FR2946769B1 - Procede et dispositif de reconfiguration d'avionique. - Google Patents

Procede et dispositif de reconfiguration d'avionique.

Info

Publication number
FR2946769B1
FR2946769B1 FR0954028A FR0954028A FR2946769B1 FR 2946769 B1 FR2946769 B1 FR 2946769B1 FR 0954028 A FR0954028 A FR 0954028A FR 0954028 A FR0954028 A FR 0954028A FR 2946769 B1 FR2946769 B1 FR 2946769B1
Authority
FR
France
Prior art keywords
avionics
reconfiguring
reconfiguring avionics
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
FR0954028A
Other languages
English (en)
Other versions
FR2946769A1 (fr
Inventor
Thierry Planche
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 FR0954028A priority Critical patent/FR2946769B1/fr
Priority to US12/816,769 priority patent/US20100318834A1/en
Publication of FR2946769A1 publication Critical patent/FR2946769A1/fr
Application granted granted Critical
Publication of FR2946769B1 publication Critical patent/FR2946769B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • G06F11/20—Error detection or correction of the data by redundancy in hardware using active fault-masking, e.g. by switching out faulty elements or by switching in spare elements
    • G06F11/202—Error detection or correction of the data by redundancy in hardware using active fault-masking, e.g. by switching out faulty elements or by switching in spare elements where processing functionality is redundant
    • G06F11/2023—Failover techniques
    • G06F11/2025—Failover techniques using centralised failover control functionality
    • 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
    • G06F11/20—Error detection or correction of the data by redundancy in hardware using active fault-masking, e.g. by switching out faulty elements or by switching in spare elements
    • G06F11/202—Error detection or correction of the data by redundancy in hardware using active fault-masking, e.g. by switching out faulty elements or by switching in spare elements where processing functionality is redundant
    • G06F11/2035—Error detection or correction of the data by redundancy in hardware using active fault-masking, e.g. by switching out faulty elements or by switching in spare elements where processing functionality is redundant without idle spare hardware
    • 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
    • G06F11/20—Error detection or correction of the data by redundancy in hardware using active fault-masking, e.g. by switching out faulty elements or by switching in spare elements
    • G06F11/202—Error detection or correction of the data by redundancy in hardware using active fault-masking, e.g. by switching out faulty elements or by switching in spare elements where processing functionality is redundant
    • G06F11/2038—Error detection or correction of the data by redundancy in hardware using active fault-masking, e.g. by switching out faulty elements or by switching in spare elements where processing functionality is redundant with a single idle spare processing component
    • 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
    • G06F11/20—Error detection or correction of the data by redundancy in hardware using active fault-masking, e.g. by switching out faulty elements or by switching in spare elements
    • G06F11/202—Error detection or correction of the data by redundancy in hardware using active fault-masking, e.g. by switching out faulty elements or by switching in spare elements where processing functionality is redundant
    • G06F11/2046—Error detection or correction of the data by redundancy in hardware using active fault-masking, e.g. by switching out faulty elements or by switching in spare elements where processing functionality is redundant where the redundant components share persistent storage

Landscapes

  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Quality & Reliability (AREA)
  • Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Hardware Redundancy (AREA)
FR0954028A 2009-06-16 2009-06-16 Procede et dispositif de reconfiguration d'avionique. Expired - Fee Related FR2946769B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0954028A FR2946769B1 (fr) 2009-06-16 2009-06-16 Procede et dispositif de reconfiguration d'avionique.
US12/816,769 US20100318834A1 (en) 2009-06-16 2010-06-16 Method and device for avionic reconfiguration

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0954028A FR2946769B1 (fr) 2009-06-16 2009-06-16 Procede et dispositif de reconfiguration d'avionique.

Publications (2)

Publication Number Publication Date
FR2946769A1 FR2946769A1 (fr) 2010-12-17
FR2946769B1 true FR2946769B1 (fr) 2011-07-01

Family

ID=41682526

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0954028A Expired - Fee Related FR2946769B1 (fr) 2009-06-16 2009-06-16 Procede et dispositif de reconfiguration d'avionique.

Country Status (2)

