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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; ARRANGEMENT 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

Landscapes

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

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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
CN111148980A (zh) * 2017-09-29 2020-05-12 庞巴迪公司 用于提供飞行器的横向重心的方法、系统和图形指示器
US10822109B2 (en) 2018-01-05 2020-11-03 The Boeing Company Methods and systems for determining airspeed of an aircraft
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
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
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
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
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
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

Family Cites Families (7)

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

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