffen - Google Patents

Architektur eines Bordsystems zur Unterstützung der Steuerung von Luftschiffen

Info

Publication number
DE602005014441D1
DE602005014441D1 DE602005014441T DE602005014441T DE602005014441D1 DE 602005014441 D1 DE602005014441 D1 DE 602005014441D1 DE 602005014441 T DE602005014441 T DE 602005014441T DE 602005014441 T DE602005014441 T DE 602005014441T DE 602005014441 D1 DE602005014441 D1 DE 602005014441D1
Authority
DE
Germany
Prior art keywords
airships
architecture
control
system supporting
board system
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
DE602005014441T
Other languages
English (en)
Inventor
Jean-Pierre Arethens
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
Publication of DE602005014441D1 publication Critical patent/DE602005014441D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Navigation (AREA)
DE602005014441T 2004-12-03 2005-11-29 Architektur eines Bordsystems zur Unterstützung der Steuerung von Luftschiffen Active DE602005014441D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0412890A FR2878953B1 (fr) 2004-12-03 2004-12-03 Architecture d'un systeme embarque d'aide au pilotage d'un aeronef

Publications (1)

Publication Number Publication Date
DE602005014441D1 true DE602005014441D1 (de) 2009-06-25

Family

ID=34954785

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005014441T Active DE602005014441D1 (de) 2004-12-03 2005-11-29 Architektur eines Bordsystems zur Unterstützung der Steuerung von Luftschiffen

Country Status (4)

Country Link
US (1) US7447590B2 (de)
EP (1) EP1679567B1 (de)
DE (1) DE602005014441D1 (de)
FR (1) FR2878953B1 (de)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
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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
FR2901893B1 (fr) * 2006-06-06 2008-09-12 Airbus France Sas Dispositif de surveillance d'informations de commande d'un aeronef
FR2905006B1 (fr) * 2006-08-21 2008-10-17 Airbus France Sas Procede de surveillance de l'integrite d'une position avion calculee a bord
FR2908904B1 (fr) * 2006-11-21 2009-02-06 Airbus France Sa Systeme de pilotage d'un aeronef comportant une base de donnees aeronautique.
US7970503B2 (en) * 2007-09-12 2011-06-28 The Boeing Company Method and apparatus for detecting anomalies in landing systems utilizing a global navigation satellite system
FR2922641B1 (fr) * 2007-10-23 2010-01-22 Airbus France Procede et dispositif de recalage de la position d'un aeronef.
CA2721830C (en) * 2008-04-21 2017-06-20 Bombardier Inc. Integrity monitoring of inertial reference unit
FR2930987B1 (fr) * 2008-05-06 2010-05-28 Airbus France Dispositif d'aide a la navigation et au guidage d'un aeronef, et systeme comportant un tel dispositif
US9308879B2 (en) * 2008-08-06 2016-04-12 Honeywell International Inc. Method, system, and apparatus of vehicle and fleet operator profile automation and deployment
US8204635B2 (en) * 2008-12-16 2012-06-19 Honeywell International Inc. Systems and methods of redundancy for aircraft inertial signal data
FR2953013B1 (fr) * 2009-11-20 2012-05-25 Sagem Defense Securite Systeme de navigation inertie/gnss
US9568321B2 (en) 2010-04-19 2017-02-14 Honeywell International Inc. Systems and methods for determining inertial navigation system faults
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.
FR2968784B1 (fr) * 2010-12-09 2014-07-18 Airbus Operations Sas Procede et dispositif de surveillance automatique d'ordres de guidage lateraux d'un aeronef.
FR2970093B1 (fr) * 2011-01-05 2013-12-13 Airbus Operations Sas Procede et dispositif de surveillance automatique d'operations aeriennes necessitant une garantie de performance de navigation et de guidage.
DE102011103875A1 (de) * 2011-06-10 2012-12-13 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zur Bestimmung der aktuellen Position eines Luftfahrzeuges
FR2977314B1 (fr) * 2011-06-29 2013-07-12 Ixblue Dispositif et procede de navigation integrant plusieurs systemes inertiels de navigation hybrides
FR3002032B1 (fr) * 2013-02-08 2016-02-12 Dassault Aviat Systeme et procede d'aide a la navigation d'un aeronef
US8862290B1 (en) * 2013-04-18 2014-10-14 Ge Aviation Systems Llc Flight system for an aircraft having an autoland system
KR101715336B1 (ko) * 2014-10-31 2017-03-10 한국항공우주연구원 항공기 착륙을 위한 통합 착륙 수신 장치 및 그 제어 방법
FR3028975B1 (fr) * 2014-11-26 2016-12-02 Thales Sa Procede de detection d'erreur d'un systeme de gestion de vol et de guidage d'un aeronef et syteme de gestion de vol et de guidage a haute integrite
CN104898678B (zh) * 2015-03-30 2017-06-06 北京航天自动控制研究所 一种运载火箭飞行控制的冗余诊断方法
US10175694B2 (en) * 2016-11-01 2019-01-08 The Boeing Company Flight control system with synthetic inertial localizer deviation and method of use
US10924180B2 (en) * 2017-05-05 2021-02-16 Via Space Networks Inc. Low latency satellite communication relay network
US10571914B2 (en) * 2017-06-29 2020-02-25 The Boeing Company Fault coverage for multiple failures in redundant systems
US11168986B2 (en) 2019-02-13 2021-11-09 Rockwell Collins, Inc. Navigation system and method
US11645928B2 (en) 2020-09-28 2023-05-09 Honeywell International Inc. Method of using multiple approach guidance systems to provide higher integrity with improved performance and availability

