FR3091344B1 - Aéronef comprenant un système avionique avec dispositif de localisation améliorée - Google Patents

Aéronef comprenant un système avionique avec dispositif de localisation améliorée Download PDF

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Publication number
FR3091344B1
FR3091344B1 FR1900718A FR1900718A FR3091344B1 FR 3091344 B1 FR3091344 B1 FR 3091344B1 FR 1900718 A FR1900718 A FR 1900718A FR 1900718 A FR1900718 A FR 1900718A FR 3091344 B1 FR3091344 B1 FR 3091344B1
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France
Prior art keywords
location information
aircraft
avionics system
external equipment
unit
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Active
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FR1900718A
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English (en)
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FR3091344A1 (fr
Inventor
Loïc Davain
Thomas Salameh
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.)
Safran Electronics and Defense SAS
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Safran Electronics and Defense SAS
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Publication date
Application filed by Safran Electronics and Defense SAS filed Critical Safran Electronics and Defense SAS
Priority to PCT/EP2019/087047 priority Critical patent/WO2020136224A2/fr
Publication of FR3091344A1 publication Critical patent/FR3091344A1/fr
Application granted granted Critical
Publication of FR3091344B1 publication Critical patent/FR3091344B1/fr
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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
    • G01C21/166—Mechanical, construction or arrangement details of inertial navigation systems
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/07—Responding to the occurrence of a fault, e.g. fault tolerance
    • G06F11/16—Error detection or correction of the data by redundancy in hardware
    • G06F11/18—Error detection or correction of the data by redundancy in hardware using passive fault-masking of the redundant circuits
    • G06F11/183—Error detection or correction of the data by redundancy in hardware using passive fault-masking of the redundant circuits by voting, the voting not being performed by the redundant components

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Theoretical Computer Science (AREA)
  • Quality & Reliability (AREA)
  • General Engineering & Computer Science (AREA)
  • Navigation (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)

Abstract

Aéronef (0) comprenant un système avionique (1) qui comprend : - une unité de commande de vol (FCS) ; et - un dispositif de localisation (2) qui comporte une unité de calcul (3) et au moins deux centrales de navigation inertielle pour délivrer des informations brutes de localisation (PVA1, PVA2) à l’unité de calcul (3) qui est adaptée à déterminer une information fiabilisée de localisation (PVAN) de l’aéronef en utilisant certaines au moins desdites informations brutes de localisation (PVA1, PVA2). L’aéronef (1) comporte : - un équipement externe (4) au système avionique (1) comprenant au moins une unité de mesure inertielle (C) fournissant une information brute de localisation (PVA3) de l’équipement externe, l’unité de calcul (3) déterminant ladite information fiabilisée de localisation (PVAN) en utilisant cette information brute de localisation (PVA3) de l’équipement externe (4). FIGURE DE L’ABREGE : Fig. 1
FR1900718A 2018-12-28 2019-01-28 Aéronef comprenant un système avionique avec dispositif de localisation améliorée Active FR3091344B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/EP2019/087047 WO2020136224A2 (fr) 2018-12-28 2019-12-26 Aeronef comprenant un systeme avionique avec dispositif de localisation amelioree

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1874358A FR3091343A1 (fr) 2018-12-28 2018-12-28 Aéronef comprenant un système avionique avec dispositif de localisation améliorée
FR1874358 2018-12-28

Publications (2)

Publication Number Publication Date
FR3091344A1 FR3091344A1 (fr) 2020-07-03
FR3091344B1 true FR3091344B1 (fr) 2021-09-17

Family

ID=67262420

Family Applications (2)

Application Number Title Priority Date Filing Date
FR1874358A Pending FR3091343A1 (fr) 2018-12-28 2018-12-28 Aéronef comprenant un système avionique avec dispositif de localisation améliorée
FR1900718A Active FR3091344B1 (fr) 2018-12-28 2019-01-28 Aéronef comprenant un système avionique avec dispositif de localisation améliorée

Family Applications Before (1)

Application Number Title Priority Date Filing Date
FR1874358A Pending FR3091343A1 (fr) 2018-12-28 2018-12-28 Aéronef comprenant un système avionique avec dispositif de localisation améliorée

Country Status (1)

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FR (2) FR3091343A1 (fr)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7805245B2 (en) * 2007-04-18 2010-09-28 Honeywell International Inc. Inertial measurement unit fault detection isolation reconfiguration using parity logic
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
IL249050B (en) * 2016-11-17 2018-03-29 Elbit Systems Ltd Self-calibrating inertial measurement method and system

Also Published As

Publication number Publication date
FR3091343A1 (fr) 2020-07-03
FR3091344A1 (fr) 2020-07-03

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