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FR3078811B1 - Procede de determination dynamique de la position du point d'arret d'un aeronef sur une piste d'atterissage, et systeme associe - Google Patents

Procede de determination dynamique de la position du point d'arret d'un aeronef sur une piste d'atterissage, et systeme associe Download PDF

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Publication number
FR3078811B1
FR3078811B1 FR1800196A FR1800196A FR3078811B1 FR 3078811 B1 FR3078811 B1 FR 3078811B1 FR 1800196 A FR1800196 A FR 1800196A FR 1800196 A FR1800196 A FR 1800196A FR 3078811 B1 FR3078811 B1 FR 3078811B1
Authority
FR
France
Prior art keywords
aircraft
determination
basis
deceleration profile
runway
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
FR1800196A
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English (en)
Other versions
FR3078811A1 (fr
Inventor
Stephane PICAUT
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 FR1800196A priority Critical patent/FR3078811B1/fr
Priority to US16/290,669 priority patent/US11069248B2/en
Priority to CA3035689A priority patent/CA3035689A1/fr
Priority to BR102019004392-0A priority patent/BR102019004392B1/pt
Publication of FR3078811A1 publication Critical patent/FR3078811A1/fr
Application granted granted Critical
Publication of FR3078811B1 publication Critical patent/FR3078811B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/50—Navigation or guidance aids
    • G08G5/54—Navigation or guidance aids for approach or landing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
    • B60T8/00—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force
    • B60T8/17—Using electrical or electronic regulation means to control braking
    • B60T8/1701—Braking or traction control means specially adapted for particular types of vehicles
    • B60T8/1703—Braking or traction control means specially adapted for particular types of vehicles for aircrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
    • B60T8/00—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force
    • B60T8/17—Using electrical or electronic regulation means to control braking
    • B60T8/172—Determining control parameters used in the regulation, e.g. by calculations involving measured or detected parameters
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/20—Instruments for performing navigational calculations
    • 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
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/70—Arrangements for monitoring traffic-related situations or conditions
    • G08G5/76—Arrangements for monitoring traffic-related situations or conditions for monitoring atmospheric conditions
    • 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
    • G08G5/20—Arrangements for acquiring, generating, sharing or displaying traffic information
    • G08G5/21—Arrangements for acquiring, generating, sharing or displaying traffic information located onboard the aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Regulating Braking Force (AREA)
  • Braking Arrangements (AREA)
  • Traffic Control Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Atmospheric Sciences (AREA)

Abstract

Ce procédé comprend les étapes suivantes : - détermination d'une première table (56) de temps moyen depuis le toucher de l'aéronef en fonction de la vitesse sol, sur la base d'un profil de décélération moyen (53) de l'aéronef ; - détermination d'un premier profil (60) de décélération adapté aux conditions courantes, sur la base d'une poussée moteur calculée pour chaque vitesse sol à partir du temps moyen déterminé dans la première table (56); - détermination d'une deuxième table (64) de temps adapté aux conditions courantes sur la base du premier profil (60) de décélération ; - détermination d'un deuxième profil (68) de décélération adapté aux conditions courantes, sur la base d'une poussée moteur calculée pour chaque vitesse sol à partir du temps déterminé dans la deuxième table (64); - calcul de la position du point d'arrêt (16) à partir du deuxième profil (68) de décélération adapté.
FR1800196A 2018-03-06 2018-03-06 Procede de determination dynamique de la position du point d'arret d'un aeronef sur une piste d'atterissage, et systeme associe Active FR3078811B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1800196A FR3078811B1 (fr) 2018-03-06 2018-03-06 Procede de determination dynamique de la position du point d'arret d'un aeronef sur une piste d'atterissage, et systeme associe
US16/290,669 US11069248B2 (en) 2018-03-06 2019-03-01 Dynamic determination method for determining the position of a stopping point of an aircraft on a landing strip and related system
CA3035689A CA3035689A1 (fr) 2018-03-06 2019-03-04 Procede de determination dynamique de la position du point d'arret d'un aeronef sur une piste d'atterissage, et systeme associe
BR102019004392-0A BR102019004392B1 (pt) 2018-03-06 2019-03-06 Método de determinação dinâmica para determinar a posição do ponto de parada de uma aeronave e sistema de determinação dinâmica para determinar a posição do ponto de parada de uma aeronave