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5719764A (en) * 1995-07-19 1998-02-17 Honeywell Inc. Fault tolerant inertial reference system
FR2749666B1 (fr) 1996-06-07 1998-09-11 Sextant Avionique Recepteur de signaux de satellites avec controle d'integrite et exclusion d'axes defectueux
FR2749665B1 (fr) 1996-06-07 1998-09-11 Sextant Avionique Recepteur de signaux de satellites avec controle d'integrite de calcul de vitesse
FR2749667B1 (fr) 1996-06-07 1998-09-11 Sextant Avionique Recepteur de signaux de satellites avec detecteur d'incoherence entre mesures phase de code et de porteuse
FR2749668B1 (fr) 1996-06-07 1998-08-28 Sextant Avionique Recepteur de signaux de satellites avec filtre d'extrapolation de position
US5923286A (en) * 1996-10-23 1999-07-13 Honeywell Inc. GPS/IRS global position determination method and apparatus with integrity loss provisions
US5969668A (en) * 1997-07-29 1999-10-19 Rockwell International Corporation Integration of aime augmentation into GNSS products
FR2772928B1 (fr) 1997-12-23 2000-03-03 Sextant Avionique Station emettrice de signaux de correction vers un recepteur de navigation
US6178363B1 (en) * 1998-12-22 2001-01-23 The Boeing Company Inertially augmented GPS landing system
US6239745B1 (en) * 1999-07-30 2001-05-29 Rockwell Collins, Inc. Satellite landing system having instrument landing system look alike guidance
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
US6549829B1 (en) * 2001-10-31 2003-04-15 The Boeing Company Skipping filter for inertially augmented landing system
FR2832005B1 (fr) 2001-11-07 2004-01-30 Thales Sa Procede de surveillance au sol des anomalies de type ewf d'un signal de satellite de localisation
FR2852686B1 (fr) * 2003-03-19 2005-08-05 Airbus France Systeme de pilotage d'un aeronef, au moins pour piloter l'aeronef lors d'une approche de non precision en vue d'un atterrissage.
FR2861051B1 (fr) 2003-10-17 2006-03-03 Thales Sa Procede de guidage d'un aeronef en phase d'approche et balise sol correspondante
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

Also Published As

Publication number Publication date
US7447590B2 (en) 2008-11-04
EP1679567A2 (de) 2006-07-12
FR2878953B1 (fr) 2007-01-26
FR2878953A1 (fr) 2006-06-09
US20060167619A1 (en) 2006-07-27
EP1679567A3 (de) 2008-05-28
EP1679567B1 (de) 2009-05-13

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