FR3027397B1 - Procede et dispositif d'estimation automatique d'au moins une vitesse d'un aeronef - Google Patents

Procede et dispositif d'estimation automatique d'au moins une vitesse d'un aeronef Download PDF

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Publication number
FR3027397B1
FR3027397B1 FR1460067A FR1460067A FR3027397B1 FR 3027397 B1 FR3027397 B1 FR 3027397B1 FR 1460067 A FR1460067 A FR 1460067A FR 1460067 A FR1460067 A FR 1460067A FR 3027397 B1 FR3027397 B1 FR 3027397B1
Authority
FR
France
Prior art keywords
speed
aircraft
data
automatically estimating
determining
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.)
Expired - Fee Related
Application number
FR1460067A
Other languages
English (en)
Other versions
FR3027397A1 (fr
Inventor
Philippe Goupil
Remy Dayre
Nicola Mimmo
Pierre Chevalier
Daniel Lopez Fernandez
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 FR1460067A priority Critical patent/FR3027397B1/fr
Priority to US14/886,727 priority patent/US9776729B2/en
Priority to CN201510678320.7A priority patent/CN105527455B/zh
Publication of FR3027397A1 publication Critical patent/FR3027397A1/fr
Application granted granted Critical
Publication of FR3027397B1 publication Critical patent/FR3027397B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • 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
    • 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
    • G01P5/02—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring forces exerted by the fluid on solid bodies, e.g. anemometer
    • 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

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Feedback Control In General (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Regulating Braking Force (AREA)

Abstract

- Procédé et dispositif d'estimation automatique d'au moins une vitesse d'un aéronef. - Le dispositif (1) comporte une première unité de génération de données (2) pour déterminer au moins un moment de charnière aérodynamique d'au moins une surface de commande (3) de l'aéronef, une seconde unité de génération de données (4) pour déterminer une pluralité de données et au moins une pression statique externe et un modèle de coefficient de moment de charnière, une unité de calcul (5) pour calculer à l'aide de ces données au moins une vitesse de l'aéronef, à savoir un nombre de Mach et/ou une vitesse conventionnelle, et une unité de transmission de données (10) pour fournir cette vitesse à un système utilisateur.
FR1460067A 2014-10-20 2014-10-20 Procede et dispositif d'estimation automatique d'au moins une vitesse d'un aeronef Expired - Fee Related FR3027397B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1460067A FR3027397B1 (fr) 2014-10-20 2014-10-20 Procede et dispositif d'estimation automatique d'au moins une vitesse d'un aeronef
US14/886,727 US9776729B2 (en) 2014-10-20 2015-10-19 Method and system for automatically estimating at least one speed of an aircraft
CN201510678320.7A CN105527455B (zh) 2014-10-20 2015-10-20 用于自动地估计飞行器的至少一个速度的方法及装置

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1460067A FR3027397B1 (fr) 2014-10-20 2014-10-20 Procede et dispositif d'estimation automatique d'au moins une vitesse d'un aeronef
FR1460067 2014-10-20

Publications (2)

Publication Number Publication Date
FR3027397A1 FR3027397A1 (fr) 2016-04-22
FR3027397B1 true FR3027397B1 (fr) 2019-05-03

Family

ID=52273279

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1460067A Expired - Fee Related FR3027397B1 (fr) 2014-10-20 2014-10-20 Procede et dispositif d'estimation automatique d'au moins une vitesse d'un aeronef

Country Status (3)

Country Link
US (1) US9776729B2 (fr)
CN (1) CN105527455B (fr)
FR (1) FR3027397B1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3024238B1 (fr) * 2014-07-23 2016-12-09 Airbus Operations Sas Procede et dispositif d'estimation du nombre de mach 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
GB2579696A (en) * 2017-09-01 2020-07-01 Thales Canada Inc Method and system for determining an estimation of an anemometric parameter in an aircraft
EP3462178B1 (fr) * 2017-09-22 2021-05-26 Rosemount Aerospace Inc. Architecture de données d'air à profil bas
FR3127047B1 (fr) * 2021-09-15 2023-09-22 Airbus Operations Sas Système et procédé d’estimation automatique d’une vitesse d’un aéronef lors d’un vol de l’aéronef.

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2853256A (en) * 1954-08-23 1958-09-23 Boeing Co Internal resistance plate for aircraft control surfaces
US5099245A (en) * 1987-10-23 1992-03-24 Hughes Aircraft Company Vehicle location system accuracy enhancement for airborne vehicles
US5078338A (en) * 1990-01-19 1992-01-07 Neill Terrence O Means for maintaining a desired relationship between roll and yaw stability in a swept-wing aircraft by varying dihedral as a function of lift coefficient
US6685138B1 (en) * 2002-11-25 2004-02-03 The Boeing Company Augmenting flight control surface actuation system and method
CN101706512B (zh) * 2009-11-25 2011-06-15 哈尔滨工业大学 基于星敏感器的姿态测量信息和飞轮的角动量测量信息的航天器伪速率的估计方法
US8374804B2 (en) * 2010-02-12 2013-02-12 Honeywell International Inc. Aircraft dynamic pressure estimation system and method
CN102901595B (zh) * 2012-10-12 2014-07-16 中国航空工业集团公司沈阳飞机设计研究所 一种舵面铰链力矩测量方法
DE102013101351A1 (de) 2013-02-12 2014-08-14 Airbus Operations Gmbh Verfahren und Einrichtung zum Ermitteln der Geschwindigkeit eines Luftfahrzeugs

Also Published As

Publication number Publication date
US20160107762A1 (en) 2016-04-21
CN105527455B (zh) 2019-11-01
FR3027397A1 (fr) 2016-04-22
CN105527455A (zh) 2016-04-27
US9776729B2 (en) 2017-10-03

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