DE60316016D1 - Hochintegre systemarchitektur mit einer schnellen wiederherstellung der digitale computerplatform - Google Patents
Hochintegre systemarchitektur mit einer schnellen wiederherstellung der digitale computerplatformInfo
- Publication number
- DE60316016D1 DE60316016D1 DE60316016T DE60316016T DE60316016D1 DE 60316016 D1 DE60316016 D1 DE 60316016D1 DE 60316016 T DE60316016 T DE 60316016T DE 60316016 T DE60316016 T DE 60316016T DE 60316016 D1 DE60316016 D1 DE 60316016D1
- Authority
- DE
- Germany
- Prior art keywords
- integre
- system architecture
- digital computer
- computer platform
- fast recovery
- 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
Links
- 238000011084 recovery Methods 0.000 title 1
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
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Safety Devices In Control Systems (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/300,185 US6813527B2 (en) | 2002-11-20 | 2002-11-20 | High integrity control system architecture using digital computing platforms with rapid recovery |
US300185 | 2002-11-20 | ||
PCT/US2003/036949 WO2004046838A1 (en) | 2002-11-20 | 2003-11-19 | High integrity control system architecture using digital computing platforms with rapid recovery |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60316016D1 true DE60316016D1 (de) | 2007-10-11 |
DE60316016T2 DE60316016T2 (de) | 2008-06-05 |
Family
ID=32297861
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60316016T Expired - Fee Related DE60316016T2 (de) | 2002-11-20 | 2003-11-19 | Hochintegre systemarchitektur mit einer schnellen wiederherstellung der digitale computerplatform |
Country Status (5)
Country | Link |
---|---|
US (1) | US6813527B2 (de) |
EP (1) | EP1563352B1 (de) |
AU (1) | AU2003291091A1 (de) |
DE (1) | DE60316016T2 (de) |
WO (1) | WO2004046838A1 (de) |
Families Citing this family (43)
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US8015973B2 (en) | 2003-02-15 | 2011-09-13 | Gulfstream Aerospace Corporation | System and method for aircraft cabin atmospheric composition control |
US7209809B2 (en) * | 2003-10-15 | 2007-04-24 | The Boeing Company | Method and apparatus for obtaining high integrity and availability in multi-channel systems |
US8789051B2 (en) | 2004-11-18 | 2014-07-22 | Hamilton Sundstrand Corporation | Operating system and architecture for embedded system |
US7971095B2 (en) * | 2005-02-16 | 2011-06-28 | Honeywell International Inc. | Fault recovery for real-time, multi-tasking computer system |
US20100318245A1 (en) * | 2005-03-03 | 2010-12-16 | Nabtesco Corporation | Flight control system |
US7789345B2 (en) * | 2005-03-03 | 2010-09-07 | Nabtesco Corporation | Actuator control apparatus |
US7698511B2 (en) * | 2005-05-19 | 2010-04-13 | Honeywell International Inc. | Interface for writing to memories having different write times |
LU91175B1 (fr) * | 2005-06-13 | 2006-12-14 | Airflowcontrol S A | Procédé et système d'économie d'énergie dans un bâtiment avec ascenseur |
US7953536B2 (en) * | 2005-07-29 | 2011-05-31 | GM Global Technology Operations LLC | Inertial sensor software architecture security method |
US7725215B2 (en) * | 2005-08-05 | 2010-05-25 | Honeywell International Inc. | Distributed and recoverable digital control system |
WO2007094808A1 (en) * | 2005-08-05 | 2007-08-23 | Honeywell International Inc. | Monitoring system and methods for a distributed and recoverable digital control system |
US8260492B2 (en) * | 2005-08-05 | 2012-09-04 | Honeywell International Inc. | Method and system for redundancy management of distributed and recoverable digital control system |
US7421320B2 (en) * | 2005-10-06 | 2008-09-02 | The Boeing Company | Methods and apparatus for implementing mid-value selection functions for dual dissimlar processing modules |
US8359112B2 (en) * | 2006-01-13 | 2013-01-22 | Emerson Process Management Power & Water Solutions, Inc. | Method for redundant controller synchronization for bump-less failover during normal and program mismatch conditions |
US7878461B2 (en) * | 2006-01-17 | 2011-02-01 | Gulfstream Aerospace Corporation | System and method for an integrated backup control system |
JP2009523658A (ja) | 2006-01-17 | 2009-06-25 | ガルフストリーム・エアロスペース・コーポレイション | 分散型飛行制御システムのバックアップ制御のための装置及び方法 |
US8977252B1 (en) * | 2006-07-06 | 2015-03-10 | Gryphonet Ltd. | System and method for automatic detection and recovery of malfunction in mobile devices |
