RU2670941C9 - Двухканальная архитектура с избыточными линиями связи ccdl - Google Patents
Двухканальная архитектура с избыточными линиями связи ccdl Download PDFInfo
- Publication number
- RU2670941C9 RU2670941C9 RU2017111197A RU2017111197A RU2670941C9 RU 2670941 C9 RU2670941 C9 RU 2670941C9 RU 2017111197 A RU2017111197 A RU 2017111197A RU 2017111197 A RU2017111197 A RU 2017111197A RU 2670941 C9 RU2670941 C9 RU 2670941C9
- Authority
- RU
- Russia
- Prior art keywords
- processing unit
- communication line
- control system
- communication
- flight control
- Prior art date
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—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme 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
- G06F11/16—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
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L12/00—Data switching networks
- H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
- H04L12/40—Bus networks
- H04L12/40169—Flexible bus arrangements
- H04L12/40176—Flexible bus arrangements involving redundancy
- H04L12/40182—Flexible bus arrangements involving redundancy by using a plurality of communication lines
-
- 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)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Theoretical Computer Science (AREA)
- Automation & Control Theory (AREA)
- General Engineering & Computer Science (AREA)
- Quality & Reliability (AREA)
- Signal Processing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Aviation & Aerospace Engineering (AREA)
- Hardware Redundancy (AREA)
- Small-Scale Networks (AREA)
- Safety Devices In Control Systems (AREA)
- Maintenance And Management Of Digital Transmission (AREA)
- Feedback Control In General (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Communication Control (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1458350 | 2014-09-05 | ||
| FR1458350A FR3025626B1 (fr) | 2014-09-05 | 2014-09-05 | Architecture bi-voies avec liaisons ccdl redondantes |
| PCT/FR2015/052342 WO2016034824A1 (fr) | 2014-09-05 | 2015-09-04 | Architecture bi-voies avec liaisons ccdl redondantes |
Publications (4)
| Publication Number | Publication Date |
|---|---|
| RU2017111197A RU2017111197A (ru) | 2018-10-05 |
| RU2017111197A3 RU2017111197A3 (enExample) | 2018-10-05 |
| RU2670941C2 RU2670941C2 (ru) | 2018-10-25 |
| RU2670941C9 true RU2670941C9 (ru) | 2018-11-26 |
Family
ID=52692714
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2017111197A RU2670941C9 (ru) | 2014-09-05 | 2015-09-04 | Двухканальная архитектура с избыточными линиями связи ccdl |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US10338560B2 (enExample) |
| EP (1) | EP3189380B1 (enExample) |
| JP (2) | JP2017530461A (enExample) |
| KR (2) | KR20170089835A (enExample) |
| CN (1) | CN107005446B (enExample) |
| CA (1) | CA2960093C (enExample) |
| FR (1) | FR3025626B1 (enExample) |
| RU (1) | RU2670941C9 (enExample) |
| WO (1) | WO2016034824A1 (enExample) |
Families Citing this family (28)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3025626B1 (fr) * | 2014-09-05 | 2017-11-03 | Sagem Defense Securite | Architecture bi-voies avec liaisons ccdl redondantes |
| CN107331185B (zh) * | 2017-08-16 | 2019-12-06 | 青岛海信网络科技股份有限公司 | 一种交通信号灯机的异常状态处理方法、主机及从机 |
| DE102018111338A1 (de) * | 2018-05-11 | 2019-11-14 | Liebherr-Aerospace Lindenberg Gmbh | System zum Steuern, Regeln und/oder Überwachen eines Luftfahrzeugs |
| EP3802322A4 (en) | 2018-05-31 | 2022-02-23 | Joby Aero, Inc. | POWER SYSTEM ARCHITECTURE AND FAULT TOLERANT VTOL AIRPLANE WITH IT |
| US12006048B2 (en) | 2018-05-31 | 2024-06-11 | Joby Aero, Inc. | Electric power system architecture and fault tolerant VTOL aircraft using same |
| CN112219036B (zh) | 2018-06-01 | 2023-08-11 | 杰欧比飞行有限公司 | 用于飞行器噪声减轻的系统和方法 |
| US10710741B2 (en) | 2018-07-02 | 2020-07-14 | Joby Aero, Inc. | System and method for airspeed determination |
| CN108924955B (zh) * | 2018-07-30 | 2021-12-14 | 山东大骋医疗科技有限公司 | 一种基于双链无线通信的ct数据传输与控制方法及装置 |
| DK201870684A1 (en) | 2018-08-27 | 2020-05-19 | Aptiv Technologies Limited | PARTITIONED WIRELESS COMMUNICATION SYSTEM WITH REDUNDANT DATA LINKS AND POWER LINES |
| US11099936B2 (en) * | 2018-09-11 | 2021-08-24 | Embraer S.A. | Aircraft integrated multi system electronic architecture |
