PROCEDE DE SURVEILLANCE D'UNE DEGRADATION D'UN DISPOSITIF EMBARQUE D'UN AERONEF INCLUANT LA DETERMINATION D'UN SEUIL DE COMPTAGE
A method of monitoring a degradation of a device on board an aircraft, implemented by a computer, the degree of the degradation of the onboard device being defined by an abnormality score formed by the counting of occurrences of anomalies noted by a control system of the device, the method of monito...
Gespeichert in:
Hauptverfasser: | , , , , |
---|---|
Format: | Patent |
Sprache: | fre |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | |
---|---|
container_issue | |
container_start_page | |
container_title | |
container_volume | |
creator | ALIMARDANI ARMAND, DARIOUCHE MASSE JEAN-REMI, ANDRE LALONDE PIERRE, GERALD HUMEAU AURORE, FABIENNE, PAULE FOIRET GUILHEM, ALCIDE, AUGUSTE |
description | A method of monitoring a degradation of a device on board an aircraft, implemented by a computer, the degree of the degradation of the onboard device being defined by an abnormality score formed by the counting of occurrences of anomalies noted by a control system of the device, the method of monitoring comprising a step of comparing an abnormality score obtained for an observation sequence of given length (n, t) with a decision threshold (ks) and a step of emitting an alarm in case of attainment or overshoot of the decision threshold (ks), the decision threshold (ks) being determined automatically for a given alarm probability Pa, corresponding to the probability that an alarm is emitted in the course of the monitoring method although the onboard device is healthy, by means of the following steps: a step of obtaining an abnormality score (r) on at least one reference sequence corresponding to flights of the aircraft without degradation and of length (m, tc) equal to a plurality of lengths (n, t) of observation sequences; a step of fitting a discrete probability law making it possible to retrieve the abnormality score (r) obtained on the reference sequence; a step of calculating the decision threshold (ks) such that by applying the discrete probability law fitted during the previous step to an observation sequence having the given length (n), the probability that an anomaly score greater than or equal to the decision threshold (ks) will occur is less than the given alarm probability Pa or an elementary probability dependent on Pa in the case where a confirmation strategy is used. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_FR3022997B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>FR3022997B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_FR3022997B13</originalsourceid><addsrcrecordid>eNqNjb0KwkAQhNNYiPoO21kJmhSScnPZiwuXu3g_tiHIWYkG4gP46CZqYSkMDPMxw8yTZ2ONoJJglAv2RKwUajHmddATrSyW6NnoN4GSXWMce5ZAdYH2GD5VQLJGkwTWQgXUHhSOa0-2Zv2zdxRYTWfC1I3HipbJ7NJdh7j6-iIBSV4cNrG_t3Hou3O8xUcrbbZN0zzfF7vsj8oLnhE7Nw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>PROCEDE DE SURVEILLANCE D'UNE DEGRADATION D'UN DISPOSITIF EMBARQUE D'UN AERONEF INCLUANT LA DETERMINATION D'UN SEUIL DE COMPTAGE</title><source>esp@cenet</source><creator>ALIMARDANI ARMAND, DARIOUCHE ; MASSE JEAN-REMI, ANDRE ; LALONDE PIERRE, GERALD ; HUMEAU AURORE, FABIENNE, PAULE ; FOIRET GUILHEM, ALCIDE, AUGUSTE</creator><creatorcontrib>ALIMARDANI ARMAND, DARIOUCHE ; MASSE JEAN-REMI, ANDRE ; LALONDE PIERRE, GERALD ; HUMEAU AURORE, FABIENNE, PAULE ; FOIRET GUILHEM, ALCIDE, AUGUSTE</creatorcontrib><description>A method of monitoring a degradation of a device on board an aircraft, implemented by a computer, the degree of the degradation of the onboard device being defined by an abnormality score formed by the counting of occurrences of anomalies noted by a control system of the device, the method of monitoring comprising a step of comparing an abnormality score obtained for an observation sequence of given length (n, t) with a decision threshold (ks) and a step of emitting an alarm in case of attainment or overshoot of the decision threshold (ks), the decision threshold (ks) being determined automatically for a given alarm probability Pa, corresponding to the probability that an alarm is emitted in the course of the monitoring method although the onboard device is healthy, by means of the following steps: a step of obtaining an abnormality score (r) on at least one reference sequence corresponding to flights of the aircraft without degradation and of length (m, tc) equal to a plurality of lengths (n, t) of observation sequences; a step of fitting a discrete probability law making it possible to retrieve the abnormality score (r) obtained on the reference sequence; a step of calculating the decision threshold (ks) such that by applying the discrete probability law fitted during the previous step to an observation sequence having the given length (n), the probability that an anomaly score greater than or equal to the decision threshold (ks) will occur is less than the given alarm probability Pa or an elementary probability dependent on Pa in the case where a confirmation strategy is used.