KR102284080B1 - 2채널 아키텍처 - Google Patents

2채널 아키텍처 Download PDF

Info

Publication number
KR102284080B1
KR102284080B1 KR1020177009173A KR20177009173A KR102284080B1 KR 102284080 B1 KR102284080 B1 KR 102284080B1 KR 1020177009173 A KR1020177009173 A KR 1020177009173A KR 20177009173 A KR20177009173 A KR 20177009173A KR 102284080 B1 KR102284080 B1 KR 102284080B1
Authority
KR
South Korea
Prior art keywords
processing unit
local
state
opposing
data
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
KR1020177009173A
Other languages
English (en)
Korean (ko)
Other versions
KR20170095183A (ko
Inventor
셀린느 리우
니콜라스 마르티
스테픈 랭포드
Original Assignee
사프란 일렉트로닉스 & 디펜스
사프란 헬리콥터 엔진스
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 사프란 일렉트로닉스 & 디펜스, 사프란 헬리콥터 엔진스 filed Critical 사프란 일렉트로닉스 & 디펜스
Publication of KR20170095183A publication Critical patent/KR20170095183A/ko
Application granted granted Critical
Publication of KR102284080B1 publication Critical patent/KR102284080B1/ko
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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)
KR1020177009173A 2014-09-05 2015-09-04 2채널 아키텍처 Active KR102284080B1 (ko)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1458354A FR3025617B1 (fr) 2014-09-05 2014-09-05 Architecture bi-voies
FR1458354 2014-09-05
PCT/FR2015/052344 WO2016034825A1 (fr) 2014-09-05 2015-09-04 Architecture bi-voies

Publications (2)

Publication Number Publication Date
KR20170095183A KR20170095183A (ko) 2017-08-22
KR102284080B1 true KR102284080B1 (ko) 2021-08-02

Family

ID=52692715

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020177009173A Active KR102284080B1 (ko) 2014-09-05 2015-09-04 2채널 아키텍처

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

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080205416A1 (en) * 2007-02-23 2008-08-28 Honeywell International, Inc. Flight control computers with ethernet based cross channel data links
FR2986398A1 (fr) * 2012-01-30 2013-08-02 Snecma Dispositif de securite pour la commande d'un moteur comprenant une redondance des acquisitions d'une mesure de capteurs

Family Cites Families (21)

* 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
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
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

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080205416A1 (en) * 2007-02-23 2008-08-28 Honeywell International, Inc. Flight control computers with ethernet based cross channel data links
FR2986398A1 (fr) * 2012-01-30 2013-08-02 Snecma Dispositif de securite pour la commande d'un moteur comprenant une redondance des acquisitions d'une mesure de capteurs

Also Published As

Publication number Publication date
KR20170095183A (ko) 2017-08-22
JP6484330B2 (ja) 2019-03-13
US20170277151A1 (en) 2017-09-28
CN107077103B (zh) 2020-10-13
FR3025617B1 (fr) 2016-12-16
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

Similar Documents

Publication Publication Date Title
KR102213762B1 (ko) 양방향 아키텍처를 구비한 리던던트 ccdl들
JP6484330B2 (ja) ２路アーキテクチャ
JP5337022B2 (ja) フォールト・トレランス・コンピューティング・システムにおけるエラー・フィルタリング
US9148297B2 (en) Information processor and control network system
US7020076B1 (en) Fault-tolerant communication channel structures
US8194533B2 (en) Fault tolerant data bus node and system
US9367375B2 (en) Direct connect algorithm
US10042812B2 (en) Method and system of synchronizing processors to the same computational point
US9747184B2 (en) Operation of I/O in a safe system
US20070220367A1 (en) Fault tolerant computing system
US10491317B2 (en) Method for operating a network arrangement, network system and network arrangement
US9665447B2 (en) Fault-tolerant failsafe computer system using COTS components
US9311212B2 (en) Task based voting for fault-tolerant fail safe computer systems

Legal Events

Date Code Title Description
PA0105 International application

St.27 status event code: A-0-1-A10-A15-nap-PA0105

T11-X000 Administrative time limit extension requested

St.27 status event code: U-3-3-T10-T11-oth-X000

T11-X000 Administrative time limit extension requested

St.27 status event code: U-3-3-T10-T11-oth-X000

P11-X000 Amendment of application requested

St.27 status event code: A-2-2-P10-P11-nap-X000

P13-X000 Application amended

St.27 status event code: A-2-2-P10-P13-nap-X000

PG1501 Laying open of application

St.27 status event code: A-1-1-Q10-Q12-nap-PG1501

A201 Request for examination
P11-X000 Amendment of application requested

St.27 status event code: A-2-2-P10-P11-nap-X000

P13-X000 Application amended

St.27 status event code: A-2-2-P10-P13-nap-X000

PA0201 Request for examination

St.27 status event code: A-1-2-D10-D11-exm-PA0201

E902 Notification of reason for refusal
PE0902 Notice of grounds for rejection

St.27 status event code: A-1-2-D10-D21-exm-PE0902

E13-X000 Pre-grant limitation requested

St.27 status event code: A-2-3-E10-E13-lim-X000

P11-X000 Amendment of application requested

St.27 status event code: A-2-2-P10-P11-nap-X000

P13-X000 Application amended

St.27 status event code: A-2-2-P10-P13-nap-X000

E701 Decision to grant or registration of patent right
PE0701 Decision of registration

St.27 status event code: A-1-2-D10-D22-exm-PE0701

GRNT Written decision to grant
PR0701 Registration of establishment

St.27 status event code: A-2-4-F10-F11-exm-PR0701

PR1002 Payment of registration fee

St.27 status event code: A-2-2-U10-U12-oth-PR1002

Fee payment year number: 1

R18-X000 Changes to party contact information recorded

St.27 status event code: A-5-5-R10-R18-oth-X000

PG1601 Publication of registration

St.27 status event code: A-4-4-Q10-Q13-nap-PG1601

R18-X000 Changes to party contact information recorded

St.27 status event code: A-5-5-R10-R18-oth-X000

PR1001 Payment of annual fee

St.27 status event code: A-4-4-U10-U11-oth-PR1001

Fee payment year number: 4

R18-X000 Changes to party contact information recorded

St.27 status event code: A-5-5-R10-R18-oth-X000

PR1001 Payment of annual fee

St.27 status event code: A-4-4-U10-U11-oth-PR1001

Fee payment year number: 5

U11 Full renewal or maintenance fee paid

Free format text: ST27 STATUS EVENT CODE: A-4-4-U10-U11-OTH-PR1001 (AS PROVIDED BY THE NATIONAL OFFICE)

Year of fee payment: 5

PR1001 Payment of annual fee

St.27 status event code: A-4-4-U10-U11-oth-PR1001

Fee payment year number: 6

U11 Full renewal or maintenance fee paid

Free format text: ST27 STATUS EVENT CODE: A-4-4-U10-U11-OTH-PR1001 (AS PROVIDED BY THE NATIONAL OFFICE)

Year of fee payment: 6