DE60316016D1 - Hochintegre systemarchitektur mit einer schnellen wiederherstellung der digitale computerplatform - Google Patents

Hochintegre systemarchitektur mit einer schnellen wiederherstellung der digitale computerplatform

Info

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
Application number
DE60316016T
Other languages
English (en)
Other versions
DE60316016T2 (de
Inventor
Richard Hess
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.)
Honeywell International Inc
Original Assignee
Honeywell International Inc
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 Honeywell International Inc filed Critical Honeywell International Inc
Publication of DE60316016D1 publication Critical patent/DE60316016D1/de
Application granted granted Critical
Publication of DE60316016T2 publication Critical patent/DE60316016T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/0055—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
    • G05D1/0077—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements using redundant signals or controls
DE60316016T 2002-11-20 2003-11-19 Hochintegre systemarchitektur mit einer schnellen wiederherstellung der digitale computerplatform Expired - Fee Related DE60316016T2 (de)

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)

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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
CN116069066A (zh) * 2016-12-22 2023-05-05 小鹰公司 分布式飞行控制系统
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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
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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

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Also Published As

Publication number Publication date
US6813527B2 (en) 2004-11-02
US20040098140A1 (en) 2004-05-20
AU2003291091A1 (en) 2004-06-15
EP1563352A1 (de) 2005-08-17
EP1563352B1 (de) 2007-08-29
DE60316016T2 (de) 2008-06-05
WO2004046838A1 (en) 2004-06-03

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Legal Events

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8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee