FR2988835B1 - Procede de determination d'un etat de credibilite de mesures de capteurs d'un aeronef et systeme correspondant - Google Patents

Procede de determination d'un etat de credibilite de mesures de capteurs d'un aeronef et systeme correspondant

Info

Publication number
FR2988835B1
FR2988835B1 FR1200924A FR1200924A FR2988835B1 FR 2988835 B1 FR2988835 B1 FR 2988835B1 FR 1200924 A FR1200924 A FR 1200924A FR 1200924 A FR1200924 A FR 1200924A FR 2988835 B1 FR2988835 B1 FR 2988835B1
Authority
FR
France
Prior art keywords
aircraft
determining
sensor measurements
corresponding system
credibility state
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
FR1200924A
Other languages
English (en)
Other versions
FR2988835A1 (fr
Inventor
De Dinechin Sebastien Dupont
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.)
Dassault Aviation SA
Original Assignee
Dassault Aviation SA
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 Dassault Aviation SA filed Critical Dassault Aviation SA
Priority to FR1200924A priority Critical patent/FR2988835B1/fr
Priority to US14/388,781 priority patent/US10078100B2/en
Priority to PCT/EP2013/056368 priority patent/WO2013144126A2/fr
Publication of FR2988835A1 publication Critical patent/FR2988835A1/fr
Application granted granted Critical
Publication of FR2988835B1 publication Critical patent/FR2988835B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • B64D43/02—Arrangements or adaptations of instruments for indicating aircraft speed or stalling conditions
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B21/00—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01G—WEIGHING
    • G01G23/00—Auxiliary devices for weighing apparatus
    • G01G23/01—Testing or calibrating of weighing apparatus
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/06—Measuring arrangements specially adapted for aerodynamic testing
    • 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
    • G01P3/00—Measuring linear or angular speed; Measuring differences of linear or angular speeds
    • G01P3/64—Devices characterised by the determination of the time taken to traverse a fixed distance
    • G01P3/80—Devices characterised by the determination of the time taken to traverse a fixed distance using auto-correlation or cross-correlation detection means
    • G01P3/806—Devices characterised by the determination of the time taken to traverse a fixed distance using auto-correlation or cross-correlation detection means in devices of the type to be classified in G01P3/68
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
    • G01P5/16—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
FR1200924A 2012-03-28 2012-03-28 Procede de determination d'un etat de credibilite de mesures de capteurs d'un aeronef et systeme correspondant Active FR2988835B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1200924A FR2988835B1 (fr) 2012-03-28 2012-03-28 Procede de determination d'un etat de credibilite de mesures de capteurs d'un aeronef et systeme correspondant
US14/388,781 US10078100B2 (en) 2012-03-28 2013-03-26 Method for determining a state of credibility of measurements made by sensors of an aircraft and corresponding system
PCT/EP2013/056368 WO2013144126A2 (fr) 2012-03-28 2013-03-26 Procede de determination d'un etat de credibilite de mesures de capteurs d'un aeronef et systeme correspondant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1200924A FR2988835B1 (fr) 2012-03-28 2012-03-28 Procede de determination d'un etat de credibilite de mesures de capteurs d'un aeronef et systeme correspondant

Publications (2)

Publication Number Publication Date
FR2988835A1 FR2988835A1 (fr) 2013-10-04
FR2988835B1 true FR2988835B1 (fr) 2015-01-30

Family

ID=46889092

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1200924A Active FR2988835B1 (fr) 2012-03-28 2012-03-28 Procede de determination d'un etat de credibilite de mesures de capteurs d'un aeronef et systeme correspondant

Country Status (3)

Country Link
US (1) US10078100B2 (fr)
FR (1) FR2988835B1 (fr)
WO (1) WO2013144126A2 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104914271B (zh) * 2014-03-13 2020-01-14 波音公司 用于确定航空器的空速的空速计算系统和方法

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2988833B1 (fr) * 2012-03-28 2014-04-25 Dassault Aviat Dispositif d'affichage de caracteristiques de vol d'un aeronef, instrumentation pour aeronef et procede associe
US9933449B2 (en) * 2014-08-05 2018-04-03 Bae Systems Information And Electronic Systems Integration Inc. Method and system of measurement of mach and dynamic pressure using internal sensors
US10451491B2 (en) 2015-09-03 2019-10-22 Honeywell International Inc. System and method to determine total air temperature from turbofan bypass flow temperature
US10308370B2 (en) * 2016-06-12 2019-06-04 William L. Hinks Unusual state alarm and recovery director
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.
US10605822B2 (en) * 2017-06-12 2020-03-31 The Boeing Company System for estimating airspeed of an aircraft based on a weather buffer model
WO2019061000A1 (fr) * 2017-09-29 2019-04-04 Bombardier Inc. Procédé, système et indicateur graphique permettant la fourniture d'un centre de gravité latéral d'un aéronef
US10822109B2 (en) 2018-01-05 2020-11-03 The Boeing Company Methods and systems for determining airspeed of an aircraft
US11029706B2 (en) * 2018-12-07 2021-06-08 The Boeing Company Flight control system for determining a fault based on error between a measured and an estimated angle of attack
US11066189B2 (en) * 2018-12-07 2021-07-20 The Boeing Company Flight control system for determining estimated dynamic pressure based on lift and drag coefficients
US11003196B2 (en) 2018-12-07 2021-05-11 The Boeing Company Flight control system for determining a common mode pneumatic fault
WO2021050294A1 (fr) 2019-09-10 2021-03-18 Integrated Energy Services Corporation Système et procédé pour assurer la qualité de l'air d'un bâtiment
CN113751511B (zh) * 2020-06-04 2024-03-08 宝山钢铁股份有限公司 一种钢板厚度控制方法、计算机可读介质及电子设备
CN112697387B (zh) * 2020-12-23 2022-08-30 中国空气动力研究与发展中心超高速空气动力研究所 风洞气动热试验薄膜电阻温度计测量数据有效性分析方法
CN113177309B (zh) * 2021-04-23 2023-04-07 合肥赛为智能有限公司 一种基于决策算法的无人机冗余传感器的数据分析方法
EP4210024A1 (fr) * 2022-01-05 2023-07-12 Honeywell International Inc. Systèmes et procédés pour permettre à un utilisateur de contrôler l'utilisation de capteurs d'aéronef situés à bord d'un aéronef
CN114577433B (zh) * 2022-02-15 2023-06-20 中国航空工业集团公司哈尔滨空气动力研究所 一种风洞虚拟飞行试验天平气动力采集处理系统
CN114662625B (zh) * 2022-05-26 2022-10-25 成都飞机工业（集团）有限责任公司 一种飞行参数数据重构方法、装置、设备及介质

