ES2037854T3 - Sistema para el accionamiento de un aeronave en balanceo lateral y en vaiven horizontal lateral. - Google Patents

Sistema para el accionamiento de un aeronave en balanceo lateral y en vaiven horizontal lateral.

Info

Publication number
ES2037854T3
ES2037854T3 ES198888401530T ES88401530T ES2037854T3 ES 2037854 T3 ES2037854 T3 ES 2037854T3 ES 198888401530 T ES198888401530 T ES 198888401530T ES 88401530 T ES88401530 T ES 88401530T ES 2037854 T3 ES2037854 T3 ES 2037854T3
Authority
ES
Spain
Prior art keywords
electrical
electrical signals
order
organ
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.)
Expired - Lifetime
Application number
ES198888401530T
Other languages
English (en)
Inventor
Jacques Farineau.
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 Group SAS
Original Assignee
Airbus Group 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 Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2037854T3 publication Critical patent/ES2037854T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • 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)
  • 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)
  • Harvester Elements (AREA)

Abstract

SEGUN EL INVENTO, ESTE SISTEMA TIENE: - UN DISPOSITIVO (16) SUSCEPTIBLE DE ELABORAR A PARTIR DE LAS SEÑALES ELECTRICAS RESPECTIVAMENTE REPRESENTATIVAS DE LA POSICION DE UN PRIMER ORGANO DE ACCIONAMIENTO VOLUNTARIO (14) DE LA VELOCIDAD DE GIRO, DE LA SUSTENTACION, DE LA VELOCIDAD DE CABECEO, DEL DESLIZAMIENTO LATERAL Y DE LA POSICION DE UN SEGUNDO ORGANO DE ACCIONAMIENTO VOLUNTARIO (15); - UNA ORDEN ELECTRICA UNICA DE MANDO EN GIRO FORMADA POR UNA COMBINACION LINEAL DE DICHAS SEÑALES ELECTRICAS; - UN DISPOSITIVO (18) SUSCEPTIBLE DE ELABORAR, A PARTIR DE DICHAS SEÑALES ELECTRICAS, UNA ORDEN ELECTRICA DE MANDO EN CABECEO FORMADA POR UNA COMBINACION LINEAL DE DICHAS SEÑALES ELECTRICAS; Y UN DISPOSITIVO (23) QUE PERMITE COMBINAR DICHA ORDEN ELECTRICA DE MANDO EN CABECEO Y UNA ORDEN MECANICA QUE PROVIENE DIRECTAMENTE DE DICHO SEGUNDO ORGANO (15) DE ACCIONAMIENTO VOLUNTARIO.
ES198888401530T 1987-06-24 1988-06-20 Sistema para el accionamiento de un aeronave en balanceo lateral y en vaiven horizontal lateral. Expired - Lifetime ES2037854T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8708870A FR2617120B1 (fr) 1987-06-24 1987-06-24 Systeme pour la commande d'un aeronef en roulis et en lacet

Publications (1)

Publication Number Publication Date
ES2037854T3 true ES2037854T3 (es) 1993-07-01

Family

ID=9352447

Family Applications (1)

Application Number Title Priority Date Filing Date
ES198888401530T Expired - Lifetime ES2037854T3 (es) 1987-06-24 1988-06-20 Sistema para el accionamiento de un aeronave en balanceo lateral y en vaiven horizontal lateral.

Country Status (8)

Country Link
US (1) US4964599A (es)
EP (1) EP0296951B1 (es)
JP (1) JPH01503697A (es)
CA (1) CA1295038C (es)
DE (1) DE3877066T2 (es)
ES (1) ES2037854T3 (es)
FR (1) FR2617120B1 (es)
WO (1) WO1988010458A1 (es)

