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FR3013834B1 - Methode de fusion de donnees de capteurs utilisant un critere de coherence - Google Patents

Methode de fusion de donnees de capteurs utilisant un critere de coherence

Info

Publication number
FR3013834B1
FR3013834B1 FR1361754A FR1361754A FR3013834B1 FR 3013834 B1 FR3013834 B1 FR 3013834B1 FR 1361754 A FR1361754 A FR 1361754A FR 1361754 A FR1361754 A FR 1361754A FR 3013834 B1 FR3013834 B1 FR 3013834B1
Authority
FR
France
Prior art keywords
measurements
parameter
sensors
main
sensor data
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.)
Active
Application number
FR1361754A
Other languages
English (en)
Other versions
FR3013834A1 (fr
Inventor
Patrice Brot
Emmanuel Fall
Corinne Mailhes
Jean-Yves Tourneret
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 FR1361754A priority Critical patent/FR3013834B1/fr
Priority to US14/553,125 priority patent/US9268330B2/en
Priority to CN201410709508.9A priority patent/CN104677379B/zh
Publication of FR3013834A1 publication Critical patent/FR3013834A1/fr
Application granted granted Critical
Publication of FR3013834B1 publication Critical patent/FR3013834B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D3/00—Indicating or recording apparatus with provision for the special purposes referred to in the subgroups
    • G01D3/08—Indicating or recording apparatus with provision for the special purposes referred to in the subgroups with provision for safeguarding the apparatus, e.g. against abnormal operation, against breakdown
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P13/00—Indicating or recording presence, absence, or direction, of movement
    • G01P13/02—Indicating direction only, e.g. by weather vane
    • G01P13/025—Indicating direction only, e.g. by weather vane indicating air data, i.e. flight variables of an aircraft, e.g. angle of attack, side slip, shear, yaw
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P21/00—Testing or calibrating of apparatus or devices covered by the preceding groups
    • G01P21/02—Testing or calibrating of apparatus or devices covered by the preceding groups of speedometers
    • G01P21/025—Testing or calibrating of apparatus or devices covered by the preceding groups of speedometers for measuring speed of fluids; for measuring speed of bodies relative to fluids

Landscapes

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

Abstract

L'invention concerne une méthode de fusion de données capable de fusionner les mesures d'un paramètre, par exemple un paramètre de vol d'un aéronef, prises par une pluralité de capteurs comprenant un ensemble de capteurs principaux et des ensembles de capteurs secondaires. On détermine l'écart entre chaque mesure principale et les mesures secondaires (410) et on en déduit un score de cohérence avec celles-ci (420). Pour chaque configuration de panne des capteurs principaux, on effectue une première estimation, dite conditionnelle, dudit paramètre (430) et l'on calcule un coefficient de pondération relatif à cette panne, tenant compte des scores de cohérence des mesures principales (440). Le paramètre est ensuite estimé en effectuant une combinaison des mesures conditionnelles avec les coefficients de pondération associés (450).
FR1361754A 2013-11-28 2013-11-28 Methode de fusion de donnees de capteurs utilisant un critere de coherence Active FR3013834B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1361754A FR3013834B1 (fr) 2013-11-28 2013-11-28 Methode de fusion de donnees de capteurs utilisant un critere de coherence
US14/553,125 US9268330B2 (en) 2013-11-28 2014-11-25 Method for fusing data from sensors using a consistency criterion
CN201410709508.9A CN104677379B (zh) 2013-11-28 2014-11-28 用于使用一致性准则融合来自传感器的数据的方法

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1361754A FR3013834B1 (fr) 2013-11-28 2013-11-28 Methode de fusion de donnees de capteurs utilisant un critere de coherence

Publications (2)

Publication Number Publication Date
FR3013834A1 FR3013834A1 (fr) 2015-05-29
FR3013834B1 true FR3013834B1 (fr) 2015-12-25

Family

ID=50231328

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1361754A Active FR3013834B1 (fr) 2013-11-28 2013-11-28 Methode de fusion de donnees de capteurs utilisant un critere de coherence

Country Status (3)

Country Link
US (1) US9268330B2 (fr)
CN (1) CN104677379B (fr)
FR (1) FR3013834B1 (fr)

