FR3032044B1 - Procede et dispositif d'aide a l'atterrissage d'un aeronef lors d'une phase d'arrondi. - Google Patents

Procede et dispositif d'aide a l'atterrissage d'un aeronef lors d'une phase d'arrondi. Download PDF

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Publication number
FR3032044B1
FR3032044B1 FR1550654A FR1550654A FR3032044B1 FR 3032044 B1 FR3032044 B1 FR 3032044B1 FR 1550654 A FR1550654 A FR 1550654A FR 1550654 A FR1550654 A FR 1550654A FR 3032044 B1 FR3032044 B1 FR 3032044B1
Authority
FR
France
Prior art keywords
deflection angle
landing
assisting
unit
aircraft
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
FR1550654A
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English (en)
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FR3032044A1 (fr
Inventor
Matthias Eberle
Philippe Perrin
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
Airbus SAS
Original Assignee
Airbus Operations SAS
Airbus 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, Airbus SAS filed Critical Airbus Operations SAS
Priority to FR1550654A priority Critical patent/FR3032044B1/fr
Priority to US15/005,387 priority patent/US9776733B2/en
Publication of FR3032044A1 publication Critical patent/FR3032044A1/fr
Application granted granted Critical
Publication of FR3032044B1 publication Critical patent/FR3032044B1/fr
Active 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
    • 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
    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • 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
    • B64D47/00—Equipment not otherwise provided for
    • B64D47/02—Arrangements or adaptations of signal or lighting devices
    • 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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/085—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability to ensure coordination between different movements
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
    • G08G5/0021—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located in the aircraft
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/02—Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
    • G08G5/025—Navigation or guidance aids

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)

Abstract

- Procédé et dispositif d'aide à l'atterrissage d'un aéronef lors d'une phase d'arrondi. - Le dispositif (1) comprend un manche de commande, une première unité (11) d'acquisition de paramètres de vol courants de l'aéronef, une seconde unité (12) d'acquisition d'un angle de déflexion courant du manche de commande, une unité de calcul (13) pour calculer la différence entre l'angle de déflexion courant du manche de commande et un angle de déflexion cible du manche de commande, et une unité d'émission acoustique (14) configurée pour émettre automatiquement un signal sonore, d'alerte ou de guidage, dans le poste de pilotage de l'aéronef, en fonction de ladite différence entre l'angle de déflexion courant et l'angle de déflexion cible du manche de commande.
FR1550654A 2015-01-28 2015-01-28 Procede et dispositif d'aide a l'atterrissage d'un aeronef lors d'une phase d'arrondi. Active FR3032044B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1550654A FR3032044B1 (fr) 2015-01-28 2015-01-28 Procede et dispositif d'aide a l'atterrissage d'un aeronef lors d'une phase d'arrondi.
US15/005,387 US9776733B2 (en) 2015-01-28 2016-01-25 Method and device for assisting in the landing of an aircraft in a flare phase

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1550654 2015-01-28
FR1550654A FR3032044B1 (fr) 2015-01-28 2015-01-28 Procede et dispositif d'aide a l'atterrissage d'un aeronef lors d'une phase d'arrondi.

Publications (2)

Publication Number Publication Date
FR3032044A1 FR3032044A1 (fr) 2016-07-29
FR3032044B1 true FR3032044B1 (fr) 2020-07-17

Family

ID=52737343

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1550654A Active FR3032044B1 (fr) 2015-01-28 2015-01-28 Procede et dispositif d'aide a l'atterrissage d'un aeronef lors d'une phase d'arrondi.

Country Status (2)

Country Link
US (1) US9776733B2 (fr)
FR (1) FR3032044B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3044810A1 (fr) * 2015-12-04 2017-06-09 Airbus Operations Sas Systeme d’aide a la gestion du vol d’un aeronef lors d’une phase d’atterrissage.
FR3056004B1 (fr) * 2016-09-14 2020-12-25 Airbus Operations Sas Procede et dispositif d'aide a l'atterrissage d'un aeronef lors d'une manoeuvre d'arrondi.

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3327973A (en) * 1965-06-14 1967-06-27 Lear Siegler Inc Automatic landing pitch axis control system for aircraft
US3604908A (en) * 1969-05-19 1971-09-14 Sperry Rand Corp Landing control system for aircraft
US4057782A (en) 1976-04-05 1977-11-08 Sundstrand Data Control, Inc. Low altitude head up display for aircraft
US4619110A (en) * 1983-07-13 1986-10-28 Moore M Samuel Helicopter engine warning or control system
GB9003653D0 (en) * 1990-02-17 1990-04-11 Smiths Industries Plc Aircraft performance monitoring
FR2717934B1 (fr) * 1994-03-22 1996-04-26 Sextant Avionique Dispositif d'évitement de collisions pour aéronef notamment avec le sol par contrôle de pente d'approche.
FR2914446B1 (fr) * 2007-03-30 2009-07-10 Airbus France Sas Procede et dispositif de modification du volume sonore d'un signal d'avertissement audio a bord d'un aeronef
US8416152B2 (en) * 2008-06-11 2013-04-09 Honeywell International Inc. Method and system for operating a near-to-eye display
US8374736B1 (en) * 2009-12-02 2013-02-12 The Boeing Company Runway slope compensation for an automatic landing system
US8831799B1 (en) * 2013-04-04 2014-09-09 The Boeing Company Flight director flare guidance

Also Published As

Publication number Publication date
US9776733B2 (en) 2017-10-03
FR3032044A1 (fr) 2016-07-29
US20160214736A1 (en) 2016-07-28

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