ATE394725T1 - Modenunterdrückung in einem flugzeug - Google Patents

Modenunterdrückung in einem flugzeug

Info

Publication number
ATE394725T1
ATE394725T1 AT05251504T AT05251504T ATE394725T1 AT E394725 T1 ATE394725 T1 AT E394725T1 AT 05251504 T AT05251504 T AT 05251504T AT 05251504 T AT05251504 T AT 05251504T AT E394725 T1 ATE394725 T1 AT E394725T1
Authority
AT
Austria
Prior art keywords
modes
aircraft
excitation
suppress
suppression
Prior art date
Application number
AT05251504T
Other languages
English (en)
Inventor
Alessandro Riccardo B Giazotto
Original Assignee
Airbus Uk Ltd
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
Priority claimed from GBGB0405613.1A external-priority patent/GB0405613D0/en
Application filed by Airbus Uk Ltd filed Critical Airbus Uk Ltd
Application granted granted Critical
Publication of ATE394725T1 publication Critical patent/ATE394725T1/de

Links

Classifications

    • 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
    • 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
    • B64C25/505—Shimmy damping
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/50—Navigation or guidance aids
    • G08G5/52—Navigation or guidance aids for take-off
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/50—Navigation or guidance aids
    • G08G5/55—Navigation or guidance aids for a single aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Regulating Braking Force (AREA)
  • Optical Radar Systems And Details Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Electrochromic Elements, Electrophoresis, Or Variable Reflection Or Absorption Elements (AREA)
AT05251504T 2004-03-12 2005-03-11 Modenunterdrückung in einem flugzeug ATE394725T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0405613.1A GB0405613D0 (en) 2004-03-12 2004-03-12 Aircraft mode suppression
GB0421231A GB2411969A (en) 2004-03-12 2004-09-23 A system for control of an aircraft during breaking by reducing excitation of the aircraft modes

Publications (1)

Publication Number Publication Date
ATE394725T1 true ATE394725T1 (de) 2008-05-15

Family

ID=34828677

Family Applications (1)

Application Number Title Priority Date Filing Date
AT05251504T ATE394725T1 (de) 2004-03-12 2005-03-11 Modenunterdrückung in einem flugzeug

Country Status (4)

Country Link
US (1) US7357357B2 (de)
EP (1) EP1574923B1 (de)
AT (1) ATE394725T1 (de)
DE (1) DE602005006451D1 (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2889162B1 (fr) * 2005-07-28 2007-09-07 Airbus France Sas Procede et dispositif de pilotage d'un aeronef selon au moins un axe de pilotage
GB2435246A (en) * 2006-02-17 2007-08-22 Decoma U K Ltd Spoiler
GB0605346D0 (en) * 2006-03-16 2006-04-26 Airbus Uk Ltd Feedback control system
GB0805829D0 (en) 2008-04-01 2008-04-30 Goodrich Actuation Systems Ltd Damping arrangement
US8504221B2 (en) * 2009-01-16 2013-08-06 The Boeing Company Apparatus and method for controlling a control surface of a vehicle based on a load identified on the control surface
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
FR2978423B1 (fr) * 2011-07-28 2014-12-19 Airbus Operations Sas Procede et dispositif de detection de l'embarquement d'une gouverne d'aeronef
RU2532720C1 (ru) * 2013-04-23 2014-11-10 Федеральное государственное унитарное предприятие "Московское опытно-конструкторское бюро "Марс" (ФГУП МОКБ "Марс") Двухканальное устройство координированного управления летательным аппаратом
GB2534915A (en) * 2015-02-05 2016-08-10 Airbus Operations Ltd Method and apparatus for control of a steerable landing gear
GB2540182A (en) 2015-07-08 2017-01-11 Airbus Operations Ltd Aircraft steering system controller
US10210765B2 (en) * 2016-01-11 2019-02-19 The Boeing Company Inference and interpolation of continuous 4D trajectories
GB2554428A (en) * 2016-09-27 2018-04-04 Airbus Operations Ltd Aircraft landing
EP3336485B1 (de) 2016-12-15 2020-09-23 Safran Landing Systems UK Limited Flugzeuganordnung mit ablenkungssensor
KR20220085401A (ko) * 2020-12-15 2022-06-22 현대자동차주식회사 항공 모빌리티의 랜딩기어 제어 시스템 및 제어 방법
CN113566657B (zh) * 2021-07-30 2022-11-01 北京机械设备研究所 一种弹上智能振动控制电动舵机及控制方法
US12337950B2 (en) * 2021-09-29 2025-06-24 Lockheed Martin Corporation Landing gear feedback control system for an aircraft
FR3154703B1 (fr) * 2023-10-25 2025-11-07 Airbus Operations Sas Dispositif et procédé de génération d’un phénomène de flottement sur au moins une partie d’un aéronef.

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2652289C2 (de) * 1976-11-17 1983-02-03 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Automatisches Richtungsstabilisierungssystem
DE3803015A1 (de) * 1988-02-02 1989-08-10 Pfister Gmbh Verfahren und system zum betrieb eines luftfahrzeugs
US5060889A (en) * 1989-05-01 1991-10-29 The Boeing Company Apparatus and methods for maintaining aircraft track angle during an asymmetric flight condition
US5113346A (en) * 1990-01-26 1992-05-12 The Boeing Company Aircraft automatic landing system with engine out provisions
FR2838101B1 (fr) * 2002-04-08 2004-12-17 Airbus France Aeronef a commandes de vol electriques, pourvu d'un fuselage susceptible de se deformer et de vibrer
US6915989B2 (en) * 2002-05-01 2005-07-12 The Boeing Company Aircraft multi-axis modal suppression system

Also Published As

Publication number Publication date
EP1574923B1 (de) 2008-05-07
EP1574923A2 (de) 2005-09-14
DE602005006451D1 (de) 2008-06-19
EP1574923A3 (de) 2006-06-07
US20050234606A1 (en) 2005-10-20
US7357357B2 (en) 2008-04-15

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Legal Events

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