ES2189144T3 - Arquitctura modular de bajo coste para pilotar el funcionamiento de un aerodino con un nivel alto de seguridad. - Google Patents

Arquitctura modular de bajo coste para pilotar el funcionamiento de un aerodino con un nivel alto de seguridad.

Info

Publication number
ES2189144T3
ES2189144T3 ES98910798T ES98910798T ES2189144T3 ES 2189144 T3 ES2189144 T3 ES 2189144T3 ES 98910798 T ES98910798 T ES 98910798T ES 98910798 T ES98910798 T ES 98910798T ES 2189144 T3 ES2189144 T3 ES 2189144T3
Authority
ES
Spain
Prior art keywords
modules
data
modular architecture
aerodine
pilot
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 - Lifetime
Application number
ES98910798T
Other languages
English (en)
Inventor
Dominique Loise
Jean-Pierre Ledoux
Patrick Sardier
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.)
Thales Avionics SAS
Original Assignee
Thales Avionics SAS
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 Thales Avionics SAS filed Critical Thales Avionics SAS
Application granted granted Critical
Publication of ES2189144T3 publication Critical patent/ES2189144T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00Error detection; Error correction; Monitoring
    • G06F11/07Responding to the occurrence of a fault, e.g. fault tolerance
    • G06F11/16Error detection or correction of the data by redundancy in hardware
    • G06F11/20Error 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
    • G06F11/202Error 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 processing functionality is redundant
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00Error detection; Error correction; Monitoring
    • G06F11/008Reliability or availability analysis
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00Error detection; Error correction; Monitoring
    • G06F11/07Responding to the occurrence of a fault, e.g. fault tolerance
    • G06F11/16Error detection or correction of the data by redundancy in hardware
    • G06F11/20Error 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Quality & Reliability (AREA)
  • Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Control By Computers (AREA)
  • Arrangements For Transmission Of Measured Signals (AREA)
  • Power Sources (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Storage Device Security (AREA)
  • Safety Devices In Control Systems (AREA)

Abstract

LA ARQUITECTURA MODULAR DE EQUIPOS ELECTRONICOS SEGUN LA INVENCION COMPRENDE MODULOS DE CONCENTRACION DE DATOS, MODULOS DE TRATAMIENTO Y DISPOSITIVOS DE VISUALIZACION (3 A 7), INTERCONECTADOS POR MEDIOS DE TRANSMISION DE DATOS CON DETECTORES (13), INSTRUMENTOS DE MEDICION (8, 9, 13) Y ACCIONADORES (12), NO CONCENTRANDO LOS MODULOS DE CONCENTRACION DE DATOS MAS QUE LOS DATOS NO CRITICOS PARA EL PROCESO INDUSTRIAL, SIENDO ESTOS DATOS TRANSMITIDOS A OTROS MODULOS MEDIANTE UN BUS DIGITAL EN SERIE MUTIRRECEPTORES, COMPRENDIENDO LOS OTROS MODULOS MEDIOS PARA RECIBIR DIRECTAMENTE LOS DATOS CRITICOS QUE SON ENCAMINADOS MEDIANTE ENLACES DIGITALES EN SERIE SEPARADOS, RESPECTIVOS (14, 15) ENTRE POR UNA PARTE, LOS DISPOSITIVO DE VISUALIZACION Y LAS FUNCIONES QUE EFECTUAN EL PILOTAJE DEL PROCESO QUE ESTAN REPARTIDAS EN LOS MODULOS DE TRATAMIENTO Y POR OTRA PARTE, LOS DETECTORES (13), LOS INSTRUMENTOS DE MEDICION (8, 9, 13) Y LOS ACCIONADORES (12).
ES98910798T 1997-02-25 1998-02-20 Arquitctura modular de bajo coste para pilotar el funcionamiento de un aerodino con un nivel alto de seguridad. Expired - Lifetime ES2189144T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9702210A FR2760103B1 (fr) 1997-02-25 1997-02-25 Architecture modulaire de pilotage d'un aerodyne presentant un faible cout tout en etant apte a assurer un niveau eleve de securite de fonctionnement

Publications (1)

Publication Number Publication Date
ES2189144T3 true ES2189144T3 (es) 2003-07-01

Family

ID=9504131

Family Applications (1)

Application Number Title Priority Date Filing Date
ES98910798T Expired - Lifetime ES2189144T3 (es) 1997-02-25 1998-02-20 Arquitctura modular de bajo coste para pilotar el funcionamiento de un aerodino con un nivel alto de seguridad.