| EP3853736B1 (en) * | 2018-09-17 | 2025-10-22 | Joby Aero, Inc. | Aircraft control system |
| WO2020180373A2 (en) | 2018-12-07 | 2020-09-10 | Joby Aero, Inc. | Aircraft control system and method |
| WO2020118310A1 (en) | 2018-12-07 | 2020-06-11 | Joby Aero, Inc. | Rotary airfoil and design method therefor |
| EP3899427B1 (en) | 2018-12-19 | 2025-09-03 | Joby Aero, Inc. | Vehicle navigation system |
| CN109707517B (zh) * | 2018-12-21 | 2021-06-25 | 中国航发控制系统研究所 | 一种控制双通道同步的方法及系统 |
| FR3094807B1 (fr) * | 2019-04-05 | 2021-03-12 | Safran Aircraft Engines | Dispositif de commande d'un moteur d'un aéronef comprenant deux voies de commande redondées |
| US11230384B2 (en) | 2019-04-23 | 2022-01-25 | Joby Aero, Inc. | Vehicle cabin thermal management system and method |
| US10960785B2 (en) | 2019-04-23 | 2021-03-30 | Joby Aero, Inc. | Battery thermal management system and method |
| WO2021025739A1 (en) | 2019-04-25 | 2021-02-11 | Joby Aero, Inc. | Vtol aircraft |
| US11491930B2 (en) * | 2019-12-03 | 2022-11-08 | Woodward, Inc. | Systems and methods for commanded or uncommanded channel switchover in a multiple processor controller |
| US11720067B2 (en) * | 2020-03-30 | 2023-08-08 | General Electric Company | Method for handling a simultaneous failure of all channels of a multi-channel engine controller for a gas turbine engine |
| EP4162473A4 (en) | 2020-06-05 | 2024-07-03 | Joby Aero, Inc. | Aircraft control system and method |
| CN113934153B (zh) * | 2020-06-29 | 2024-09-03 | 中国航发商用航空发动机有限责任公司 | 航空发动机控制系统的多通道仿真方法和系统 |
| CN112346331B (zh) * | 2020-11-18 | 2022-11-18 | 西安爱生技术集团公司 | 一种三余度飞控计算机的通道选择方法 |
| CN113824698B (zh) * | 2021-08-27 | 2023-04-07 | 中国航空无线电电子研究所 | 一种保障民用航空电子系统数据完整性的方法 |
| CN113504720A (zh) * | 2021-09-07 | 2021-10-15 | 中国商用飞机有限责任公司 | 一种基于分布式电传飞控架构的备份控制系统及工作方法 |
| FR3131401A1 (fr) * | 2021-12-24 | 2023-06-30 | Dassault Aviation | Architecture de commande virtualisee d un aeronef et procede associe. |
| CN116300627B (zh) * | 2023-03-24 | 2025-10-10 | 中国航发控制系统研究所 | 一种fadec系统双通道工作模式切换方法 |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5274554A (en) * | 1991-02-01 | 1993-12-28 | The Boeing Company | Multiple-voting fault detection system for flight critical actuation control systems |
| US20080205416A1 (en) * | 2007-02-23 | 2008-08-28 | Honeywell International, Inc. | Flight control computers with ethernet based cross channel data links |
| US20120297108A1 (en) * | 2009-12-16 | 2012-11-22 | Kawasaki Jukogyo Kabushiki Kaisha | Integrated electronic system mounted on aircraft |
| US8504178B2 (en) * | 2009-02-27 | 2013-08-06 | Mitsubishi Heavy Industries, Ltd. | Multiple redundant control system |
Family Cites Families (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2984715B2 (ja) * | 1988-04-12 | 1999-11-29 | 第一電気株式会社 | 航空機等空海交通機関の姿勢制御装置 |
| 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 |
| US6611499B1 (en) * | 1999-03-18 | 2003-08-26 | At&T Corp. | Method for measuring the availability of router-based connectionless networks |
| WO2003042928A2 (en) * | 2001-11-13 | 2003-05-22 | Goodrich Pump & Engine Control Systems, Inc. | Fault management system for gas turbine engines |
| US20040153700A1 (en) * | 2003-01-02 | 2004-08-05 | Nixon Mark J. | Redundant application stations for process control systems |
| KR100564758B1 (ko) * | 2003-12-12 | 2006-03-27 | 한국전자통신연구원 | 통신경로 이중화장치 및 이중화된 통신경로의 운용방법 |
| 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 |
| KR100603599B1 (ko) * | 2004-11-25 | 2006-07-24 | 한국전자통신연구원 | 이중화된 스위치 보드의 이중화 제어장치 및 그 방법 |
| 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 |
| FR2922959B1 (fr) * | 2007-10-31 | 2009-12-04 | Airbus France | Systeme de controle et procede de controle. |
| US8503484B2 (en) * | 2009-01-19 | 2013-08-06 | Honeywell International Inc. | System and method for a cross channel data link |
| CN102130722B (zh) * | 2011-03-01 | 2014-04-23 | 南京航空航天大学 | 用于光传飞行控制系统中的交叉通道数据链路系统 |
| 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 |
| 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 |
| US9449498B2 (en) * | 2012-08-17 | 2016-09-20 | Illinois Tool Works Inc. | Wireless communication network power optimization for control of industrial equipment in harsh environments |
