FR2908384B1 - ALARM MONITORING AND ALARM SYSTEM - Google Patents

ALARM MONITORING AND ALARM SYSTEM

Info

Publication number
FR2908384B1
FR2908384B1 FR0654799A FR0654799A FR2908384B1 FR 2908384 B1 FR2908384 B1 FR 2908384B1 FR 0654799 A FR0654799 A FR 0654799A FR 0654799 A FR0654799 A FR 0654799A FR 2908384 B1 FR2908384 B1 FR 2908384B1
Authority
FR
France
Prior art keywords
alarm
function
aircraft
values
loss
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
FR0654799A
Other languages
French (fr)
Other versions
FR2908384A1 (en
Inventor
Christine Bezard
Laurent Spaggiari
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations 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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR0654799A priority Critical patent/FR2908384B1/en
Publication of FR2908384A1 publication Critical patent/FR2908384A1/en
Application granted granted Critical
Publication of FR2908384B1 publication Critical patent/FR2908384B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • G05B23/00—Testing or monitoring of control systems or parts thereof
    • G05B23/02—Electric testing or monitoring
    • G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
    • G05B23/0259—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterized by the response to fault detection
    • G05B23/0267—Fault communication, e.g. human machine interface [HMI]
    • G05B23/0272—Presentation of monitored results, e.g. selection of status reports to be displayed; Filtering information to the user
    • 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
    • G05B23/00—Testing or monitoring of control systems or parts thereof
    • G05B23/02—Electric testing or monitoring
    • G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
    • G05B23/0259—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterized by the response to fault detection
    • G05B23/0275—Fault isolation and identification, e.g. classify fault; estimate cause or root of failure
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Human Computer Interaction (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Testing Or Calibration Of Command Recording Devices (AREA)
  • Testing And Monitoring For Control Systems (AREA)

Abstract

The system has a diagnostic unit (210) receiving signals e.g. speed measurement signal, from sensors (C1-Ck) and determining values of state variables from the signals. The variables describe configurations of failure of elements of an aircraft and systems composed of the elements. A calculation unit (220) calculates a cost function from the values and cost values stored in a database (240). The function describes a loss of operational capacity of the aircraft for an operational function. An input/output interface (230) presents characteristic information of the loss of the capacity.
FR0654799A 2006-11-09 2006-11-09 ALARM MONITORING AND ALARM SYSTEM Expired - Fee Related FR2908384B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0654799A FR2908384B1 (en) 2006-11-09 2006-11-09 ALARM MONITORING AND ALARM SYSTEM

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0654799A FR2908384B1 (en) 2006-11-09 2006-11-09 ALARM MONITORING AND ALARM SYSTEM

Publications (2)

Publication Number Publication Date
FR2908384A1 FR2908384A1 (en) 2008-05-16
FR2908384B1 true FR2908384B1 (en) 2009-03-20

Family

ID=38093036

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0654799A Expired - Fee Related FR2908384B1 (en) 2006-11-09 2006-11-09 ALARM MONITORING AND ALARM SYSTEM

Country Status (1)

Country Link
FR (1) FR2908384B1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2976374B1 (en) * 2011-06-10 2016-10-14 Thales Sa OPTIMIZED TASK TREATMENT METHOD AND DEVICE FOR FWS.
US20150321748A1 (en) * 2014-05-08 2015-11-12 Honeywell International Inc. Speed brake alerting system and method
FR3083881B1 (en) * 2018-07-11 2020-12-25 Dassault Aviat SYSTEM FOR MONITORING AN OPERATING STATE OF AN AIRCRAFT E AND ASSOCIATED PROCESS

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5359326A (en) * 1993-03-16 1994-10-25 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Aircraft maneuver envelope warning system
US6043757A (en) * 1998-06-12 2000-03-28 The Boeing Company Dynamic, multi-attribute hazard prioritization system for aircraft
US6757668B1 (en) * 1999-11-05 2004-06-29 General Electric Company Information fusion of classifiers in systems with partial redundant information
DE10046007C1 (en) * 2000-09-18 2001-10-31 Eads Deutschland Gmbh Flight control system installed in aircraft cockpit continuously monitors flight parameters with evaluation via fuzzy logic for controlling pilot information display

Also Published As

Publication number Publication date
FR2908384A1 (en) 2008-05-16

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Legal Events

Date Code Title Description
CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

ST Notification of lapse

Effective date: 20200911