IT7920458A0 - Controreazione meccanica attiva per dispositivo di comando con il sistema di governo di un aereo. - Google Patents

Controreazione meccanica attiva per dispositivo di comando con il sistema di governo di un aereo.

Info

Publication number
IT7920458A0
IT7920458A0 IT7920458A IT2045879A IT7920458A0 IT 7920458 A0 IT7920458 A0 IT 7920458A0 IT 7920458 A IT7920458 A IT 7920458A IT 2045879 A IT2045879 A IT 2045879A IT 7920458 A0 IT7920458 A0 IT 7920458A0
Authority
IT
Italy
Prior art keywords
aircraft
control device
steering system
mechanical feedback
active mechanical
Prior art date
Application number
IT7920458A
Other languages
English (en)
Other versions
IT1110227B (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

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/38Transmitting means with power amplification
    • B64C13/50Transmitting means with power amplification using electrical energy
    • B64C13/507Transmitting means with power amplification using electrical energy with artificial feel
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/38Transmitting means with power amplification
    • B64C13/50Transmitting means with power amplification using electrical energy
    • B64C13/503Fly-by-Wire
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/0055Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
    • G05D1/0061Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements for transition from automatic pilot to manual pilot and vice versa
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 true IT7920458A0 (it) 1979-02-23
IT1110227B 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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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
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US5347204A (en) * 1992-10-06 1994-09-13 Honeywell Inc. Position dependent rate dampening in any active hand controller
KR960702399A (ko) * 1993-05-06 1996-04-27 제임스, 씨. 존슨 구조형상 제어장치 및 제어방법(apparatus and method for controlling the shape of structures)
ATE175503T1 (de) * 1994-04-29 1999-01-15 Lodge Flying Ltd Stabilisierung eines funkgesteuerten luftfahrzeuges
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
US8015973B2 (en) 2003-02-15 2011-09-13 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
US8725321B2 (en) * 2006-05-17 2014-05-13 Textron Innovations Inc. Flight control system
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
US7750593B2 (en) * 2006-10-26 2010-07-06 Honeywell International Inc. Active human-machine interface system without a force sensor
US8500451B2 (en) 2007-01-16 2013-08-06 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
EP2826707B1 (en) * 2013-07-16 2022-05-11 Tactilair Limited Feedback system for a flying control member of an aircraft
US10196131B2 (en) * 2016-02-16 2019-02-05 The Boeing Company Hydraulic system and method for an aircraft flight control system
US11084571B2 (en) 2017-02-21 2021-08-10 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
IT1110227B (it) 1985-12-23
DE2807902B1 (de) 1979-08-23
GB2014917B (en) 1982-05-06
FR2418152A1 (fr) 1979-09-21
CA1118516A (en) 1982-02-16
US4236685A (en) 1980-12-02
DE2807902C2 (de) 1980-04-30
FR2418152B1 (it) 1983-06-17
GB2014917A (en) 1979-09-05
JPS54122598A (en) 1979-09-22

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