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CN107543540B (zh) * 2016-06-27 2020-05-15 杭州海康机器人技术有限公司 一种飞行设备的数据融合和飞行模式切换方法及装置
CN106778883A (zh) * 2016-12-23 2017-05-31 贵州电网有限责任公司电力科学研究院 一种基于模糊集合的证据理论智能巡检信息融合方法
FR3065543B1 (fr) * 2017-04-19 2019-05-03 Airbus Operations (S.A.S.) Calculateur de commande de vol d'un aeronef
FR3066755B1 (fr) * 2017-05-23 2019-06-07 Airbus Operations Procede et dispositif de surveillance et d'estimation de parametres relatifs au vol d'un aeronef.
US10948511B2 (en) 2018-03-05 2021-03-16 Honeywell International Inc. Apparatus and method for verifying operation of air data probes
FR3080197A1 (fr) * 2018-04-13 2019-10-18 Airbus Operations Procede et systeme de fusion de mesures de parametres de vol d'un aeronef.
CN109982287B (zh) * 2019-03-13 2021-10-15 北京工业大学 基于zigbee无线传感器网络的林业多传感器火警告警系统
CN111058958B (zh) * 2019-12-11 2022-01-07 厦门林巴贺航空发动机股份有限公司 一种活塞式航空发动机的控制方法
CN111257592B (zh) * 2020-03-05 2022-04-12 广东零偏科技有限公司 一种用于检测装置的静态判别的方法
CN111694342B (zh) * 2020-06-12 2023-05-16 中国船舶重工集团公司第七0三研究所 一种基于相似度的工业锅炉故障诊断方法
CN112003891B (zh) * 2020-07-16 2022-09-06 山东派蒙机电技术有限公司 用于智能网联车辆控制器的多传感数据融合方法
FR3113518B1 (fr) 2020-08-24 2022-08-26 Arianegroup Sas Procédé de détermination de panne pour un ensemble de capteurs
KR20220025585A (ko) 2020-08-24 2022-03-03 삼성전자주식회사 위치 추정 방법 및 장치
CN112903008B (zh) * 2021-01-15 2023-01-10 泉州师范学院 基于多传感数据融合技术的山体滑坡预警方法
FR3121430B1 (fr) 2021-04-06 2023-10-20 Airbus Helicopters Système d’affichage de données d’un aéronef
CN114034338B (zh) * 2021-10-29 2023-08-11 国网安徽省电力有限公司电力科学研究院 一种基于改进d-s证据理论的开关柜多源参量监测方法
CN115270266B (zh) * 2022-08-03 2023-06-30 南昌大学 基于改进层次分析法的边坡监测状态风险判断方法
CN115469136A (zh) * 2022-10-25 2022-12-13 南方电网数字电网研究院有限公司 一种基于电场传感器阵列的非侵入式三相电压测量方法
CN115982646B (zh) * 2023-03-20 2023-07-18 西安弘捷电子技术有限公司 一种基于云平台的多源测试数据的管理方法及系统

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JP4229358B2 (ja) * 2001-01-22 2009-02-25 株式会社小松製作所 無人車両の走行制御装置
DE10297009B4 (de) * 2001-06-25 2020-07-23 Schneider Electric Systems Usa, Inc. Sensorfusion unter Verwendung von selbstvaluierenden Prozesssensoren
US7099796B2 (en) * 2001-10-22 2006-08-29 Honeywell International Inc. Multi-sensor information fusion technique
FR2857447B1 (fr) * 2003-07-07 2005-09-30 Airbus France Procede et dispositif pour surveiller la validite d'au moins un parametre qui est calcule par une centrale anemometrique d'un aeronef
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EP2159779B1 (fr) * 2008-08-27 2013-01-16 Saab Ab Utilisation d'un capteur d'images et d'un filtre de suivi de temps restant pour éviter les collisions dans l'espace
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FR2978858B1 (fr) * 2011-08-01 2013-08-30 Airbus Operations Sas Procede et systeme pour la determination de parametres de vol d'un aeronef
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Also Published As

Publication number Publication date
US20150148997A1 (en) 2015-05-28
US9268330B2 (en) 2016-02-23
CN104677379A (zh) 2015-06-03
CN104677379B (zh) 2019-11-29
FR3013834A1 (fr) 2015-05-29

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