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FR2668750B1 (fr) * 1990-11-06 1993-01-22 Aerospatiale Systeme pour la commande integree en profondeur et en poussee d'un aeronef.
US5588620A (en) * 1992-08-26 1996-12-31 Gilbert; Raymond D. Radial-force spoiler system
US5458304A (en) * 1992-08-26 1995-10-17 Gilbert; Raymond D. Disk spoiler system
US5564656A (en) * 1994-08-29 1996-10-15 Gilbert; Raymond D. Segmented spoilers
US6206329B1 (en) * 1995-09-15 2001-03-27 Jean-Pierre Gautier Process and device for the control of the rudder of an aircraft
US5806806A (en) * 1996-03-04 1998-09-15 Mcdonnell Douglas Corporation Flight control mechanical backup system
US5839697A (en) * 1996-05-14 1998-11-24 The Boeing Company Method and apparatus for turn coordination gain as a function of flap position
US6260796B1 (en) * 1997-03-04 2001-07-17 Wallace Neil Klingensmith Multi-thrustered hover craft
US5899415A (en) * 1997-03-14 1999-05-04 Conway; Robert Personnel guided aerial delivery device
US6061611A (en) * 1998-01-06 2000-05-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Closed-form integrator for the quaternion (euler angle) kinematics equations
US6126111A (en) * 1998-07-08 2000-10-03 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Emergency flight control system using one engine and fuel transfer
FR2789500B1 (fr) * 1999-02-04 2001-03-30 Aerospatiale Systeme pour la commande en lacet d'un aeronef
FR2806791B1 (fr) * 2000-03-23 2002-05-31 Aerospatiale Matra Airbus Procede pour determiner une vitesse minimale de controle d'un aeronef
KR100589983B1 (ko) * 2000-04-14 2006-06-15 한국항공우주산업 주식회사 항공기의 가로방향 제어 시스템
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
FR2850356B1 (fr) * 2003-01-28 2005-03-18 Airbus France Systeme de controle du regime d'au moins un moteur d'un aeronef
DE10313728B4 (de) * 2003-03-27 2011-07-21 Airbus Operations GmbH, 21129 Klappensystem am Tragflügel eines Starrflügel-Flugzeuges
US6923405B2 (en) * 2003-11-17 2005-08-02 The Boeing Company Enhanced rudder control system
DE10361891A1 (de) * 2003-12-23 2005-08-04 Airbus Deutschland Gmbh Vorrichtung zur Ansteuerung und Verstellung von Klappen an Flugzeugtragflächen
WO2007001369A2 (en) * 2004-09-17 2007-01-04 Aurora Flight Sciences System and method for controlling engine rpm of a ducted fan aircraft
WO2007001372A2 (en) 2004-09-17 2007-01-04 Aurora Flight Sciences Ducted spinner for engine cooling
WO2006137869A2 (en) * 2004-09-17 2006-12-28 Aurora Flight Sciences System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft
WO2007001373A2 (en) * 2004-09-17 2007-01-04 Aurora Flight Sciences Inbound transition control for a trail-sitting vertical take off and landing aircraft
WO2007001371A2 (en) * 2004-09-17 2007-01-04 Aurora Flight Sciences Vibration isolation engine mount system and method for ducted fan aircraft
WO2007005040A2 (en) * 2004-09-17 2007-01-11 Aurora Flight Sciences Adaptive landing gear
DE102004047008A1 (de) * 2004-09-28 2006-03-30 Liebherr-Aerospace Lindenberg Gmbh Vorrichtung zur Einstellung von Flugzeughöhenflossen
US7607611B2 (en) * 2005-05-11 2009-10-27 Honeywell International Inc. Flight control surface actuation system with redundantly configured and lockable actuator assemblies
US7556224B2 (en) * 2005-12-27 2009-07-07 Honeywell International Inc. Distributed flight control surface actuation system
FR2897592B1 (fr) * 2006-02-20 2008-04-04 Airbus France Sas Procede et dispositif de detection d'une dissymetrie laterale d'un aeronef.
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
US8401716B2 (en) * 2006-05-17 2013-03-19 Textron Innovations Inc. Flight control systems
US9340278B2 (en) 2006-05-17 2016-05-17 Textron Innovations, Inc. Flight control system
US8725321B2 (en) * 2006-05-17 2014-05-13 Textron Innovations Inc. Flight control system
US8380364B2 (en) * 2006-05-17 2013-02-19 Textron Innovations, Inc. Manual and computerized flight control system with natural feedback
FR2912242B1 (fr) 2007-02-07 2009-03-13 Airbus France Sas Dispositif et procede d'aide a la gestion d'une panne moteur d'un aeronef
FR2912243B1 (fr) 2007-02-07 2009-03-13 Airbus France Sas Dispositif et procede d'aide a la gestion d'une panne moteur d'un aeronef
FR2914075B1 (fr) 2007-03-22 2009-04-24 Airbus France Sas Procede et dispositif de limitation de la commande de roulis d'un aeronef en fonction d'une dissymetrie de poussee
FR2922301B1 (fr) 2007-10-11 2010-02-26 Airbus Dispositif et procede d'estimation d'un angle de derapage d'un aeronef
FR2927427B1 (fr) * 2008-02-11 2014-12-12 Airbus France Procede et dispositif pour attenuer sur un aeronef des effets lateraux engendres par une turbulence.
FR2945514B1 (fr) * 2009-05-18 2012-09-28 Airbus France Procede et dispositif pour detecter automatiquement une dissymetrie laterale d'un aeronef
FR2945513B1 (fr) * 2009-05-18 2013-02-08 Airbus France Procede et dispositif d'optimisation des performances d'un aeronef en presence d'une dissymetrie laterale
FR2947242B1 (fr) * 2009-06-24 2013-02-22 Airbus Procede et dispositif d'equilibrage lateral en vol d'un avion
CN102141468B (zh) * 2010-12-20 2013-05-01 中国商用飞机有限责任公司 一种二自由度操纵杆驱动试验装置及其控制方法
FR2981045B1 (fr) 2011-10-10 2013-10-25 Eurocopter France Systeme de pilotage en lacet pour giravion, mettant en oeuvre un organe entraine par l'homme qui genere des commandes de vol par objectif
US8874286B2 (en) 2012-02-27 2014-10-28 Textron Innovations, Inc. Yaw damping system and method for aircraft
US8620492B2 (en) 2012-02-27 2013-12-31 Textron Innovations Inc. Yaw damping system and method for aircraft
WO2015065551A1 (en) * 2013-07-25 2015-05-07 Lam Aviation, Inc. Aircraft wing structure and control system
CN109716254B (zh) * 2016-06-21 2022-08-19 庞巴迪公司 用于踏板到翻滚耦合的控制律
US10144504B1 (en) * 2017-09-01 2018-12-04 Kitty Hawk Corporation Decoupled hand controls for aircraft with vertical takeoff and landing and forward flight capabilities