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1800196A FR3078811B1 (fr) 2018-03-06 2018-03-06 Procede de determination dynamique de la position du point d'arret d'un aeronef sur une piste d'atterissage, et systeme associe
FR1800196 2018-03-06

Publications (2)

Publication Number Publication Date
FR3078811A1 FR3078811A1 (fr) 2019-09-13
FR3078811B1 true FR3078811B1 (fr) 2020-04-03

Family

ID=62528523

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1800196A Active FR3078811B1 (fr) 2018-03-06 2018-03-06 Procede de determination dynamique de la position du point d'arret d'un aeronef sur une piste d'atterissage, et systeme associe

Country Status (3)

Country Link
US (1) US11069248B2 (fr)
CA (1) CA3035689A1 (fr)
FR (1) FR3078811B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2599167A (en) * 2020-09-29 2022-03-30 Airbus Operations Ltd Aircraft system
CN114460947B (zh) * 2022-01-19 2024-07-26 江苏深蓝航天有限公司 一种飞行器回收下降减速方法、飞行器
CN119024865B (zh) * 2024-10-28 2025-02-07 四川沃飞长空科技发展有限公司 飞行器着陆辅助方法、装置、设备以及存储介质

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8346455B2 (en) * 2005-02-23 2013-01-01 Zoltan Ivan Rado Method and device for communicating true runway braking performance using data from the flight data management systems of landed aircraft
FR2895726B1 (fr) * 2006-01-03 2009-10-23 Thales Sa Systeme et procede d'assistance au freinage d'un aeronef sur une piste d'atterrissage
US7586422B2 (en) * 2006-08-02 2009-09-08 The Boeing Company Determination of runway landing conditions
US7626513B2 (en) * 2006-08-02 2009-12-01 The Boeing Company Communication of landing conditions
US7818100B2 (en) * 2007-04-03 2010-10-19 The Boeing Company System and method for optimized runway exiting
FR2936079B1 (fr) * 2008-09-16 2010-09-17 Thales Sa Procede de surveillance de la phase d'atterrissage d'un aeronef.
FR2936077B1 (fr) * 2008-09-16 2014-12-12 Airbus France Procede et dispositif d'aide au pilotage d'un aeronef lors d'une phase d'atterrissage.
FR2988671B1 (fr) * 2012-03-30 2014-04-04 Airbus Procede de commande du freinage d’un avion sur une piste d’atterrissage et avion apte a mettre en oeuvre ce procede
FR2998702B1 (fr) * 2012-11-27 2015-12-18 Dassault Aviat Procede de determination dynamique de la position du point d'arret d'un aeronef sur un terrain, et systeme associe
US9340300B2 (en) * 2013-09-16 2016-05-17 The Boeing Company On-ground braking alerts for airplanes
US9082301B2 (en) * 2013-10-28 2015-07-14 The Boeing Company Aircraft stopping performance display and warning
US20150127196A1 (en) * 2013-11-06 2015-05-07 Honeywell International Inc. System and method for alerting of remaining runway upon landing based on deceleration
US9428161B2 (en) * 2013-11-19 2016-08-30 Goodrich Corporation Brake control initiation using tire runway friction map data
US10576948B2 (en) * 2015-12-08 2020-03-03 Airbus Group India Private Limited Aircraft braking based on real time runway condition
FR3045197B1 (fr) * 2015-12-11 2018-01-26 Airbus Procede et systeme ameliores d'aide au pilotage d'un aeronef en phase d'atterrissage
FR3049265B1 (fr) * 2016-03-24 2019-09-13 Airbus Operations Procede et dispositif d'affichage d'une symbologie d'aide au pilotage d'un aeronef lors d'une phase d'atterrissage
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US20190054906A1 (en) * 2017-08-18 2019-02-21 Rockwell Collins, Inc. Aircraft braking system and method using runway condition parameters

Also Published As

Publication number Publication date
US20190279517A1 (en) 2019-09-12
US11069248B2 (en) 2021-07-20
FR3078811A1 (fr) 2019-09-13
BR102019004392A2 (pt) 2019-09-17
CA3035689A1 (fr) 2019-09-06

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