| CN103853626A (zh) * | 2012-12-07 | 2014-06-11 | 深圳航天东方红海特卫星有限公司 | 一种星载电子设备的双工冗余备份总线通信方法及装置 |
| CN103441875A (zh) * | 2013-08-23 | 2013-12-11 | 中国铁道科学研究院 | 一种实现信号集中监测系统冗余通信的方法 |
| CN103490959B (zh) * | 2013-10-10 | 2016-12-07 | 北京航天发射技术研究所 | 一种双冗余can总线故障检测方法 |
| FR3025626B1 (fr) * | 2014-09-05 | 2017-11-03 | Sagem Defense Securite | Architecture bi-voies avec liaisons ccdl redondantes |
-
2014
- 2014-09-05 FR FR1458350A patent/FR3025626B1/fr active Active
-
2015
- 2015-09-04 JP JP2017512815A patent/JP2017530461A/ja active Pending
- 2015-09-04 EP EP15767223.9A patent/EP3189380B1/fr active Active
- 2015-09-04 CA CA2960093A patent/CA2960093C/fr active Active
- 2015-09-04 KR KR1020177007922A patent/KR20170089835A/ko not_active Ceased
- 2015-09-04 KR KR1020187021423A patent/KR102213762B1/ko active Active
- 2015-09-04 US US15/508,476 patent/US10338560B2/en active Active
- 2015-09-04 CN CN201580047789.9A patent/CN107005446B/zh active Active
- 2015-09-04 RU RU2017111197A patent/RU2670941C9/ru active
- 2015-09-04 WO PCT/FR2015/052342 patent/WO2016034824A1/fr not_active Ceased
-
2019
- 2019-07-12 JP JP2019130023A patent/JP2020030815A/ja active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5274554A (en) * | 1991-02-01 | 1993-12-28 | The Boeing Company | Multiple-voting fault detection system for flight critical actuation control systems |
| US20080205416A1 (en) * | 2007-02-23 | 2008-08-28 | Honeywell International, Inc. | Flight control computers with ethernet based cross channel data links |
| US8504178B2 (en) * | 2009-02-27 | 2013-08-06 | Mitsubishi Heavy Industries, Ltd. | Multiple redundant control system |
| US20120297108A1 (en) * | 2009-12-16 | 2012-11-22 | Kawasaki Jukogyo Kabushiki Kaisha | Integrated electronic system mounted on aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| US20170277152A1 (en) | 2017-09-28 |
| CN107005446A (zh) | 2017-08-01 |
| US10338560B2 (en) | 2019-07-02 |
| WO2016034824A1 (fr) | 2016-03-10 |
| EP3189380B1 (fr) | 2018-08-22 |
| JP2020030815A (ja) | 2020-02-27 |
| KR102213762B1 (ko) | 2021-02-09 |
| CA2960093A1 (fr) | 2016-03-10 |
| RU2670941C2 (ru) | 2018-10-25 |
| JP2017530461A (ja) | 2017-10-12 |
| EP3189380A1 (fr) | 2017-07-12 |
| CN107005446B (zh) | 2018-11-27 |
| KR20170089835A (ko) | 2017-08-04 |
| KR20180087468A (ko) | 2018-08-01 |
| FR3025626A1 (fr) | 2016-03-11 |
| FR3025626B1 (fr) | 2017-11-03 |
| RU2017111197A (ru) | 2018-10-05 |
| CA2960093C (fr) | 2020-03-10 |
| RU2017111197A3 (enExample) | 2018-10-05 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| RU2670941C9 (ru) | Двухканальная архитектура с избыточными линиями связи ccdl | |
| RU2679706C2 (ru) | Двухканальная архитектура | |
| Alena et al. | Communications for integrated modular avionics | |
| 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 | |
| US9876598B2 (en) | Switch for transmission of data between heterogeneous networks for aircraft | |
| JP3827772B2 (ja) | 分散型制御システムのための投票ノード | |
| US9582376B2 (en) | Unified communications module (UCM) | |
| US8194533B2 (en) | Fault tolerant data bus node and system | |
| CN110361979A (zh) | 一种铁路信号领域的安全计算机平台 | |
| EP3699764B1 (en) | Redundant ethernet-based secure computer system | |
| EP0883838B1 (en) | Shared bw architecture for applications with varying levels of integrity requirements | |
| US10911298B2 (en) | Communication network, communication installation within an aircraft and aircraft comprising such a communication installation | |
| Bai | Analysis of a SAE AS5643 Mil-1394b based high-speed avionics network architecture for space and defense applications | |
| US9686363B2 (en) | Aircraft communication system, aircraft communication method, and communication device | |
| Hiergeist et al. | Internal redundancy in future UAV FCCs and the challenge of synchronization | |
| McCabe et al. | Avionics architecture interface considerations between constellation vehicles | |
| Hiergeist et al. | Fault-tolerant FCC Architecture for future UAV systems based on COTS SoC | |
| CN111177793B (zh) | 数字量采集及通信传输系统 | |
| An et al. | Architecture Design of Aviation Fault-tolerant Computer Based on ARINC659 Bus Technology | |
| Fidi | Deterministic Ethernet for Scalable, Modular Launcher Avionics |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| TH4A | Reissue of patent specification |