IT1110227B - Dispositivo di comando con controreazione meccanica attiva per il sistema di governo di un aereo - Google Patents

Dispositivo di comando con controreazione meccanica attiva per il sistema di governo di un aereo

Info

Publication number
IT1110227B
IT1110227B IT20458/79A IT2045879A IT1110227B IT 1110227 B IT1110227 B IT 1110227B IT 20458/79 A IT20458/79 A IT 20458/79A IT 2045879 A IT2045879 A IT 2045879A IT 1110227 B IT1110227 B IT 1110227B
Authority
IT
Italy
Prior art keywords
controration
aircraft
mechanical
active
command device
Prior art date
Application number
IT20458/79A
Other languages
English (en)
Other versions
IT7920458A0 (it
Original Assignee
Messerschmitt Boelkow Blohm
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 Messerschmitt Boelkow Blohm filed Critical Messerschmitt Boelkow Blohm
Publication of IT7920458A0 publication Critical patent/IT7920458A0/it
Application granted granted Critical
Publication of IT1110227B publication Critical patent/IT1110227B/it

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
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/507—Transmitting means with power amplification using electrical energy with artificial feel
    • 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
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/503—Fly-by-Wire
    • 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
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Control Devices (AREA)
  • Feedback Control In General (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Toys (AREA)
IT20458/79A 1978-02-24 1979-02-23 Dispositivo di comando con controreazione meccanica attiva per il sistema di governo di un aereo IT1110227B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2807902A DE2807902C2 (de) 1978-02-24 1978-02-24 Steuereinrichtung mit aktiver Kraft rückführung

Publications (2)

Publication Number Publication Date
IT7920458A0 IT7920458A0 (it) 1979-02-23
IT1110227B true IT1110227B (it) 1985-12-23

Family

ID=6032796

Family Applications (1)

Application Number Title Priority Date Filing Date
IT20458/79A IT1110227B (it) 1978-02-24 1979-02-23 Dispositivo di comando con controreazione meccanica attiva per il sistema di governo di un aereo

Country Status (7)

Country Link
US (1) US4236685A (it)
JP (1) JPS54122598A (it)
CA (1) CA1118516A (it)
DE (1) DE2807902C2 (it)
FR (1) FR2418152A1 (it)
GB (1) GB2014917B (it)
IT (1) IT1110227B (it)

