FR3072650B1 - Systeme de controle d'une trajectoire laterale d'un aeronef au sol - Google Patents

Systeme de controle d'une trajectoire laterale d'un aeronef au sol Download PDF

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Publication number
FR3072650B1
FR3072650B1 FR1701107A FR1701107A FR3072650B1 FR 3072650 B1 FR3072650 B1 FR 3072650B1 FR 1701107 A FR1701107 A FR 1701107A FR 1701107 A FR1701107 A FR 1701107A FR 3072650 B1 FR3072650 B1 FR 3072650B1
Authority
FR
France
Prior art keywords
caster
angle
aircraft
setpoint
range
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
FR1701107A
Other languages
English (en)
Other versions
FR3072650A1 (fr
Inventor
Olivier Cantinaud
Laurent Goerig
Julien Prodigue
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 FR1701107A priority Critical patent/FR3072650B1/fr
Priority to CA3021110A priority patent/CA3021110A1/fr
Priority to US16/168,795 priority patent/US10486801B2/en
Priority to BR102018071751-0A priority patent/BR102018071751A2/pt
Publication of FR3072650A1 publication Critical patent/FR3072650A1/fr
Application granted granted Critical
Publication of FR3072650B1 publication Critical patent/FR3072650B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/50—Steerable undercarriages; Shimmy-damping
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42—Arrangement or adaptation of brakes
    • B64C25/426—Braking devices providing an automatic sequence of braking
    • 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
    • G05D1/0083—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots to help an aircraft pilot in the rolling phase
    • 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
    • G05D1/02—Control of position or course in two dimensions
    • G05D1/0202—Control of position or course in two dimensions specially adapted to aircraft
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/06—Traffic control systems for aircraft, e.g. air-traffic control [ATC] for control when on the ground
    • G08G5/065—Navigation or guidance aids, e.g. for taxiing or rolling
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface  wheeled type, e.g. multi-wheeled bogies
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Regulating Braking Force (AREA)
  • Steering Control In Accordance With Driving Conditions (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

Ce système (40) comprend un module (120) de commande configuré pour générer une commande d'une trajectoire latérale de consigne, un module de limitation (58) configuré pour déterminer, en fonction d'une vitesse et d'un angle de dérapage maximal autorisé de la roulette (5) de l'aéronef, une plage d'angle de braquage de la roulette (5) telle que, l'angle de braquage de la roulette (5) étant dans cette plage, l'angle de dérapage de la roulette (5) est inférieur audit angle de dérapage maximal, et un module de contrôle (130) configuré pour déterminer, en fonction de la commande, un angle de braquage de consigne compris dans ladite plage et propre à engendrer un mouvement latéral de l'aéronef conforme à ou tendant vers la trajectoire de consigne, et pour transmettre une instruction de braquage à la roulette (5) afin de l'orienter selon l'angle de consigne.
FR1701107A 2017-10-24 2017-10-24 Systeme de controle d'une trajectoire laterale d'un aeronef au sol Active FR3072650B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1701107A FR3072650B1 (fr) 2017-10-24 2017-10-24 Systeme de controle d'une trajectoire laterale d'un aeronef au sol
CA3021110A CA3021110A1 (fr) 2017-10-24 2018-10-16 Systeme de controle d'une trajectoire laterale d'un aeronef au sol
US16/168,795 US10486801B2 (en) 2017-10-24 2018-10-23 System for controlling a ground lateral trajectory of an aircraft
BR102018071751-0A BR102018071751A2 (pt) 2017-10-24 2018-10-23 Sistema de controle de uma trajetória lateral de uma aeronave e método para controlar uma trajetória lateral de uma aeronave

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1701107A FR3072650B1 (fr) 2017-10-24 2017-10-24 Systeme de controle d'une trajectoire laterale d'un aeronef au sol
FR1701107 2017-10-24

Publications (2)

Publication Number Publication Date
FR3072650A1 FR3072650A1 (fr) 2019-04-26
FR3072650B1 true FR3072650B1 (fr) 2021-07-30

Family

ID=63014581

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1701107A Active FR3072650B1 (fr) 2017-10-24 2017-10-24 Systeme de controle d'une trajectoire laterale d'un aeronef au sol

Country Status (4)

Country Link
US (1) US10486801B2 (fr)
BR (1) BR102018071751A2 (fr)
CA (1) CA3021110A1 (fr)
FR (1) FR3072650B1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110550233B (zh) * 2019-09-12 2021-09-07 中国商用飞机有限责任公司 飞机前轮转弯自动调校方法和系统
GB2588377A (en) * 2019-10-09 2021-04-28 Airbus Operations Ltd Heading control system
US11754408B2 (en) * 2019-10-09 2023-09-12 Argo AI, LLC Methods and systems for topological planning in autonomous driving
CN111479057B (zh) * 2020-04-13 2022-04-15 杭州今奥信息科技股份有限公司 基于无人飞行器的图斑智能举证方法
GB2605177A (en) * 2021-03-25 2022-09-28 Airbus Operations Ltd Monitoring system for an aircraft
CN116679750B (zh) * 2023-06-06 2024-03-29 北京理工大学 一种基于动态舵资源控制分配的飞行器制导控制方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1368975A1 (fr) 2001-03-09 2003-12-10 Ayman L.L.C. Systeme et procede d'identification d'un point de contact universel
JP5608918B2 (ja) * 2009-06-22 2014-10-22 独立行政法人 宇宙航空研究開発機構 航空機のステアリング角制御システム
DE102009060561A1 (de) * 2009-12-23 2011-06-30 Deutsches Zentrum für Luft- und Raumfahrt e.V., 51147 Steuervorrichtung für Flugzeuge
FR3001438B1 (fr) * 2013-01-30 2015-01-23 Airbus Operations Sas Procede et dispositif de pilotage lateral d'un aeronef roulant au sol.
GB2540182A (en) * 2015-07-08 2017-01-11 Airbus Operations Ltd Aircraft steering system controller
EP3232284B1 (fr) * 2016-04-11 2019-09-11 Airbus Operations Limited Procédé et appareil pour la commande d'un train d'atterrissage orientable

Also Published As

Publication number Publication date
BR102018071751A2 (pt) 2019-11-26
US10486801B2 (en) 2019-11-26
FR3072650A1 (fr) 2019-04-26
CA3021110A1 (fr) 2019-04-24
US20190118939A1 (en) 2019-04-25

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