ATE406606T1 - Verfahren zum unterstützten abheben für flugzeuge - Google Patents

Verfahren zum unterstützten abheben für flugzeuge

Info

Publication number
ATE406606T1
ATE406606T1 AT06743759T AT06743759T ATE406606T1 AT E406606 T1 ATE406606 T1 AT E406606T1 AT 06743759 T AT06743759 T AT 06743759T AT 06743759 T AT06743759 T AT 06743759T AT E406606 T1 ATE406606 T1 AT E406606T1
Authority
AT
Austria
Prior art keywords
aircraft
reference value
assisted take
accordance
deviation
Prior art date
Application number
AT06743759T
Other languages
English (en)
Inventor
Gerard Mathieu
Franck Delaplace
Tron Xavier Le
Original Assignee
Airbus France
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 France filed Critical Airbus France
Application granted granted Critical
Publication of ATE406606T1 publication Critical patent/ATE406606T1/de

Links

Classifications

    • 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
    • G05D1/0661—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Control Of Position Or Direction (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Vehicle Body Suspensions (AREA)
  • Control Of Electric Motors In General (AREA)
  • Steering Controls (AREA)
  • Macromonomer-Based Addition Polymer (AREA)
  • Bridges Or Land Bridges (AREA)
  • Control And Safety Of Cranes (AREA)
  • Attitude Control For Articles On Conveyors (AREA)
  • Toys (AREA)
AT06743759T 2005-05-10 2006-05-04 Verfahren zum unterstützten abheben für flugzeuge ATE406606T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0504662A FR2885706B1 (fr) 2005-05-10 2005-05-10 Procede d'aide au decollage d'un aeronef.

Publications (1)

Publication Number Publication Date
ATE406606T1 true ATE406606T1 (de) 2008-09-15

Family

ID=35559480

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06743759T ATE406606T1 (de) 2005-05-10 2006-05-04 Verfahren zum unterstützten abheben für flugzeuge

Country Status (11)

Country Link
US (1) US8014910B2 (de)
EP (1) EP1880259B1 (de)
JP (1) JP4932830B2 (de)
CN (1) CN100501625C (de)
AT (1) ATE406606T1 (de)
BR (1) BRPI0613368A2 (de)
CA (1) CA2607265C (de)
DE (1) DE602006002511D1 (de)
FR (1) FR2885706B1 (de)
RU (1) RU2359867C1 (de)
WO (1) WO2006120321A2 (de)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2942612B1 (fr) * 2009-03-02 2012-09-28 Airbus France Procede et dispositif d'optimisation automatique au sol de la configuration aerodynamique d'un avion
ES2350544B1 (es) * 2009-03-12 2012-05-16 Airbus Operations, S.L. Sistema de aumento de controlabilidad para una aeronave.
DE102009022602A1 (de) * 2009-05-26 2010-12-02 Airbus Deutschland Gmbh Flugzeug mit einem Hochauftriebssystem
FR2973840B1 (fr) * 2011-04-07 2015-09-18 Airbus Operations Sas Procede et dispositif pour la commande du regime des moteurs d'un aeronef au cours d'une phase de decollage.
CN102229357B (zh) * 2011-05-12 2013-07-03 北京航空航天大学 具有安装角可调节平尾的尾翼
US9529010B2 (en) * 2013-06-17 2016-12-27 Honeywell International Inc. Flight deck display systems and methods for visually indicating low speed change conditions during takeoff and landing
GB2516916B (en) * 2013-08-06 2016-09-14 Lacsop Ltd Method and apparatus for determining the mass of a body
US9878776B2 (en) * 2014-05-15 2018-01-30 The Boeing Company System and method for optimizing horizontal tail loads
US9506945B2 (en) 2014-06-10 2016-11-29 Sikorsky Aircraft Corporation Rotorcraft flight parameter estimation
EP3363731B1 (de) 2015-09-02 2021-06-30 Jetoptera, Inc. Ejektor- und airfoil-konfigurationen
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
US11001378B2 (en) 2016-08-08 2021-05-11 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
WO2017187300A1 (en) * 2016-04-25 2017-11-02 Bombardier Inc. Aircraft pitch control system with electronically geared elevator
FR3052251B1 (fr) * 2016-06-03 2018-05-18 Airbus Operations (S.A.S.) Procede d'optimisation des parametres de decollage d'un aeronef
US11226639B2 (en) * 2016-09-23 2022-01-18 Yaborã Indústria Aeronáutica S.A. Enhanced take-off system
US10479481B2 (en) * 2016-09-28 2019-11-19 The Boeing Company Process and machine for reducing a drag component of a horizontal stabilizer on an aircraft
CN111727312B (zh) 2017-06-27 2023-07-14 杰拓普特拉股份有限公司 航空飞行器垂直起降系统的配置
US10816998B2 (en) * 2017-09-18 2020-10-27 The Boeing Company Airplane takeoff trims utilizing both stabilizers and elevators
EP3489140B1 (de) * 2017-11-27 2022-02-23 Airbus Operations, S.L. Flugzeugsystem mit unterstütztem rollen, starten und steigflug
US11046418B2 (en) * 2018-09-25 2021-06-29 The Boeing Company Articulated empennage with ruddervator
US11292579B2 (en) 2018-09-25 2022-04-05 The Boeing Company Articulated empennage with rudder and elevator
CN110069070B (zh) * 2019-05-08 2022-01-18 成都高威节能科技有限公司 一种提高大型飞机起飞过程安全性的方法
US20210405658A1 (en) * 2020-06-25 2021-12-30 Embraer S.A. Longitudinal trim control movement during takeoff rotation
RU2761687C1 (ru) * 2021-05-20 2021-12-13 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Способ управления самолётом при выводе на большие углы атаки
CN117690332B (zh) * 2024-02-02 2024-04-26 北京东方瑞丰航空技术有限公司 一种操纵指引方法、装置、设备及介质