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US4642774A (en) * 1982-07-01 1987-02-10 Rockwell International Corporation Automatic flight control with pilot fly-through
US4477043A (en) * 1982-12-15 1984-10-16 The United States Of America As Represented By The Secretary Of The Air Force Biodynamic resistant control stick
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SE442851B (sv) * 1983-04-18 1986-02-03 Saab Scania Ab Forfarande och anordning vid styrsystem
US4527653A (en) * 1984-01-23 1985-07-09 General Motors Corporation Road load insensitive electric power steering system
DE3416969A1 (de) * 1984-05-08 1985-11-14 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Verfahren und vorrichtung zur steuerkraftstabilisierung bei einem drehfluegelflugzeug
US4849900A (en) * 1986-05-02 1989-07-18 The Boeing Company Flight control system and method
FR2604001B1 (fr) * 1986-09-15 1988-12-09 Aerospatiale Systeme de commande de vol electrique avec protection en incidence pour aeronef
FR2617120B1 (fr) * 1987-06-24 1989-12-08 Aerospatiale Systeme pour la commande d'un aeronef en roulis et en lacet
SE8800848D0 (sv) * 1988-03-10 1988-03-10 Saab Scania Ab Sett och anordning for att overvaka en fordonsforares styrbeteende
US5012423A (en) * 1989-04-17 1991-04-30 Mcdonnell Douglas Corporation Back-up fly by wire control system
US5076517A (en) * 1989-08-14 1991-12-31 United Technologies Corporation Programmable, linear collective control system for a helicopter
US5107080A (en) * 1989-12-01 1992-04-21 Massachusetts Institute Of Technology Multiple degree of freedom damped hand controls
US5209661A (en) * 1990-10-29 1993-05-11 Systems Control Technology, Inc. Motor control desired dynamic load of a simulating system and method
US5255880A (en) * 1991-02-08 1993-10-26 Rockwell International Corporation Fly by wire/fly by light control system with manual override
US5197697A (en) * 1991-02-08 1993-03-30 Rockwell International Corporation Fly by wire/fly by light control system with manual override
US5493497A (en) * 1992-06-03 1996-02-20 The Boeing Company Multiaxis redundant fly-by-wire primary flight control system
GB2268467A (en) * 1992-07-07 1994-01-12 Frederick George Wilson Lift.
US5458304A (en) * 1992-08-26 1995-10-17 Gilbert; Raymond D. Disk spoiler system
US5347204A (en) * 1992-10-06 1994-09-13 Honeywell Inc. Position dependent rate dampening in any active hand controller
US5264768A (en) * 1992-10-06 1993-11-23 Honeywell, Inc. Active hand controller feedback loop
DE69425654T2 (de) * 1993-05-06 2000-12-28 Northrop Grumman Corp., Los Angeles Gerät und verfahren zur veränderung der form einer struktur
AU2316695A (en) * 1994-04-29 1995-11-29 Lodge Flying Ltd. Stabilisation of radio controlled aircraft
US5489830A (en) * 1994-09-09 1996-02-06 Mcdonnell Douglas Corporation Control system with loadfeel and backdrive
US5826834A (en) * 1994-10-19 1998-10-27 Honeywell Inc. Self adaptive limiter for automatic control of approach and landing
US5797564A (en) * 1995-05-15 1998-08-25 The Boeing Company System for backdrive of flight deck controls during autopilot operation
JPH0924898A (ja) * 1995-07-12 1997-01-28 Teijin Seiki Co Ltd 小型航空機の操縦装置
US6062513A (en) * 1998-09-14 2000-05-16 The Boeing Company Total energy based flight control system
FR2789500B1 (fr) * 1999-02-04 2001-03-30 Aerospatiale Systeme pour la commande en lacet d'un aeronef
IL143255A (en) 2001-05-20 2015-09-24 Simbionix Ltd Endoscopic ultrasonography simulation
US6711476B2 (en) * 2001-09-27 2004-03-23 The Boeing Company Method and computer program product for estimating at least one state of a dynamic system
US20030183728A1 (en) * 2002-03-29 2003-10-02 The Boeing Company Aircraft control surface controller and associated method
DE10249967B4 (de) * 2002-10-26 2006-03-09 Airbus Deutschland Gmbh Vorrichtung zur Ansteuerung der Vorflügel und Landeklappen eines Flugzeuges
FR2847352B1 (fr) * 2002-11-18 2005-01-28 Airbus France Systeme de commandes de vol electriques pour aeronef comportant une detection de couplages oscillatoires de pilotage et organe de pilotage pour un tel systeme
CA2515775A1 (en) 2003-02-15 2004-09-02 Gulfstream Aerospace Corporation System and method for aircraft cabin atmospheric composition control
US7850456B2 (en) 2003-07-15 2010-12-14 Simbionix Ltd. Surgical simulation device, system and method
US7285932B2 (en) * 2003-10-28 2007-10-23 United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method and apparatus for loss of control inhibitor systems
US7272473B2 (en) * 2004-09-17 2007-09-18 The Boeing Company Methods and systems for analyzing system operator coupling susceptibility
BRPI0706593A2 (pt) * 2006-01-17 2011-04-05 Gulfstream Aerospace Corp sistema e método para um sistema de controle de backup integrado
JP2009523658A (ja) 2006-01-17 2009-06-25 ガルフストリーム・エアロスペース・コーポレイション 分散型飛行制御システムのバックアップ制御のための装置及び方法
US8380364B2 (en) 2006-05-17 2013-02-19 Textron Innovations, Inc. Manual and computerized flight control system with natural feedback
US9340278B2 (en) 2006-05-17 2016-05-17 Textron Innovations, Inc. Flight control system
US8401716B2 (en) * 2006-05-17 2013-03-19 Textron Innovations Inc. Flight control systems
US8725321B2 (en) * 2006-05-17 2014-05-13 Textron Innovations Inc. Flight control system
US7750593B2 (en) * 2006-10-26 2010-07-06 Honeywell International Inc. Active human-machine interface system without a force sensor
WO2008087629A2 (en) 2007-01-16 2008-07-24 Simbionix Ltd. Preoperative surgical simulation
US8543338B2 (en) 2007-01-16 2013-09-24 Simbionix Ltd. System and method for performing computerized simulations for image-guided procedures using a patient specific model
ES2378007B1 (es) * 2009-02-12 2013-01-31 Eads Construcciones Aeronáuticas, S.A. Conjunto de control y mando para aeronave.
DE102010035822A1 (de) * 2010-08-30 2012-03-01 Liebherr-Aerospace Lindenberg Gmbh Steuersystem für ein Luftfahrzeug
US8494690B2 (en) * 2011-04-26 2013-07-23 The Boeing Company Flight controller management system with a backdrive monitor
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
ES2913951T3 (es) * 2013-07-16 2022-06-06 Tactilair Ltd Sistema de retroalimentación para un miembro de control de vuelo de una aeronave
US10196131B2 (en) * 2016-02-16 2019-02-05 The Boeing Company Hydraulic system and method for an aircraft flight control system
WO2018156618A1 (en) * 2017-02-21 2018-08-30 Configurable Controls, Llc Motion control system for foot-actuated flight controller
US11524767B2 (en) 2021-03-31 2022-12-13 Beta Air, Llc Methods and systems for flight control configured for use in an electric aircraft

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DE1082128B (de) * 1958-06-23 1960-05-19 Sperry Gyroscope Co Ltd Flugzeugsteuereinrichtung fuer schnelle Wendungen
US3005606A (en) * 1959-09-17 1961-10-24 English Electric Co Ltd Aircraft manoeuvre boost control systems
US3033496A (en) * 1959-09-23 1962-05-08 Honeywell Regulator Co Control apparatus
US3493826A (en) * 1965-09-13 1970-02-03 Honeywell Inc Servomechanism including a lead network feedback and means to modify the lead network responsive to rate
US3450375A (en) * 1967-02-02 1969-06-17 Bertea Corp Load feel computer
US3476335A (en) * 1967-05-19 1969-11-04 Sperry Rand Corp Pseudo control stick steering system for aircraft having a damper system
US3520499A (en) * 1968-05-29 1970-07-14 United Aircraft Corp Flight control system
US3659173A (en) * 1970-06-19 1972-04-25 Bendix Corp Aircraft control system including limiting means
US4095763A (en) * 1977-02-25 1978-06-20 Textron, Inc. Fail safe augmentation system

Also Published As

Publication number Publication date
FR2418152B1 (it) 1983-06-17
JPS54122598A (en) 1979-09-22
CA1118516A (en) 1982-02-16
US4236685A (en) 1980-12-02
DE2807902C2 (de) 1980-04-30
GB2014917B (en) 1982-05-06
IT7920458A0 (it) 1979-02-23
DE2807902B1 (de) 1979-08-23
FR2418152A1 (fr) 1979-09-21
GB2014917A (en) 1979-09-05

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