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FR1018086A (fr) * 1949-05-07 1952-12-26 Sperry Corp Installation de commande automatique du vol pour avions
US2953329A (en) * 1956-08-30 1960-09-20 Honeywell Regulator Co Automatic control apparatus for aircraft
US3512737A (en) * 1968-07-01 1970-05-19 Bendix Corp Aircraft control system including means for adjusting flight condition signal gain
US3730461A (en) * 1971-05-05 1973-05-01 S Knemeyer Stability augmentation system for light aircraft providing pilot assist and turn
DE2807902C2 (de) * 1978-02-24 1980-04-30 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Steuereinrichtung mit aktiver Kraft rückführung
EP0046875B1 (de) * 1980-09-02 1989-09-20 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Anordnung, insbesondere für Luftfahrzeuge zur Übertragung von Steuersignalen
DE3151623A1 (de) * 1981-12-28 1983-07-07 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Steuereinrichtung zum einstellen von steuerflaechen fuer luftfahrzeuge
US4527242A (en) * 1982-06-28 1985-07-02 Rockwell International Corporation Automatic flight control pilot assist system

Also Published As

Publication number Publication date
US4964599A (en) 1990-10-23
DE3877066T2 (de) 1993-05-19
EP0296951B1 (fr) 1992-12-30
CA1295038C (fr) 1992-01-28
FR2617120A1 (fr) 1988-12-30
DE3877066D1 (de) 1993-02-11
FR2617120B1 (fr) 1989-12-08
EP0296951A1 (fr) 1988-12-28
JPH01503697A (ja) 1989-12-14
WO1988010458A1 (fr) 1988-12-29

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