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2760268B1 (fr) 1997-03-03 1999-04-30 Aerospatiale Procede et dispositif pour verifier la coherence des mesures d'une sonde d'incidence
FR2857754B1 (fr) 2003-07-18 2005-09-23 Airbus France Procede et dispositif de surveillance de la validite d'une information de vitesse d'un aeronef et systeme de generation d'une information de vitesse comportant un tel dispositif
FR2898584B1 (fr) * 2006-03-15 2008-12-19 Airbus France Sas Procede et dispositif de commande de la poussee d'un aeronef multimoteur
FR2916276B1 (fr) * 2007-05-14 2009-08-28 Airbus France Sas Dispositif et procede d'estimation d'un angle d'incidence d'un aeronef
US8761970B2 (en) 2008-10-21 2014-06-24 The Boeing Company Alternative method to determine the air mass state of an aircraft and to validate and augment the primary method
US8527233B2 (en) * 2010-09-27 2013-09-03 The Boeing Company Airspeed sensing system for an aircraft
US8665120B2 (en) * 2011-05-25 2014-03-04 The Boeing Company Primary flight display pitch- and power-based unreliable airspeed symbology

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104914271B (zh) * 2014-03-13 2020-01-14 波音公司 用于确定航空器的空速的空速计算系统和方法

Also Published As

Publication number Publication date
US20150057960A1 (en) 2015-02-26
FR2988835A1 (fr) 2013-10-04
US10078100B2 (en) 2018-09-18
WO2013144126A3 (fr) 2013-11-14
WO2013144126A2 (fr) 2013-10-03

Similar Documents

Publication Publication Date Title
FR2988835B1 (fr) Procede de determination d'un etat de credibilite de mesures de capteurs d'un aeronef et systeme correspondant
FR2988851B1 (fr) Procede de determination d'un etat de credibilite de mesures d'un capteur d'incidence d'un aeronef et systeme correspondant
FR2988836B1 (fr) Procede de determination d'une masse estimee d'un aeronef et systeme correspondant
PL2675338T3 (pl) Układ i sposób mierzenia wewnętrznych wymiarów obiektu za pomocą optycznej tomografii koherencyjnej
FR3008805B3 (fr) Procede de determination de mesures oculaires avec un capteur grand public
DK2469296T3 (da) Optoelectronic sensor and method for recording and determining the distance of an object
FR2996302B1 (fr) Procede et systeme de mesure a capteurs multiples
BR112013017313A2 (pt) método e aparelho para monitorar vibração usando sensores de fibra ótica
WO2013030578A3 (fr) Procédé de détection de nucléosomes
FR2978858B1 (fr) Procede et systeme pour la determination de parametres de vol d'un aeronef
FR2987120B1 (fr) Procede et dispositif de mesure de la couleur d'un objet
FR2988829B1 (fr) Procede de mesure telemetrique et telemetre pour la mesure de distances, de longueurs, de surfaces et de niveaux
PL2458321T3 (pl) Sposób i urządzenie do pomiaru odstępów między powierzchniami optycznymi układu optycznego
FR2973883B1 (fr) Procede et systeme de detection d'un court-circuit affectant un capteur
FR2994273B1 (fr) Systeme de sonde, sonde mixte de reference primaire pour aeronef, aeronef et procede de mesure associes
FR2973882B1 (fr) Procede et dispositif pour la determination de diagnostics
IL208055A0 (en) Diagnosing system for consciousness level measurement and method thereof
HK1205262A1 (en) Methods for determining and or monitoring conditions of a three dimensional cell culture system and optical sensor device for conducting said methods
EP2843694A4 (fr) Système de mesure de caractéristiques de capacitance-tension (cv) et procédé pour mesurer des caractéristiques cv
FR3008073B1 (fr) Aeronef comprenant une sonde de mesure et procede de determination de parametres de vol d un tel aeronef
HK1212779A1 (zh) 借助測量用光學器件確定定距離下的景深的方法及裝置
FR2966926B1 (fr) Systeme interferometrique apolarise et procede de mesure interferometrique apolarise
EP2772014A4 (fr) Procédé et système d'évaluation d'observations de capteurs
FR3009281B1 (fr) Aeronef comprenant un systeme de mesure de pression et procede associe
FR2985070B1 (fr) Procede et systeme de detection de chutes de personnes

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 9

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