ES2081883T3 - Procedimiento y dispositivo para reconocimiento e identificacion de errores en sensores. - Google Patents

Procedimiento y dispositivo para reconocimiento e identificacion de errores en sensores.

Info

Publication number
ES2081883T3
ES2081883T3 ES90116029T ES90116029T ES2081883T3 ES 2081883 T3 ES2081883 T3 ES 2081883T3 ES 90116029 T ES90116029 T ES 90116029T ES 90116029 T ES90116029 T ES 90116029T ES 2081883 T3 ES2081883 T3 ES 2081883T3
Authority
ES
Spain
Prior art keywords
vector
measurement
parity
sensors
determination
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
ES90116029T
Other languages
English (en)
Inventor
Uwe Krogmann
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.)
Bodenseewerk Geratetechnik GmbH
Original Assignee
Bodenseewerk Geratetechnik GmbH
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 Bodenseewerk Geratetechnik GmbH filed Critical Bodenseewerk Geratetechnik GmbH
Application granted granted Critical
Publication of ES2081883T3 publication Critical patent/ES2081883T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • G06F11/187—Voting techniques
    • G06F11/188—Voting techniques where exact match is not required
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C25/00—Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass
    • 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
    • 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
    • G06F11/08—Error detection or correction by redundancy in data representation, e.g. by using checking codes
    • G06F11/10—Adding special bits or symbols to the coded information, e.g. parity check, casting out 9's or 11's
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Quality & Reliability (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Automation & Control Theory (AREA)
  • Remote Sensing (AREA)
  • Manufacturing & Machinery (AREA)
  • Gyroscopes (AREA)
  • Navigation (AREA)
  • Testing Or Calibration Of Command Recording Devices (AREA)
  • Investigating Or Analysing Materials By The Use Of Chemical Reactions (AREA)
  • Investigating Or Analyzing Materials By The Use Of Magnetic Means (AREA)
  • Testing Electric Properties And Detecting Electric Faults (AREA)
  • Testing And Monitoring For Control Systems (AREA)
  • Inspection Of Paper Currency And Valuable Securities (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

UN PROCEDIMIENTO PARA RECONOCER E IDENTIFICAR FALLOS EN SENSORES PARA MEDIDAS DE ESTADO, QUE SON LIGADOS CON MEDIDAS DADAS DIRECTAMENTE POR LOS SENSORES, MEDIANTE UNA ECUACION DE MEDICION M = HX + W, SIENDO M UN VECTOR DE LAS MEDIDAS DE MEDICION, X UN VECTOR DE LAS MEDIDAS DE ESTADO Y H LA MATRIZ DE MEDICION, Y DONDE EL ORDEN DE M ES MAYOR QUE EL ORDEN DE X, TIENE LOS PASOS DE PROCESAMIENTO: (A) DEFINICION DE VECTORES DE VALIDACION VI COMO VECTORES DE COLUMNAS DE UNA MATRIZ P = [V1 V2...VN] (B) DETERMINACION DE UN VECTOR DE PARIDAD V COMO ELEMENTO DE UN ESPACIO DE PARIDAD, QUE ES EL COMPLEMENTO ORTOGONAL DEL ESPACIO DE SEÑAL, COMO COMBINACION LINEAL DE LOS VECTORES DE VALIDACION CON LOS CORRESPONDIENTES ELEMENTOS MI DEL VECTOR DE MEDICION M: V = .... (C) FORMACION DE UNA FUNCION DE DETECCION DF = < V V > COMO PRODUCTO DE ESCALA DEL VECTOR DE PARIDAD CONSIGO MISMO, Y COMPROBACION, SI ESTA FUNCION DE DETECCION ES MAYOR O MENOR QUE UN VALOR LIMITE PREVIAMENTE DADO. SOBREPASAR ESTE VALOR LIMITESEÑALIZA LA EXISTENCIA DE UN FALLO. (D) AL EXISTIR UN FALLO, SE PUEDEN HACER CALCULOS DE FUNCIONES DE LOCALIZACION DE LOS COMPONENTES DEL VECTOR DE PARIDAD Y HACER LA DETERMINACION DE LA FUNCION DE LOCALIZACION MAXIMA DE LA CUAL SE PUEDE DEDUCIR EL SENSOR QUE FALLA. (E) RECONFIGURACION DE LAS SEÑALES DE SENSOR, TENDIENDO EN CUENTA DE ESTADO DE FALLO CALCULADO DE ESTA MANERA
ES90116029T 1989-09-05 1990-08-22 Procedimiento y dispositivo para reconocimiento e identificacion de errores en sensores. Expired - Lifetime ES2081883T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3929404A DE3929404A1 (de) 1989-09-05 1989-09-05 Verfahren und vorrichtung zum erkennen und identifizieren von fehlern an sensoren

Publications (1)

Publication Number Publication Date
ES2081883T3 true ES2081883T3 (es) 1996-03-16

Family

ID=6388638

Family Applications (1)

Application Number Title Priority Date Filing Date
ES90116029T Expired - Lifetime ES2081883T3 (es) 1989-09-05 1990-08-22 Procedimiento y dispositivo para reconocimiento e identificacion de errores en sensores.

