ATE303627T1 - Fly-by-wire gesteuertes flugzeug mit einem flexiblen, schwingungsfähigen rumpf - Google Patents

Fly-by-wire gesteuertes flugzeug mit einem flexiblen, schwingungsfähigen rumpf

Info

Publication number
ATE303627T1
ATE303627T1 AT03290076T AT03290076T ATE303627T1 AT E303627 T1 ATE303627 T1 AT E303627T1 AT 03290076 T AT03290076 T AT 03290076T AT 03290076 T AT03290076 T AT 03290076T AT E303627 T1 ATE303627 T1 AT E303627T1
Authority
AT
Austria
Prior art keywords
fly
flexible
controlled aircraft
wire controlled
vibrating
Prior art date
Application number
AT03290076T
Other languages
English (en)
Inventor
Francois Kubica
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 ATE303627T1 publication Critical patent/ATE303627T1/de

Links

Classifications

    • 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
    • G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/166—Mechanical, construction or arrangement details of inertial navigation systems
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Navigation (AREA)
  • Vibration Prevention Devices (AREA)
  • Details Of Aerials (AREA)
  • Toys (AREA)
  • Agricultural Chemicals And Associated Chemicals (AREA)
AT03290076T 2002-04-08 2003-01-13 Fly-by-wire gesteuertes flugzeug mit einem flexiblen, schwingungsfähigen rumpf ATE303627T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0204334A FR2838101B1 (fr) 2002-04-08 2002-04-08 Aeronef a commandes de vol electriques, pourvu d'un fuselage susceptible de se deformer et de vibrer

Publications (1)

Publication Number Publication Date
ATE303627T1 true ATE303627T1 (de) 2005-09-15

Family

ID=28052182

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03290076T ATE303627T1 (de) 2002-04-08 2003-01-13 Fly-by-wire gesteuertes flugzeug mit einem flexiblen, schwingungsfähigen rumpf

Country Status (7)

Country Link
US (3) US6669139B2 (de)
EP (1) EP1353253B1 (de)
AT (1) ATE303627T1 (de)
CA (1) CA2418228C (de)
DE (1) DE60301428T2 (de)
ES (1) ES2248709T3 (de)
FR (1) FR2838101B1 (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
FR2853094B1 (fr) * 2003-03-26 2005-05-27 Airbus France Procede pour contrer les vibrations induites dans un aeronef par le fonctionnement en moulinet d'une soufflante et systeme de commandes de vol electriques mettant en oeuvre ce procede
EP2146263B1 (de) * 2003-11-03 2019-05-08 The Boeing Company Mehrachsiges Modenunterdrückungssystem für Luftfahrzeug
FR2864026B1 (fr) * 2003-12-23 2007-01-19 Eurocopter France Procede et dispositif pour reduire par une derive orientable les vibrations engendrees sur le fuselage d'un helicoptere
FR2864025B1 (fr) * 2003-12-23 2007-01-12 Eurocopter France Procede et dispositif pour reduire par un empennage orientable les vibrations engendrees sur le fuselage d'un helicoptere
US7424989B2 (en) 2004-03-11 2008-09-16 The Boeing Company Intelligent multifunctional actuation system for vibration and buffet suppression
ATE394725T1 (de) * 2004-03-12 2008-05-15 Airbus Uk Ltd Modenunterdrückung in einem flugzeug
US20060255206A1 (en) * 2005-04-18 2006-11-16 Jolly Mark R Method and aircraft system for active suppression of aircraft low frequency aerostructure lateral bending modes
US7367530B2 (en) 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
FR2899561B1 (fr) * 2006-04-11 2008-05-16 Airbus France Sas Procede et dispostif de pilotage d'un aeronef autour d'un axe de pilotage
US7689473B2 (en) * 2008-03-19 2010-03-30 Ashdan Llc Method for generating a shopping list using virtual merchandising options
JP5595978B2 (ja) * 2011-05-28 2014-09-24 双葉電子工業株式会社 遠隔制御機器の駆動制御装置
US8620492B2 (en) * 2012-02-27 2013-12-31 Textron Innovations Inc. Yaw damping system and method for aircraft
US8874286B2 (en) 2012-02-27 2014-10-28 Textron Innovations, Inc. Yaw damping system and method for aircraft
CN104501802A (zh) * 2015-01-09 2015-04-08 中国人民解放军63961部队 一种用于高速飞行器对地目标捕获、识别方法
CN105467158B (zh) * 2015-12-28 2019-01-29 太原航空仪表有限公司 直升机机动飞行的空速修正方法
US10919617B2 (en) * 2016-10-21 2021-02-16 Aurora Flight Sciences Corporation Distributed acceleration sensing for robust disturbance rejection
CN116661331B (zh) * 2023-08-02 2023-09-26 成都正扬博创电子技术有限公司 一种利用软硬件协同的多余度飞控计算机系统

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2487793A (en) * 1946-12-18 1949-11-15 Sperry Corp Object controlling electric motor system
US2985409A (en) * 1955-09-26 1961-05-23 North American Aviation Inc Gust alleviation system
US3079108A (en) * 1960-09-14 1963-02-26 Honeywell Regulator Co Control apparatus
US3241077A (en) * 1961-07-06 1966-03-15 North American Aviation Inc Self-adaptive control system eliminating variable unwanted component
US3279725A (en) * 1963-12-11 1966-10-18 North American Aviation Inc Flight controller for flexible vehicles
US3549108A (en) * 1968-03-25 1970-12-22 Honeywell Inc Control apparatus
US4171115A (en) * 1977-12-12 1979-10-16 Sperry Rand Corporation Stability augmentation system for relaxed static stability aircraft
US4280188A (en) * 1978-10-11 1981-07-21 Grumman Aerospace Corporation Survivable redundant vector sensors for systems with differing maximum output requirements
FR2531676A1 (fr) * 1982-08-11 1984-02-17 Onera (Off Nat Aerospatiale) Procede et installation de reduction du tremblement de la voilure d'un aeronef au moyen de gouvernes actives
US5072893A (en) * 1987-05-28 1991-12-17 The Boeing Company Aircraft modal suppression system
FR2617120B1 (fr) * 1987-06-24 1989-12-08 Aerospatiale Systeme pour la commande d'un aeronef en roulis et en lacet
FR2672028B1 (fr) * 1991-01-29 1993-05-14 Aerospatiale Systeme permettant d'ameliorer le comportement en flottement d'un aeronef.
US5654906A (en) * 1995-07-06 1997-08-05 Youngquist; John S. Rate gyro error correction and use as heading source
DE19841632C2 (de) * 1998-09-11 2001-06-07 Daimler Chrysler Ag Verfahren zum Kompensieren von Strukturschwingungen eines Flugzeugs aufgrund von äußeren Störungen
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
US20040155156A1 (en) 2004-08-12
DE60301428D1 (de) 2005-10-06
CA2418228A1 (fr) 2003-10-08
EP1353253A1 (de) 2003-10-15
US20040155155A1 (en) 2004-08-12
FR2838101A1 (fr) 2003-10-10
ES2248709T3 (es) 2006-03-16
CA2418228C (fr) 2010-08-17
US6976656B2 (en) 2005-12-20
US20030189129A1 (en) 2003-10-09
US6986483B2 (en) 2006-01-17
EP1353253B1 (de) 2005-08-31
DE60301428T2 (de) 2006-06-08
FR2838101B1 (fr) 2004-12-17
US6669139B2 (en) 2003-12-30

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Legal Events

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