FR3025617B1 - Architecture bi-voies - Google Patents

Architecture bi-voies

Info

Publication number
FR3025617B1
FR3025617B1 FR1458354A FR1458354A FR3025617B1 FR 3025617 B1 FR3025617 B1 FR 3025617B1 FR 1458354 A FR1458354 A FR 1458354A FR 1458354 A FR1458354 A FR 1458354A FR 3025617 B1 FR3025617 B1 FR 3025617B1
Authority
FR
France
Prior art keywords
track architecture
architecture
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
FR1458354A
Other languages
English (en)
French (fr)
Other versions
FR3025617A1 (fr
Inventor
Celine Liu
Nicolas Marti
Stephen Langford
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 Helicopter Engines SAS
Safran Electronics and Defense SAS
Original Assignee
Sagem Defense Securite SA
Turbomeca 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
Priority to FR1458354A priority Critical patent/FR3025617B1/fr
Application filed by Sagem Defense Securite SA, Turbomeca SA filed Critical Sagem Defense Securite SA
Priority to CA2960107A priority patent/CA2960107C/fr
Priority to RU2017111184A priority patent/RU2679706C2/ru
Priority to KR1020177009173A priority patent/KR102284080B1/ko
Priority to CN201580051534.XA priority patent/CN107077103B/zh
Priority to EP15780914.6A priority patent/EP3189381B1/fr
Priority to PCT/FR2015/052344 priority patent/WO2016034825A1/fr
Priority to US15/508,455 priority patent/US10162314B2/en
Priority to JP2017512804A priority patent/JP6484330B2/ja
Publication of FR3025617A1 publication Critical patent/FR3025617A1/fr
Application granted granted Critical
Publication of FR3025617B1 publication Critical patent/FR3025617B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B9/00—Safety arrangements
    • G05B9/02—Safety arrangements electric
    • G05B9/03—Safety arrangements electric with multiple-channel loop, i.e. redundant control systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B19/00—Program-control systems
    • G05B19/02—Program-control systems electric
    • G05B19/04—Program control other than numerical control, i.e. in sequence controllers or logic controllers
    • G05B19/048—Monitoring; Safety
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; 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
    • G06F11/14—Error detection or correction of the data by redundancy in operations
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; 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
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; 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
    • G06F11/2002—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 interconnections or communication control functionality are redundant
    • G06F11/2007—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 interconnections or communication control functionality are redundant using redundant communication media
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; 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
    • G06F11/2028—Failover techniques eliminating a faulty processor or activating a spare
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; 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
    • G06F11/2033—Failover techniques switching over of hardware resources
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; 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
    • G06F11/2097—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 maintaining the standby controller/processing unit updated
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/30—Monitoring
    • G06F11/3003—Monitoring arrangements specially adapted to the computing system or computing system component being monitored
    • G06F11/3013—Monitoring arrangements specially adapted to the computing system or computing system component being monitored where the computing system is an embedded system, i.e. a combination of hardware and software dedicated to perform a certain function in mobile devices, printers, automotive or aircraft systems
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/30—Monitoring
    • G06F11/3089—Monitoring arrangements determined by the means or processing involved in sensing the monitored data, e.g. interfaces, connectors, sensors, probes, agents
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D2045/0085—Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00—Program-control systems
    • G05B2219/20—Pc systems
    • G05B2219/23—Pc programming
    • G05B2219/23316—Standby, inactive, sleep or active, operation mode
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00—Program-control systems
    • G05B2219/20—Pc systems
    • G05B2219/24—Pc safety
    • G05B2219/24182—Redundancy
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00—Program-control systems
    • G05B2219/20—Pc systems
    • G05B2219/25—Pc structure of the system
    • G05B2219/25144—Between microcomputers, processors
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00—Program-control systems
    • G05B2219/20—Pc systems
    • G05B2219/25—Pc structure of the system
    • G05B2219/25163—Transmit twice, redundant, same data on different channels, check each channel
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00—Program-control systems
    • G05B2219/20—Pc systems
    • G05B2219/25—Pc structure of the system
    • G05B2219/25174—Ethernet