US7793147B2 (en) * | 2006-07-18 | 2010-09-07 | Honeywell International Inc. | Methods and systems for providing reconfigurable and recoverable computing resources |
US20080098234A1 (en) * | 2006-10-20 | 2008-04-24 | Honeywell International Inc. | Fault-containment and/or failure detection using encryption |
US20100257139A1 (en) * | 2007-03-29 | 2010-10-07 | Gm Global Technology Operations, Inc. | Vehicle Data Security Method and System |
US20080288120A1 (en) * | 2007-05-14 | 2008-11-20 | General Electric Company | Methods and Systems for Modifying Turbine Control Systems |
US8036805B2 (en) * | 2007-07-13 | 2011-10-11 | Honeywell International Inc. | Distributed engine control system |
US8948960B2 (en) * | 2007-11-30 | 2015-02-03 | Honeywell International Inc. | Systems and methods for arbitrating sensor and actuator signals in a multi-channel control system |
US8209526B2 (en) * | 2008-09-30 | 2012-06-26 | General Electric Company | Method and systems for restarting a flight control system |
US7877627B1 (en) | 2008-12-18 | 2011-01-25 | Supercon, L.L.C. | Multiple redundant computer system combining fault diagnostics and majority voting with dissimilar redundancy technology |
JP4840483B2 (ja) * | 2009-07-13 | 2011-12-21 | トヨタ自動車株式会社 | 制御目標演算装置 |
FR2978423B1 (fr) * | 2011-07-28 | 2014-12-19 | Airbus Operations Sas | Procede et dispositif de detection de l'embarquement d'une gouverne d'aeronef |
US20140163907A1 (en) * | 2012-12-10 | 2014-06-12 | General Electric Company | Systems and methods for fault detection |
US9740178B2 (en) * | 2013-03-14 | 2017-08-22 | GM Global Technology Operations LLC | Primary controller designation in fault tolerant systems |
US8862290B1 (en) * | 2013-04-18 | 2014-10-14 | Ge Aviation Systems Llc | Flight system for an aircraft having an autoland system |
EP2851291B1 (de) | 2013-09-23 | 2016-05-11 | Airbus Operations (S.A.S) | Steuersystem eines Luftfahrzeugs |
US9284043B2 (en) * | 2013-11-21 | 2016-03-15 | Aai Corporation | Evaluating aileron deflection while an unmanned aerial vehicle is in flight |
US9915925B2 (en) * | 2014-02-25 | 2018-03-13 | Honeywell International Inc. | Initiated test health management system and method |
JP6207483B2 (ja) * | 2014-09-03 | 2017-10-04 | 双葉電子工業株式会社 | 通信機器、被操縦装置 |
CN105204327B (zh) * | 2015-08-24 | 2017-08-29 | 北京航空航天大学 | 基于最小路不交化的飞机非相似作动系统可靠性确认方法 |
WO2018118070A1 (en) * | 2016-12-22 | 2018-06-28 | Kitty Hawk Corporation | Distributed flight control system |
US10850868B1 (en) * | 2018-05-29 | 2020-12-01 | Rockwell Collins, Inc. | Operational scenario specific adaptive sensor voter |
US11099238B2 (en) | 2019-03-27 | 2021-08-24 | General Electric Company | Distributed control modules with built-in tests and control-preserving fault responses |
US11661895B2 (en) | 2020-02-24 | 2023-05-30 | General Electric Comapny | Autonomous safety mode for distributed control of turbomachines |
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 |
US11435761B1 (en) | 2021-07-23 | 2022-09-06 | Beta Air, Llc | System and method for distributed flight control system for an electric vehicle |
US11465734B1 (en) | 2021-09-16 | 2022-10-11 | Beta Air, Llc | Systems and methods for distrubuted flight controllers for redundancy for an electric aircraft |
JP2024009696A (ja) * | 2022-07-11 | 2024-01-23 | 横河電機株式会社 | 制御装置、制御システム、制御方法、及び制御プログラム |
Family Cites Families (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3805235A (en) | 1972-12-26 | 1974-04-16 | Collins Radio Co | Equalization means for multi-channel redundant control system |
FR2344063A1 (fr) | 1976-03-10 | 1977-10-07 | Smiths Industries Ltd | Circuit numerique de commande a deux voies au moins |
US4751670A (en) | 1986-03-31 | 1988-06-14 | Honeywell Inc. | High integrity digital processor architecture |
DE3642851A1 (de) | 1986-12-16 | 1988-06-30 | Bbc Brown Boveri & Cie | Fehlertolerantes rechensystem und verfahren zum erkennen, lokalisieren und eliminieren von fehlerhaften einheiten in einem solchen system |
US4996687A (en) | 1988-10-11 | 1991-02-26 | Honeywell Inc. | Fault recovery mechanism, transparent to digital system function |
US5226152A (en) * | 1990-12-07 | 1993-07-06 | Motorola, Inc. | Functional lockstep arrangement for redundant processors |
US5313625A (en) | 1991-07-30 | 1994-05-17 | Honeywell Inc. | Fault recoverable computer system |
FR2692379B1 (fr) | 1991-10-04 | 1996-08-14 | Aerospatiale Ste Nat Indle | Procede de detection et de passivation de pannes dans un systeme de traitement de donnees, et systeme de traitement de donnees adapte a sa mise en oeuvre |