Country Status (10)

Country Link
US (1) US6600963B1 (es)
EP (1) EP0965072B1 (es)
JP (1) JP2001513238A (es)
CN (1) CN1160603C (es)
CA (1) CA2282089C (es)
DE (1) DE69811344T2 (es)
ES (1) ES2189144T3 (es)
FR (1) FR2760103B1 (es)
RU (1) RU99120177A (es)
WO (1) WO1998038553A1 (es)

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US7020878B1 (en) 1998-08-28 2006-03-28 Oracle International Corporation System for allocating resource using the weight that represents a limitation on number of allowance active sessions associated with each resource consumer group
US7526767B1 (en) 1998-08-28 2009-04-28 Oracle International Corporation Methods for automatic group switching according to a resource plan
US7451448B1 (en) 1998-08-28 2008-11-11 Oracle International Corporation Methods for selectively quiescing a computer system
DE502004003469D1 (de) * 2004-05-10 2007-05-24 Siemens Ag Sicherheitsgerichtete Übertragung von Daten
US7971095B2 (en) * 2005-02-16 2011-06-28 Honeywell International Inc. Fault recovery for real-time, multi-tasking computer system
DE102005009795A1 (de) * 2005-03-03 2006-09-14 Wago Verwaltungsgesellschaft Mbh Mikroprozessorsystem für eine Maschinensteuerung in sicherheitszertifizierbaren Anwendungen
US7765427B2 (en) * 2005-08-05 2010-07-27 Honeywell International Inc. Monitoring system and methods for a distributed and recoverable digital control system
WO2007018652A1 (en) * 2005-08-05 2007-02-15 Honeywell International, Inc. Distributed and recoverable digital control system
WO2007018651A1 (en) * 2005-08-05 2007-02-15 Honeywell International, Inc. Method for redunancy management of distributed and recoverable digital control system
DE102005055000A1 (de) 2005-11-18 2007-05-24 Airbus Deutschland Gmbh Modulares Avioniksystem eines Flugzeuges
US7793147B2 (en) * 2006-07-18 2010-09-07 Honeywell International Inc. Methods and systems for providing reconfigurable and recoverable computing resources
DE102007025447A1 (de) * 2006-10-09 2008-04-17 Siemens Ag Verfahren zur Steuerung und/oder Regelung eines industriellen Prozesses
CN101913427B (zh) * 2010-08-04 2013-01-09 北京航空航天大学 一种适用于多用途无人飞行器的航空电子系统
EP2704682A4 (en) * 2011-05-05 2014-10-22 Aegis Analytical Corp SYSTEM FOR DESIGNATING, DISPLAYING AND SELECTING TYPES OF PROCESS PARAMETERS AND PRODUCT RESET PARAMETERS
US9270113B2 (en) * 2012-08-27 2016-02-23 Hamilton Sundstrand Corporation Power distribution cabinet
US9286738B2 (en) 2014-05-23 2016-03-15 Immortal Data, Inc. Distributed data storage and recovery
JP6316522B1 (ja) * 2017-01-25 2018-04-25 三菱電機株式会社 計算機装置、タスク起動方法およびタスク起動プログラム
CN109937439A (zh) * 2017-09-29 2019-06-25 深圳市大疆创新科技有限公司 一种保护飞控系统的方法及电路
US11970286B2 (en) 2021-06-04 2024-04-30 Ge Aviation Systems Llc Flight recorder system and method
CN113636090B (zh) * 2021-08-24 2022-08-09 中国商用飞机有限责任公司 监控飞行器的实时时钟的方法、系统和介质
CN116661331B (zh) * 2023-08-02 2023-09-26 成都正扬博创电子技术有限公司 一种利用软硬件协同的多余度飞控计算机系统

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4155116A (en) * 1978-01-04 1979-05-15 The Bendix Corporation Digital control system including built in test equipment
US4400694A (en) * 1979-12-03 1983-08-23 Wong Raphael W H Microprocessor base for monitor/control of communications facilities
US4421716A (en) * 1980-12-29 1983-12-20 S. Levy, Inc. Safety monitoring and reactor transient interpreter
FR2610120B1 (fr) * 1987-01-26 1989-07-13 Merlin Gerin Ensemble de commande et de protection connectant un reseau de communication local a un processus industriel
DE3732334A1 (de) * 1987-09-25 1989-04-27 Kloeckner Moeller Elektrizit Einrichtung und schaltungsanordnung zum schutz gegen ueberstrom und ueberspannung
US5267277A (en) * 1989-11-02 1993-11-30 Combustion Engineering, Inc. Indicator system for advanced nuclear plant control complex
US5237518A (en) * 1990-10-27 1993-08-17 Vanderbilt University Optimization method for adaptive sensor reading scheduling and delayed alarm evaluation in real-time diagnostic systems
JPH0576136A (ja) * 1991-09-13 1993-03-26 Hitachi Ltd 電力供給系統
US5640061A (en) * 1993-11-05 1997-06-17 Vari-Lite, Inc. Modular lamp power supply system

Also Published As

Publication number Publication date
EP0965072B1 (fr) 2003-02-12
CA2282089C (fr) 2009-04-21
EP0965072A1 (fr) 1999-12-22
JP2001513238A (ja) 2001-08-28
DE69811344D1 (de) 2003-03-20
CN1250530A (zh) 2000-04-12
US6600963B1 (en) 2003-07-29
RU99120177A (ru) 2001-08-27
FR2760103B1 (fr) 2000-02-04
WO1998038553A1 (fr) 1998-09-03
DE69811344T2 (de) 2003-10-30
CA2282089A1 (fr) 1998-09-03
FR2760103A1 (fr) 1998-08-28
CN1160603C (zh) 2004-08-04

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