</description><language>fre</language><subject>CALCULATING ; COMPUTING ; CONTROL OR REGULATING SYSTEMS IN GENERAL ; CONTROLLING ; COUNTING ; DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FORADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORYOR FORECASTING PURPOSES ; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS ; MEASURING ; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS ; PHYSICS ; REGULATING ; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE,COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTINGPURPOSES, NOT OTHERWISE PROVIDED FOR ; TESTING ; TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES ; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</subject><creationdate>2016</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160610&DB=EPODOC&CC=FR&NR=3022997B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160610&DB=EPODOC&CC=FR&NR=3022997B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ALIMARDANI ARMAND, DARIOUCHE</creatorcontrib><creatorcontrib>MASSE JEAN-REMI, ANDRE</creatorcontrib><creatorcontrib>LALONDE PIERRE, GERALD</creatorcontrib><creatorcontrib>HUMEAU AURORE, FABIENNE, PAULE</creatorcontrib><creatorcontrib>FOIRET GUILHEM, ALCIDE, AUGUSTE</creatorcontrib><title>PROCEDE DE SURVEILLANCE D'UNE DEGRADATION D'UN DISPOSITIF EMBARQUE D'UN AERONEF INCLUANT LA DETERMINATION D'UN SEUIL DE COMPTAGE</title><description>A method of monitoring a degradation of a device on board an aircraft, implemented by a computer, the degree of the degradation of the onboard device being defined by an abnormality score formed by the counting of occurrences of anomalies noted by a control system of the device, the method of monitoring comprising a step of comparing an abnormality score obtained for an observation sequence of given length (n, t) with a decision threshold (ks) and a step of emitting an alarm in case of attainment or overshoot of the decision threshold (ks), the decision threshold (ks) being determined automatically for a given alarm probability Pa, corresponding to the probability that an alarm is emitted in the course of the monitoring method although the onboard device is healthy, by means of the following steps: a step of obtaining an abnormality score (r) on at least one reference sequence corresponding to flights of the aircraft without degradation and of length (m, tc) equal to a plurality of lengths (n, t) of observation sequences; a step of fitting a discrete probability law making it possible to retrieve the abnormality score (r) obtained on the reference sequence; a step of calculating the decision threshold (ks) such that by applying the discrete probability law fitted during the previous step to an observation sequence having the given length (n), the probability that an anomaly score greater than or equal to the decision threshold (ks) will occur is less than the given alarm probability Pa or an elementary probability dependent on Pa in the case where a confirmation strategy is used.</description><subject>CALCULATING</subject><subject>COMPUTING</subject><subject>CONTROL OR REGULATING SYSTEMS IN GENERAL</subject><subject>CONTROLLING</subject><subject>COUNTING</subject><subject>DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FORADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORYOR FORECASTING PURPOSES</subject><subject>FUNCTIONAL ELEMENTS OF SUCH SYSTEMS</subject><subject>MEASURING</subject><subject>MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS</subject><subject>PHYSICS</subject><subject>REGULATING</subject><subject>SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE,COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTINGPURPOSES, NOT OTHERWISE PROVIDED FOR</subject><subject>TESTING</subject><subject>TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES</subject><subject>TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjb0KwkAQhNNYiPoO21kJmhSScnPZiwuXu3g_tiHIWYkG4gP46CZqYSkMDPMxw8yTZ2ONoJJglAv2RKwUajHmddATrSyW6NnoN4GSXWMce5ZAdYH2GD5VQLJGkwTWQgXUHhSOa0-2Zv2zdxRYTWfC1I3HipbJ7NJdh7j6-iIBSV4cNrG_t3Hou3O8xUcrbbZN0zzfF7vsj8oLnhE7Nw</recordid><startdate>20160610</startdate><enddate>20160610</enddate><creator>ALIMARDANI ARMAND, DARIOUCHE</creator><creator>MASSE JEAN-REMI, ANDRE</creator><creator>LALONDE PIERRE, GERALD</creator><creator>HUMEAU AURORE, FABIENNE, PAULE</creator><creator>FOIRET GUILHEM, ALCIDE, AUGUSTE</creator><scope>EVB</scope></search><sort><creationdate>20160610</creationdate><title>PROCEDE DE SURVEILLANCE