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3522729A (en) * 1968-01-22 1970-08-04 Sperry Rand Corp Airspeed command system
US4261533A (en) * 1978-06-26 1981-04-14 Dynamic Engineering, Inc. All-axis control of aircraft in ultra deep stall
US4825375A (en) * 1985-12-23 1989-04-25 Boeing Company Apparatus and methods for apportioning commands between aircraft flight control surfaces
FR2609546B1 (fr) * 1987-01-08 1991-01-04 Aerospatiale Procede et systeme pour la determination de la position longitudinale du centre de gravite d'un aeronef pourvu d'un empennage horizontal reglable
FR2609545B1 (fr) * 1987-01-08 1991-01-04 Aerospatiale Procede et systeme pour la determination de la position longitudinale du centre de gravite d'un aeronef pourvu d'un empennage horizontal reglable et application a la surveillance dudit centre de gravite au voisinage du foyer de l'aeronef
US5722620A (en) * 1995-05-15 1998-03-03 The Boeing Company Aircraft pitch-axis stability and command augmentation
FR2817535B1 (fr) 2000-12-06 2003-03-21 Eads Airbus Sa Systeme pour commander automatiquement des dispositifs hypersustentateurs d'un aeronef durant le decollage
FR2826469B1 (fr) * 2001-06-25 2003-10-24 Eads Airbus Sa Procede et dispositif pour commander au moins une surface aerodynamique de profondeur d'un avion lors d'un decollage
FR2864023B1 (fr) * 2003-12-19 2006-03-03 Airbus France Procede pour ameliorer la manoeuvrabilite d'un aeronef lors d'une ressource.
FR2865999B1 (fr) * 2004-02-06 2006-04-07 Airbus France Procede pour ameliorer l'atterrissage d'un aeronef.
FR2868852B1 (fr) * 2004-04-09 2006-06-30 Airbus France Sas Procede pour assurer la securite d'un aeronef volant horizontalement a faible vitesse
FR2869588B1 (fr) * 2004-04-28 2006-07-14 Airbus France Sas Procede d'aide au decollage d'un aeronef.
ES2300184B1 (es) * 2006-04-28 2009-05-01 Airbus España, S.L. Disposicion para acoplar un pivote de acoplamiento para un estabilizador horizontal trimable al fuselaje de cola de una aeronave.
US7764201B2 (en) * 2008-11-26 2010-07-27 Red Hat, Inc. Table management for LZW with fixed-size tables

Also Published As

Publication number Publication date
EP1880259A2 (de) 2008-01-23
FR2885706A1 (fr) 2006-11-17
CN100501625C (zh) 2009-06-17
RU2359867C1 (ru) 2009-06-27
BRPI0613368A2 (pt) 2011-01-11
FR2885706B1 (fr) 2007-06-15
CA2607265C (fr) 2013-10-22
DE602006002511D1 (de) 2008-10-09
CN101171557A (zh) 2008-04-30
WO2006120321A2 (fr) 2006-11-16
CA2607265A1 (fr) 2006-11-16
WO2006120321A3 (fr) 2007-02-22
JP4932830B2 (ja) 2012-05-16
JP2008540229A (ja) 2008-11-20
US8014910B2 (en) 2011-09-06
US20080188999A1 (en) 2008-08-07
EP1880259B1 (de) 2008-08-27

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