Country Status (4)

Country Link
EP (1) EP0416370B1 (es)
AT (1) ATE130687T1 (es)
DE (2) DE3929404A1 (es)
ES (1) ES2081883T3 (es)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4241822C2 (de) * 1992-12-11 1996-09-19 Bosch Gmbh Robert Schaltungsanordnung zur Fehlererkennung bei der Auswertung von Sensorsignalen
DE4244014A1 (de) * 1992-12-24 1994-07-07 Bodenseewerk Geraetetech Verfahren zum Erkennen und Identifizieren von Fehlern an Sensoren
JP3221184B2 (ja) * 1993-10-13 2001-10-22 株式会社日立製作所 故障診断装置および方法
DE4410709A1 (de) * 1994-03-28 1995-10-05 Bodenseewerk Geraetetech Überwachungs-Einrichtung zur Überwachung der Flugsicherheit von Flugzeugen
EP0720004B1 (de) * 1994-12-27 2000-02-16 LITEF GmbH FDIC-Verfahren zur Minimierung von Messfehlern in einer Messanordnung von redundanten Sensoren
DE59603161D1 (de) * 1995-03-10 1999-10-28 Siemens Ag Verfahren zur bestimmung einer zuverlässigkeits-kenngrösse eines responsiven systems sowie ein entsprechendes system zur signalverarbeitung
US6085127A (en) 1997-03-18 2000-07-04 Aurora Flight Sciences Corporation Fault tolerant automatic control system utilizing analytic redundancy
US6539290B1 (en) 1995-06-07 2003-03-25 Dabulamanzi Holdings, Llc Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI'zation
US5615119A (en) * 1995-06-07 1997-03-25 Aurora Flight Sciences Corporation Fault tolerant automatic control system utilizing analytic redundancy
US6594620B1 (en) 1998-08-17 2003-07-15 Aspen Technology, Inc. Sensor validation apparatus and method
EP1112532B1 (en) 1998-08-17 2003-04-02 Aspen Technology, Inc. Sensor validation apparatus and method
DE19857894A1 (de) 1998-12-15 2000-06-21 Bodenseewerk Geraetetech Flugkörper
DE102004037352B4 (de) * 2004-07-30 2008-06-26 Eads Deutschland Gmbh Verfahren zur Überwachung einer zulässigen Konfidenz einer Messgröße eines dynamischen Systems
US7805245B2 (en) * 2007-04-18 2010-09-28 Honeywell International Inc. Inertial measurement unit fault detection isolation reconfiguration using parity logic
EP3531243B1 (en) * 2018-02-23 2021-12-29 Rohde & Schwarz GmbH & Co. KG Measurement instrument identification system as well as method for finding a particular measurement instrument
US20230249845A1 (en) * 2022-02-07 2023-08-10 Hamilton Sundstrand Corporation Artificial intelligence and/or machine learning (ai/ml) monitor systems

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3984672A (en) * 1974-12-05 1976-10-05 Control Systems Research, Inc. Solid state translator
US4268354A (en) * 1978-10-12 1981-05-19 Westinghouse Electric Corp. Nuclear reactor in core flux mapping system
US4580234A (en) * 1982-08-02 1986-04-01 Nippon Business Consultant Co., Ltd. Measurement system of enhanced reliability
US4622667A (en) * 1984-11-27 1986-11-11 Sperry Corporation Digital fail operational automatic flight control system utilizing redundant dissimilar data processing
US4787058A (en) * 1985-09-13 1988-11-22 Rockwell International Corporation Synthetic quadrature generating apparatus
US4665748A (en) * 1985-10-21 1987-05-19 Sundstrand Data Control, Inc. Automatic continuous nulling of angular rate sensor
DE3634023A1 (de) * 1986-10-07 1988-04-21 Bodenseewerk Geraetetech Integriertes, redundantes referenzsystem fuer die flugregelung und zur erzeugung von kurs- und lageinformationen

Also Published As

Publication number Publication date
DE3929404A1 (de) 1991-03-07
EP0416370B1 (de) 1995-11-22
DE59009896D1 (de) 1996-01-04
EP0416370A3 (en) 1992-05-20
EP0416370A2 (de) 1991-03-13
ATE130687T1 (de) 1995-12-15

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