D'UNE DEGRADATION D'UN DISPOSITIF EMBARQUE D'UN AERONEF INCLUANT LA DETERMINATION D'UN SEUIL DE COMPTAGE</title><author>ALIMARDANI ARMAND, DARIOUCHE ; MASSE JEAN-REMI, ANDRE ; LALONDE PIERRE, GERALD ; HUMEAU AURORE, FABIENNE, PAULE ; FOIRET GUILHEM, ALCIDE, AUGUSTE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_FR3022997B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>fre</language><creationdate>2016</creationdate><topic>CALCULATING</topic><topic>COMPUTING</topic><topic>CONTROL OR REGULATING SYSTEMS IN GENERAL</topic><topic>CONTROLLING</topic><topic>COUNTING</topic><topic>DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FORADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORYOR FORECASTING PURPOSES</topic><topic>FUNCTIONAL ELEMENTS OF SUCH SYSTEMS</topic><topic>MEASURING</topic><topic>MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS</topic><topic>PHYSICS</topic><topic>REGULATING</topic><topic>SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE,COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTINGPURPOSES, NOT OTHERWISE PROVIDED FOR</topic><topic>TESTING</topic><topic>TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES</topic><topic>TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</topic><toplevel>online_resources</toplevel><creatorcontrib>ALIMARDANI ARMAND, DARIOUCHE</creatorcontrib><creatorcontrib>MASSE JEAN-REMI, ANDRE</creatorcontrib><creatorcontrib>LALONDE PIERRE, GERALD</creatorcontrib><creatorcontrib>HUMEAU AURORE, FABIENNE, PAULE</creatorcontrib><creatorcontrib>FOIRET GUILHEM, ALCIDE, AUGUSTE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ALIMARDANI ARMAND, DARIOUCHE</au><au>MASSE JEAN-REMI, ANDRE</au><au>LALONDE PIERRE, GERALD</au><au>HUMEAU AURORE, FABIENNE, PAULE</au><au>FOIRET GUILHEM, ALCIDE, AUGUSTE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>PROCEDE DE SURVEILLANCE D'UNE DEGRADATION D'UN DISPOSITIF EMBARQUE D'UN AERONEF INCLUANT LA DETERMINATION D'UN SEUIL DE COMPTAGE</title><date>2016-06-10</date><risdate>2016</risdate><abstract>A method of monitoring a degradation of a device on board an aircraft, implemented by a computer, the degree of the degradation of the onboard device being defined by an abnormality score formed by the counting of occurrences of anomalies noted by a control system of the device, the method of monitoring comprising a step of comparing an abnormality score obtained for an observation sequence of given length (n, t) with a decision threshold (ks) and a step of emitting an alarm in case of attainment or overshoot of the decision threshold (ks), the decision threshold (ks) being determined automatically for a given alarm probability Pa, corresponding to the probability that an alarm is emitted in the course of the monitoring method although the onboard device is healthy, by means of the following steps: a step of obtaining an abnormality score (r) on at least one reference sequence corresponding to flights of the aircraft without degradation and of length (m, tc) equal to a plurality of lengths (n, t) of observation sequences; a step of fitting a discrete probability law making it possible to retrieve the abnormality score (r) obtained on the reference sequence; a step of calculating the decision threshold (ks) such that by applying the discrete probability law fitted during the previous step to an observation sequence having the given length (n), the probability that an anomaly score greater than or equal to the decision threshold (ks) will occur is less than the given alarm probability Pa or an elementary probability dependent on Pa in the case where a confirmation strategy is used.</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | fre |
recordid | cdi_epo_espacenet_FR3022997B1 |
source | esp@cenet |
subjects | CALCULATING COMPUTING CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COUNTING DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FORADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORYOR FORECASTING PURPOSES FUNCTIONAL ELEMENTS OF SUCH SYSTEMS MEASURING MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PHYSICS REGULATING SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE,COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTINGPURPOSES, NOT OTHERWISE PROVIDED FOR TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR |
title | PROCEDE DE SURVEILLANCE D'UNE DEGRADATION D'UN DISPOSITIF EMBARQUE D'UN AERONEF INCLUANT LA DETERMINATION D'UN SEUIL DE COMPTAGE |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-29T04%3A40%3A56IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=ALIMARDANI%20ARMAND,%20DARIOUCHE&rft.date=2016-06-10&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EFR3022997B1%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |