ATE431944T1 - Fehlertolerantes computergesteuertes system - Google Patents

Fehlertolerantes computergesteuertes system

Info

Publication number
ATE431944T1
ATE431944T1 AT03001308T AT03001308T ATE431944T1 AT E431944 T1 ATE431944 T1 AT E431944T1 AT 03001308 T AT03001308 T AT 03001308T AT 03001308 T AT03001308 T AT 03001308T AT E431944 T1 ATE431944 T1 AT E431944T1
Authority
AT
Austria
Prior art keywords
controlled system
tolerant computer
fault
data item
actuator
Prior art date
Application number
AT03001308T
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
Application granted granted Critical
Publication of ATE431944T1 publication Critical patent/ATE431944T1/de

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)
  • Automation & Control Theory (AREA)
  • Quality & Reliability (AREA)
  • General Engineering & Computer Science (AREA)
  • Hardware Redundancy (AREA)
  • Multi Processors (AREA)
  • Safety Devices In Control Systems (AREA)
AT03001308T 2003-01-23 2003-01-23 Fehlertolerantes computergesteuertes system ATE431944T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP03001308A EP1443399B1 (de) 2003-01-23 2003-01-23 Fehlertolerantes computergesteuertes System

Publications (1)

Publication Number Publication Date
ATE431944T1 true ATE431944T1 (de) 2009-06-15

Family

ID=32605236

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03001308T ATE431944T1 (de) 2003-01-23 2003-01-23 Fehlertolerantes computergesteuertes system

Country Status (10)

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

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US20180044034A1 (en) * 2015-03-27 2018-02-15 Astronautics Corporation Of America Auxiliary Security System for Aircraft Black Box System
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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
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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
JP2021525673A (ja) 2018-05-31 2021-09-27 ジョビー エアロ, インコーポレイテッドJoby Aero, Inc. 電力システムアーキテクチャとこれを用いたフォールトトレラントｖｔｏｌ航空機
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US11230384B2 (en) 2019-04-23 2022-01-25 Joby Aero, Inc. Vehicle cabin thermal management system and method
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US10988248B2 (en) 2019-04-25 2021-04-27 Joby Aero, Inc. VTOL aircraft
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Also Published As

Publication number Publication date
EP1443399B1 (de) 2009-05-20
CA2455478A1 (en) 2004-07-23
CN100363899C (zh) 2008-01-23
US7263630B2 (en) 2007-08-28
RU2004102029A (ru) 2005-07-10
AU2004200226B2 (en) 2008-10-30
JP4309296B2 (ja) 2009-08-05
HK1069890A1 (en) 2005-06-03
US20040195460A1 (en) 2004-10-07
JP2004342077A (ja) 2004-12-02
DE60327687D1 (de) 2009-07-02
RU2333528C2 (ru) 2008-09-10
EP1443399A1 (de) 2004-08-04
AU2004200226A1 (en) 2004-08-12
CN1550988A (zh) 2004-12-01

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