WO2013144126A3 - 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 Download PDF

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Publication number
WO2013144126A3
WO2013144126A3 PCT/EP2013/056368 EP2013056368W WO2013144126A3 WO 2013144126 A3 WO2013144126 A3 WO 2013144126A3 EP 2013056368 W EP2013056368 W EP 2013056368W WO 2013144126 A3 WO2013144126 A3 WO 2013144126A3
Authority
WO
WIPO (PCT)
Prior art keywords
determining
aircraft
state
sensors
credibility
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.)
Ceased
Application number
PCT/EP2013/056368
Other languages
English (en)
Other versions
WO2013144126A2 (fr
Inventor
Sébastien DUPONT DE DINECHIN
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 US14/388,781 priority Critical patent/US10078100B2/en
Publication of WO2013144126A2 publication Critical patent/WO2013144126A2/fr
Publication of WO2013144126A3 publication Critical patent/WO2013144126A3/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P21/00Testing or calibrating of apparatus or devices covered by the preceding groups
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00Arrangements or adaptations of instruments
    • B64D43/02Arrangements or adaptations of instruments for indicating aircraft speed or stalling conditions
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B21/00Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01GWEIGHING
    • G01G23/00Auxiliary devices for weighing apparatus
    • G01G23/01Testing or calibrating of weighing apparatus
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/06Measuring arrangements specially adapted for aerodynamic testing
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P13/00Indicating or recording presence, absence, or direction, of movement
    • G01P13/02Indicating direction only, e.g. by weather vane
    • G01P13/025Indicating 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
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P3/00Measuring linear or angular speed; Measuring differences of linear or angular speeds
    • G01P3/64Devices characterised by the determination of the time taken to traverse a fixed distance
    • G01P3/80Devices characterised by the determination of the time taken to traverse a fixed distance using auto-correlation or cross-correlation detection means
    • G01P3/806Devices 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
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14Measuring 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
    • G01P5/16Measuring 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

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid Mechanics (AREA)
  • Measuring Fluid Pressure (AREA)

Abstract

Ce procédé de détermination d'un état de crédibilité de mesures de capteurs de pressions statique et totale et d'incidence d'un aéronef comprend les étapes suivantes : - déterminer (31) une vitesse de l'aéronef, à partir de mesures de pressions statique et totale, - déterminer (33) un coefficient de portance de l'aéronef à partir d'une mesure (31) d'incidence et de ladite vitesse, - déterminer (39) une masse de l'aéronef, - déterminer (70) si une équation de sustentation de l'aéronef est vérifiée, - activer un état de crédibilité optimale (74), dans lequel les mesures desdits capteurs sont jugées fiables, si ladite équation de sustentation est vérifiée, - activer (75, 83) un état de crédibilité non optimale (76; 84), dans lequel les mesures d'au moins un capteur sont jugées non fiables, si ladite équation de sustentation n'est pas vérifiée.
PCT/EP2013/056368 2012-03-28 2013-03-26 Procede de determination d'un etat de credibilite de mesures de capteurs d'un aeronef et systeme correspondant Ceased WO2013144126A2 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
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

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1200924 2012-03-28
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
WO2013144126A2 WO2013144126A2 (fr) 2013-10-03
WO2013144126A3 true WO2013144126A3 (fr) 2013-11-14

Family

ID=46889092

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2013/056368 Ceased 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

Country Status (3)

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

Families Citing this family (24)

* 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
US9383381B2 (en) * 2014-03-13 2016-07-05 The Boeing Company Airspeed calculation system for an aircraft
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
US11661206B2 (en) * 2017-09-29 2023-05-30 Bombardier Inc. Method, system, and graphical indicator for providing a lateral center of gravity of an aircraft
US10822109B2 (en) 2018-01-05 2020-11-03 The Boeing Company Methods and systems for determining airspeed of an aircraft
US11003196B2 (en) 2018-12-07 2021-05-11 The Boeing Company Flight control system for determining a common mode pneumatic fault
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
US11976832B2 (en) 2019-09-10 2024-05-07 Integrated Energy Services Corporation System and method for assuring building air quality
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
US12091189B2 (en) 2022-01-05 2024-09-17 Honeywell International Inc. Systems and methods for enabling user control over use of aircraft sensors located onboard an aircraft
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
CN118913607B (zh) * 2024-07-10 2025-10-28 中国特种飞行器研究所 一种适用于对流层载人飞艇试飞稳定性试飞方法
CN118936818B (zh) * 2024-07-10 2025-10-28 中国特种飞行器研究所 一种适用于对流层载人飞艇的全发爬升、下滑性能试飞方法
CN119085735B (zh) * 2024-11-06 2025-02-21 山东交通学院 一种用于水下爆炸检测的传感器数据分析系统

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0863451A1 (fr) * 1997-03-03 1998-09-09 Aerospatiale Societe Nationale Industrielle Procédé et dispositif pour vérifier la cohérence des mesures d'une sonde d'incidence
EP1498737A1 (fr) * 2003-07-18 2005-01-19 Airbus France Procédé et dispositif de surveillance de la validité d'une information de vitesse d'un aéronef
WO2007104851A1 (fr) * 2006-03-15 2007-09-20 Airbus France Procede et dispositif de commande de la poussee d'un aeronef multimoteur
US20100100260A1 (en) * 2008-10-21 2010-04-22 Mcintyre Melville Duncan Walter Alternative method to determine the air mass state of an aircraft and to validate and augment the primary method

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2916276B1 (fr) * 2007-05-14 2009-08-28 Airbus France Sas Dispositif et procede d'estimation d'un angle d'incidence d'un aeronef
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

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0863451A1 (fr) * 1997-03-03 1998-09-09 Aerospatiale Societe Nationale Industrielle Procédé et dispositif pour vérifier la cohérence des mesures d'une sonde d'incidence
EP1498737A1 (fr) * 2003-07-18 2005-01-19 Airbus France Procédé et dispositif de surveillance de la validité d'une information de vitesse d'un aéronef
WO2007104851A1 (fr) * 2006-03-15 2007-09-20 Airbus France Procede et dispositif de commande de la poussee d'un aeronef multimoteur
US20100100260A1 (en) * 2008-10-21 2010-04-22 Mcintyre Melville Duncan Walter Alternative method to determine the air mass state of an aircraft and to validate and augment the primary method

Also Published As

Publication number Publication date
US20150057960A1 (en) 2015-02-26
FR2988835B1 (fr) 2015-01-30
WO2013144126A2 (fr) 2013-10-03
US10078100B2 (en) 2018-09-18
FR2988835A1 (fr) 2013-10-04

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