US5502728A (en) | 1992-02-14 | 1996-03-26 | International Business Machines Corporation | Large, fault-tolerant, non-volatile, multiported memory |
JPH07507891A (ja) * | 1992-06-12 | 1995-08-31 | ザ、ダウ、ケミカル、カンパニー | インテリジェントプロセス制御通信システムおよび方法 |
ES2162659T3 (es) * | 1992-06-12 | 2002-01-01 | Dow Chemical Co | Sistema de comunicacion cabeza-cola seguro y metodo para el procedimiento en ordenadores de control. |
US5583757A (en) * | 1992-08-04 | 1996-12-10 | The Dow Chemical Company | Method of input signal resolution for actively redundant process control computers |
US5307409A (en) | 1992-12-22 | 1994-04-26 | Honeywell Inc | Apparatus and method for fault detection on redundant signal lines via encryption |
US5386424A (en) | 1993-03-31 | 1995-01-31 | Honeywell, Inc. | Apparatus and method for transmitting information between dual redundant components utilizing four signal paths |
US5343474A (en) | 1993-03-31 | 1994-08-30 | Honeywell Inc. | Slotted arbitration without time jitter in a table driven protocol |
US5550736A (en) | 1993-04-27 | 1996-08-27 | Honeywell Inc. | Fail-operational fault tolerant flight critical computer architecture and monitoring method |
US5909541A (en) | 1993-07-14 | 1999-06-01 | Honeywell Inc. | Error detection and correction for data stored across multiple byte-wide memory devices |
US5572620A (en) * | 1993-07-29 | 1996-11-05 | Honeywell Inc. | Fault-tolerant voter system for output data from a plurality of non-synchronized redundant processors |
US5491625A (en) * | 1993-12-23 | 1996-02-13 | The Dow Chemical Company | Information display system for actively redundant computerized process control |
US5491787A (en) * | 1994-08-25 | 1996-02-13 | Unisys Corporation | Fault tolerant digital computer system having two processors which periodically alternate as master and slave |
US5881971A (en) | 1995-05-15 | 1999-03-16 | The Boeing Company | Monitoring systems for detecting failures in fly-by-wire aircraft flight control systems |
US6085127A (en) | 1997-03-18 | 2000-07-04 | Aurora Flight Sciences Corporation | Fault tolerant automatic control system utilizing analytic redundancy |
US5757641A (en) | 1995-07-03 | 1998-05-26 | General Electric Company | Triplex control system with sensor failure compensation |
FR2737029B1 (fr) * | 1995-07-19 | 1997-09-26 | Sextant Avionique | Dispositif d'interface entre un calculateur a architecture redondante et un moyen de communication |
DE19747125C2 (de) | 1997-10-24 | 1999-09-30 | Siemens Ag | Verfahren zur Einstellung von Reglerparametern eines Zustandsreglers |
US6163480A (en) | 1997-12-29 | 2000-12-19 | Honeywell International Inc. | Memory with high integrity memory cells |
US6272386B1 (en) | 1998-03-27 | 2001-08-07 | Honeywell International Inc | Systems and methods for minimizing peer-to-peer control disruption during fail-over in a system of redundant controllers |
US6178522B1 (en) | 1998-06-02 | 2001-01-23 | Alliedsignal Inc. | Method and apparatus for managing redundant computer-based systems for fault tolerant computing |
US6449732B1 (en) | 1998-12-18 | 2002-09-10 | Triconex Corporation | Method and apparatus for processing control using a multiple redundant processor control system |
US6532550B1 (en) * | 2000-02-10 | 2003-03-11 | Westinghouse Electric Company Llc | Process protection system |
US6954875B2 (en) | 2001-03-12 | 2005-10-11 | Honeywell International Inc. | Method of recovering a flight critical computer after a radiation event |
US6862693B2 (en) * | 2001-04-13 | 2005-03-01 | Sun Microsystems, Inc. | Providing fault-tolerance by comparing addresses and data from redundant processors running in lock-step |
-
2002
- 2002-11-20 US US10/300,185 patent/US6813527B2/en not_active Expired - Fee Related
-
2003
- 2003-11-19 AU AU2003291091A patent/AU2003291091A1/en not_active Abandoned
- 2003-11-19 DE DE60316016T patent/DE60316016T2/de not_active Expired - Fee Related
- 2003-11-19 EP EP03783680A patent/EP1563352B1/de not_active Expired - Fee Related
- 2003-11-19 WO PCT/US2003/036949 patent/WO2004046838A1/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
EP1563352A1 (de) | 2005-08-17 |
US20040098140A1 (en) | 2004-05-20 |
AU2003291091A1 (en) | 2004-06-15 |
US6813527B2 (en) | 2004-11-02 |
WO2004046838A1 (en) | 2004-06-03 |
DE60316016T2 (de) | 2008-06-05 |
EP1563352B1 (de) | 2007-08-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |