HK1069890A1 - Fault tolerant computer controlled system - Google Patents

Fault tolerant computer controlled system

Info

Publication number
HK1069890A1
HK1069890A1 HK05100868.4A HK05100868A HK1069890A1 HK 1069890 A1 HK1069890 A1 HK 1069890A1 HK 05100868 A HK05100868 A HK 05100868A HK 1069890 A1 HK1069890 A1 HK 1069890A1
Authority
HK
Hong Kong
Prior art keywords
controlled system
computer controlled
tolerant computer
fault tolerant
data item
Prior art date
Application number
HK05100868.4A
Other languages
English (en)
Inventor
Thomas Michael Sailer
Original Assignee
Supercomputing Systems Ag
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 Supercomputing Systems Ag filed Critical Supercomputing Systems Ag
Publication of HK1069890A1 publication Critical patent/HK1069890A1/xx

Links

Classifications

    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR 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
    • G06F11/18—Error detection or correction of the data by redundancy in hardware using passive fault-masking of the redundant circuits
    • G06F11/183—Error detection or correction of the data by redundancy in hardware using passive fault-masking of the redundant circuits by voting, the voting not being performed by the redundant components
    • G06F11/184—Error detection or correction of the data by redundancy in hardware using passive fault-masking of the redundant circuits by voting, the voting not being performed by the redundant components where the redundant components implement processing functionality
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Quality & Reliability (AREA)
  • General Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Hardware Redundancy (AREA)
  • Safety Devices In Control Systems (AREA)
  • Multi Processors (AREA)
HK05100868.4A 2003-01-23 2005-02-02 Fault tolerant computer controlled system HK1069890A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP03001308A EP1443399B1 (en) 2003-01-23 2003-01-23 Fault tolerant computer controlled system

Publications (1)

Publication Number Publication Date
HK1069890A1 true HK1069890A1 (en) 2005-06-03

Family

ID=32605236

Family Applications (1)

Application Number Title Priority Date Filing Date
HK05100868.4A HK1069890A1 (en) 2003-01-23 2005-02-02 Fault tolerant computer controlled system

Country Status (10)

Country Link
US (1) US7263630B2 (xx)
EP (1) EP1443399B1 (xx)
JP (1) JP4309296B2 (xx)
CN (1) CN100363899C (xx)
AT (1) ATE431944T1 (xx)
AU (1) AU2004200226B2 (xx)
CA (1) CA2455478A1 (xx)
DE (1) DE60327687D1 (xx)
HK (1) HK1069890A1 (xx)
RU (1) RU2333528C2 (xx)

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US10025344B2 (en) 2015-04-21 2018-07-17 The United States Of America As Represented By The Administrator Of Nasa Self-stabilizing distributed symmetric-fault tolerant synchronization protocol
US10328872B2 (en) * 2016-06-29 2019-06-25 Hamilton Sundstrand Corporation Methodology for simplification of aircraft harnessing in multi-redundant control systems
CN106354141B (zh) * 2016-11-02 2019-09-13 北京汽车集团有限公司 一种驾驶控制系统和方法
US10248430B2 (en) * 2016-12-16 2019-04-02 Hamilton Sundstrand Corporation Runtime reconfigurable dissimilar processing platform
JP2019070902A (ja) * 2017-10-06 2019-05-09 横河電機株式会社 制御システム、制御方法及び等値化装置
JP2019179964A (ja) * 2018-03-30 2019-10-17 株式会社Ｓｕｂａｒｕ 航空機
KR20240007689A (ko) 2018-05-31 2024-01-16 조비 에어로, 인크. 전력 시스템 아키텍처 및 이를 이용한 내고장성 vtol 항공기
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US11230384B2 (en) 2019-04-23 2022-01-25 Joby Aero, Inc. Vehicle cabin thermal management system and method
CN116646641A (zh) 2019-04-23 2023-08-25 杰欧比飞行有限公司 电池热管理系统及方法
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US11273906B2 (en) * 2019-05-10 2022-03-15 Honeywell International Inc. Redundant fly-by-wire systems with fault resiliency
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Also Published As

Publication number Publication date
AU2004200226A1 (en) 2004-08-12
CN1550988A (zh) 2004-12-01
RU2333528C2 (ru) 2008-09-10
ATE431944T1 (de) 2009-06-15
US20040195460A1 (en) 2004-10-07
DE60327687D1 (de) 2009-07-02
RU2004102029A (ru) 2005-07-10
EP1443399A1 (en) 2004-08-04
JP4309296B2 (ja) 2009-08-05
JP2004342077A (ja) 2004-12-02
AU2004200226B2 (en) 2008-10-30
EP1443399B1 (en) 2009-05-20
CA2455478A1 (en) 2004-07-23
US7263630B2 (en) 2007-08-28
CN100363899C (zh) 2008-01-23

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Legal Events

Date Code Title Description
PC Patent ceased (i.e. patent has lapsed due to the failure to pay the renewal fee)

Effective date: 20130123