Country Link
US (1) US20100318834A1 (fr)
FR (1) FR2946769B1 (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012158081A1 (fr) 2011-05-17 2012-11-22 Saab Ab Système avionique réparti et procédé de sauvegarde de manipulation dans un système avionique
US20130181809A1 (en) * 2011-07-27 2013-07-18 Michael R. Lin SpaceCube MINI
US20140309818A1 (en) * 2013-04-15 2014-10-16 Hamilton Sundstrand Corporation Ram air turbine autodeployment logic
US9552271B1 (en) * 2014-06-06 2017-01-24 Rockwell Collins, Inc. Enhanced dispatch for integrated modular avionics solutions system and related method
CN104656439B (zh) * 2014-12-26 2017-07-28 北京控制工程研究所 一种基于故障可重构性约束的卫星控制系统方案优选方法
CN108108329B (zh) * 2017-11-09 2021-07-16 中国航空无线电电子研究所 Ima系统动态重构策略多特性分析方法
US11175937B2 (en) * 2018-03-30 2021-11-16 The Boeing Company Virtualized avionics systems for operational environments
TR201921508A2 (tr) * 2019-12-25 2021-07-26 Tusas Tuerk Havacilik Ve Uzay Sanayii Anonim Sirketi Bir birleştirilmiş aviyonik sistem mimarisi.
US11780603B2 (en) * 2020-11-02 2023-10-10 Ge Aviation Systems Llc Method for resiliency in compute resources in avionics
FR3118512B1 (fr) * 2020-12-30 2023-02-24 Thales Sa Procédé de contrôle d’un ensemble de cartes de calcul d’un serveur multimédia embarqué à bord d’un aéronef, programme d’ordinateur, dispositif électronique de contrôle, et serveur multimédia associés
EP4123458A1 (fr) * 2021-07-21 2023-01-25 Airbus Defence and Space S.A.U. Reconfiguration de l'avionique modulaire intégrée (ima) en vol
WO2023043406A1 (fr) * 2021-09-15 2023-03-23 Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi Architecture d'ordinateur avionique

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2590379B1 (fr) * 1985-11-20 1988-02-26 Aerospatiale Systeme pour la commande centralisee d'une pluralite d'appareils de radiocommunication et de radionavigation montes a bord d'un aeronef
US5531402A (en) * 1995-03-23 1996-07-02 Dahl; Robert M. Wireless flight control system
JP2002228552A (ja) * 2001-01-31 2002-08-14 Mazda Motor Corp 車両の遠隔故障診断用サーバ、車両の遠隔故障診断方法、遠隔故障診断用プログラム、車載の遠隔故障診断システム、及び、車両の遠隔故障診断システム
US6671589B2 (en) * 2001-02-13 2003-12-30 William Holst Method and apparatus to support remote and automatically initiated data loading and data acquisition of airborne computers using a wireless spread spectrum aircraft data services link
US7146260B2 (en) * 2001-04-24 2006-12-05 Medius, Inc. Method and apparatus for dynamic configuration of multiprocessor system
JP4923990B2 (ja) * 2006-12-04 2012-04-25 株式会社日立製作所 フェイルオーバ方法、およびその計算機システム。
JP5011073B2 (ja) * 2007-11-22 2012-08-29 株式会社日立製作所 サーバ切り替え方法、およびサーバシステム

Also Published As

Publication number Publication date
US20100318834A1 (en) 2010-12-16
FR2946769A1 (fr) 2010-12-17

Similar Documents

Publication Publication Date Title
FR2946769B1 (fr) Procede et dispositif de reconfiguration d'avionique.
FR2937208B1 (fr) Procede et dispositif de tele-visionnage
FR2902266B1 (fr) Procede et dispositif de repartition de la bande passante de communication
FR2897277B1 (fr) Procede et dispositif de separation.
FR2944598B1 (fr) Procede et dispositif de pesage
FR2949880B1 (fr) Dispositif configurable, systeme et procede de configuration.
FR2928093B1 (fr) Dispositif de separation de molecules et procede de fabrication.
FR2928077B1 (fr) Dispositif et procede de micro-elastographie.
FR2944111B1 (fr) Procede et systeme de saisie de l'environnement
FR2922391B1 (fr) Procede et dispositif de transmission de donnees
FR2939592B1 (fr) Procede et dispositif de communication par visioconference.
FR2943263B1 (fr) Dispositif de decoupe et procede de decoupe correspondant
FR2928021B1 (fr) Procede et dispositif de detection d'un aeronef environnant.
FR2984020B1 (fr) Dispositif et procede de configuration d'antenne
FR2923947B1 (fr) Procede et dispositif de gravure selective.
FR2946820B1 (fr) Procede de transmission de donnees et dispositif associe.
FR2902080B1 (fr) Dispositif et procede de suveillance d'un aeronef
FR2935493B1 (fr) Procede et dispositif de suivi d'antenne.
FR2912659B1 (fr) Dispositif implantable et procede de fabrication correspondant
FR2989193B1 (fr) Procede et dispositif de fourniture rapide d'information
FR2922641B1 (fr) Procede et dispositif de recalage de la position d'un aeronef.
FR2930099B1 (fr) Procede et dispositif de routage de donnees
FR2911436B1 (fr) Dispositif et procede de connexion
FR2934453B1 (fr) Procede et dispositif de masquage d'erreurs
FR2935133B1 (fr) Procede et dispositif d'etayage d'un aeronef

Legal Events

Date Code Title Description
CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14

ST Notification of lapse

Effective date: 20240205