Landscapes

  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Quality & Reliability (AREA)
  • General Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Computing Systems (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mathematical Physics (AREA)
  • Safety Devices In Control Systems (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Hardware Redundancy (AREA)
  • Small-Scale Networks (AREA)
FR1458354A 2014-09-05 2014-09-05 Architecture bi-voies Active FR3025617B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR1458354A FR3025617B1 (fr) 2014-09-05 2014-09-05 Architecture bi-voies
RU2017111184A RU2679706C2 (ru) 2014-09-05 2015-09-04 Двухканальная архитектура
KR1020177009173A KR102284080B1 (ko) 2014-09-05 2015-09-04 2채널 아키텍처
CN201580051534.XA CN107077103B (zh) 2014-09-05 2015-09-04 双向架构
CA2960107A CA2960107C (fr) 2014-09-05 2015-09-04 Architecture bi-voies
EP15780914.6A EP3189381B1 (fr) 2014-09-05 2015-09-04 Architecture bi-voies
PCT/FR2015/052344 WO2016034825A1 (fr) 2014-09-05 2015-09-04 Architecture bi-voies
US15/508,455 US10162314B2 (en) 2014-09-05 2015-09-04 Two-way architecture
JP2017512804A JP6484330B2 (ja) 2014-09-05 2015-09-04 ２路アーキテクチャ

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1458354A FR3025617B1 (fr) 2014-09-05 2014-09-05 Architecture bi-voies

Publications (2)

Publication Number Publication Date
FR3025617A1 FR3025617A1 (fr) 2016-03-11
FR3025617B1 true FR3025617B1 (fr) 2016-12-16

Family

ID=52692715

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1458354A Active FR3025617B1 (fr) 2014-09-05 2014-09-05 Architecture bi-voies

Country Status (9)

Country Link
US (1) US10162314B2 (enExample)
EP (1) EP3189381B1 (enExample)
JP (1) JP6484330B2 (enExample)
KR (1) KR102284080B1 (enExample)
CN (1) CN107077103B (enExample)
CA (1) CA2960107C (enExample)
FR (1) FR3025617B1 (enExample)
RU (1) RU2679706C2 (enExample)
WO (1) WO2016034825A1 (enExample)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3025617B1 (fr) * 2014-09-05 2016-12-16 Sagem Defense Securite Architecture bi-voies
US11283556B2 (en) * 2016-06-10 2022-03-22 Tttech Flexibilis Oy Receiving frames at redundant port connecting node to communications network
GB2563242B (en) 2017-06-07 2020-01-29 Ge Aviat Systems Ltd A method and system for enabling component monitoring redundancy in a digital network of intelligent sensing devices
EP3428748B1 (de) * 2017-07-13 2020-08-26 Siemens Aktiengesellschaft Verfahren und anordnung zum betrieb von zwei redundanten systemen
US10698752B2 (en) * 2017-10-26 2020-06-30 Bank Of America Corporation Preventing unauthorized access to secure enterprise information systems using a multi-intercept system
IT201900012900A1 (it) * 2019-07-25 2021-01-25 Hitachi Rail Sts S P A Apparato e metodo per il controllo di un sistema ferroviario
CN113900979B (zh) * 2021-09-08 2024-03-19 中国航空工业集团公司西安航空计算技术研究所 一种双功能区共单ccdl传输体系
GB2615072A (en) 2022-01-24 2023-08-02 Airbus Operations Ltd An aircraft control system
CN115469531A (zh) * 2022-10-25 2022-12-13 亿航智能设备（广州）有限公司 一种多飞控备份切换方法、设备及计算机可读存储介质

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0410832A (ja) * 1990-04-27 1992-01-16 Nec Commun Syst Ltd パケットネットワークシステムのバックアップ方式
US5790791A (en) * 1995-05-12 1998-08-04 The Boeing Company Apparatus for synchronizing flight management computers where only the computer chosen to be the master received pilot inputs and transfers the inputs to the spare
EP0900415B1 (en) * 1996-05-14 2002-09-11 The Boeing Company Flight management system providing for automatic control display unit backup utilizing structured data routing
US6611499B1 (en) * 1999-03-18 2003-08-26 At&T Corp. Method for measuring the availability of router-based connectionless networks
JP4478037B2 (ja) * 2004-01-30 2010-06-09 日立オートモティブシステムズ株式会社 車両制御装置
FR2879388B1 (fr) * 2004-12-15 2007-03-16 Sagem Procede de transmission securisee, systeme, pare-feu et routeur le mettant en oeuvre
US20060184253A1 (en) * 2005-02-03 2006-08-17 International Business Machines Corporation Intelligent method of organizing and presenting operational mode information on an instrument panel of a flight deck
US7346793B2 (en) * 2005-02-10 2008-03-18 Northrop Grumman Corporation Synchronization of multiple operational flight programs
US7620465B2 (en) * 2005-02-28 2009-11-17 Delphi Technologies, Inc. Fault-tolerant node architecture for distributed systems
JP4754993B2 (ja) * 2006-02-16 2011-08-24 デルファイ・テクノロジーズ・インコーポレーテッド 分布システムのためのフォールトトレランスのノードアーキテクチャー
US20080205416A1 (en) * 2007-02-23 2008-08-28 Honeywell International, Inc. Flight control computers with ethernet based cross channel data links
RU2378521C2 (ru) * 2007-12-25 2010-01-10 Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "САЛЮТ") Система автоматического управления газотурбинным двигателем
JP5404101B2 (ja) * 2009-02-27 2014-01-29 三菱重工業株式会社 多重冗長系制御システム
FR2943036B1 (fr) * 2009-03-11 2011-04-15 Airbus France Systeme distribue de commande de vol implemente selon une architecture avionique modulaire integree.
FR2959489B1 (fr) * 2010-05-03 2013-02-15 Airbus Operations Sas Panneau de commande pour aeronef.
US9625894B2 (en) * 2011-09-22 2017-04-18 Hamilton Sundstrand Corporation Multi-channel control switchover logic
JP6227239B2 (ja) * 2011-11-16 2017-11-08 ナブテスコ株式会社 航空機制御装置及び航空機制御システム
FR2983319B1 (fr) * 2011-11-25 2014-02-07 Turbomeca Procede et systeme de regulation de puissance en cas de defaillance d'au moins un moteur d'aeronef
FR2986398B1 (fr) * 2012-01-30 2014-03-07 Snecma Dispositif de securite pour la commande d'un moteur comprenant une redondance des acquisitions d'une mesure de capteurs
RU136011U1 (ru) * 2012-12-27 2013-12-27 Российская Федерация в лице Министерства промышленности и торговли Российской Федерации Самолет с системой управления общесамолетным оборудованием и самолетными системами
EP2790073A1 (en) * 2013-04-09 2014-10-15 Airbus Operations GmbH Control of aircraft systems with at least two remote data concentrators for control of an aircraft system component
CN103955188B (zh) * 2014-04-24 2017-02-15 清华大学 支持冗余切换功能的控制系统及方法
FR3025617B1 (fr) * 2014-09-05 2016-12-16 Sagem Defense Securite Architecture bi-voies

Also Published As

Publication number Publication date
KR20170095183A (ko) 2017-08-22
JP6484330B2 (ja) 2019-03-13
US20170277151A1 (en) 2017-09-28
KR102284080B1 (ko) 2021-08-02
CN107077103B (zh) 2020-10-13
US10162314B2 (en) 2018-12-25
JP2017534502A (ja) 2017-11-24
EP3189381A1 (fr) 2017-07-12
RU2679706C2 (ru) 2019-02-12
CA2960107C (fr) 2020-03-10
WO2016034825A1 (fr) 2016-03-10
RU2017111184A3 (enExample) 2018-10-05
RU2017111184A (ru) 2018-10-05
CN107077103A (zh) 2017-08-18
CA2960107A1 (fr) 2016-03-10
EP3189381B1 (fr) 2018-07-25
FR3025617A1 (fr) 2016-03-11

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