FR2418152A1 - Installation de pilotage d'avion - Google Patents
Installation de pilotage d'avionInfo
- Publication number
- FR2418152A1 FR2418152A1 FR7904695A FR7904695A FR2418152A1 FR 2418152 A1 FR2418152 A1 FR 2418152A1 FR 7904695 A FR7904695 A FR 7904695A FR 7904695 A FR7904695 A FR 7904695A FR 2418152 A1 FR2418152 A1 FR 2418152A1
- Authority
- FR
- France
- Prior art keywords
- piloting
- force
- antagonistic
- control member
- differential signal
- 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.)
- Granted
Links
- 230000003042 antagnostic effect Effects 0.000 abstract 2
- 238000013016 damping Methods 0.000 abstract 2
- 238000009434 installation Methods 0.000 abstract 1
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)
Abstract
Installation de pilotage d'un avion à organe de commande manuelle sur lequel s'exerce une force antagoniste correspondant à l'écart entre l'ordre de pilotage et les conditions du vol. L'organe de commande manuelle 10 est associé à un comparateur 12 formant un signal différentiel à partir de l'ordre de pilotage et du signal de réaction d'un gyroscope. Une unité d'effort et d'amortissement permet d'exercer sur le manche une force antagoniste et/ou d'amortissement en fonction des paramètres du vol et dudit signal différentiel. Application : pilotage d'avions supersoniques.
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 |
---|---|
FR2418152A1 true FR2418152A1 (fr) | 1979-09-21 |
FR2418152B1 FR2418152B1 (fr) | 1983-06-17 |
Family
ID=6032796
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7904695A Granted FR2418152A1 (fr) | 1978-02-24 | 1979-02-23 | Installation de pilotage d'avion |
Country Status (7)
Country | Link |
---|---|
US (1) | US4236685A (fr) |
JP (1) | JPS54122598A (fr) |
CA (1) | CA1118516A (fr) |
DE (1) | DE2807902C2 (fr) |
FR (1) | FR2418152A1 (fr) |
GB (1) | GB2014917B (fr) |
IT (1) | IT1110227B (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2604001A1 (fr) * | 1986-09-15 | 1988-03-18 | Aerospatiale | Systeme de commande de vol electrique avec protection en incidence pour aeronef |
WO1995012152A1 (fr) * | 1992-10-06 | 1995-05-04 | Honeywell Inc. | Boucle d'asservissement de dispositif de commande manuel actif |
Families Citing this family (55)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4398242A (en) * | 1980-02-25 | 1983-08-09 | The Boeing Company | Electronic controller |
US4527242A (en) * | 1982-06-28 | 1985-07-02 | Rockwell International Corporation | Automatic flight control pilot assist system |
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 |
SE442851B (sv) * | 1983-04-18 | 1986-02-03 | Saab Scania Ab | Forfarande och anordning vid styrsystem |
SE442852B (sv) * | 1983-04-18 | 1986-02-03 | Saab Scania Ab | Forfarande och anordning vid styrsystem for att astadkomma forhojd momentgradient for sma manoverdonsrorelser |
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 |
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 |
US5197697A (en) * | 1991-02-08 | 1993-03-30 | Rockwell International Corporation | Fly by wire/fly by light control system with manual override |
US5255880A (en) * | 1991-02-08 | 1993-10-26 | 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 |
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 |
JP4490963B2 (ja) | 2003-02-15 | 2010-06-30 | ガルフストリーム・エアロスペース・コーポレイション | 航空機キャビン大気組成制御方法 |
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 |
EP1977297A4 (fr) * | 2006-01-17 | 2010-02-24 | Gulfstream Aerospace Corp | Appareil et procédé de commande de secours utilisés dans un système de commande de vol distribué |
JP2009523657A (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 | 統合バックアップ制御システム用のシステムおよび方法 |
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 |
US8401716B2 (en) * | 2006-05-17 | 2013-03-19 | Textron Innovations Inc. | Flight control systems |
US8380364B2 (en) | 2006-05-17 | 2013-02-19 | Textron Innovations, Inc. | Manual and computerized flight control system with natural feedback |
US7750593B2 (en) * | 2006-10-26 | 2010-07-06 | Honeywell International Inc. | Active human-machine interface system without a force sensor |
WO2008087629A2 (fr) | 2007-01-16 | 2008-07-24 | Simbionix Ltd. | Simulation chirurgicale préopératoire |
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 |
EP3594111A1 (fr) * | 2013-07-16 | 2020-01-15 | McCulloch, Norman L | Système de rétroaction pour un élément de commande de vol |
US10196131B2 (en) * | 2016-02-16 | 2019-02-05 | The Boeing Company | Hydraulic system and method for an aircraft flight control system |
WO2018156618A1 (fr) * | 2017-02-21 | 2018-08-30 | Configurable Controls, Llc | Système de commande de mouvement pour dispositif de commande de vol actionné au pied |
US11524767B2 (en) | 2021-03-31 | 2022-12-13 | Beta Air, Llc | Methods and systems for flight control configured for use in an electric aircraft |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
FR1562705A (fr) * | 1967-05-19 | 1969-04-04 | ||
US3450375A (en) * | 1967-02-02 | 1969-06-17 | Bertea Corp | Load feel computer |
US3659173A (en) * | 1970-06-19 | 1972-04-25 | Bendix Corp | Aircraft control system including limiting means |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
US3520499A (en) * | 1968-05-29 | 1970-07-14 | United Aircraft Corp | Flight control system |
US4095763A (en) * | 1977-02-25 | 1978-06-20 | Textron, Inc. | Fail safe augmentation system |
-
1978
- 1978-02-24 DE DE2807902A patent/DE2807902C2/de not_active Expired
-
1979
- 1979-02-21 US US06/013,748 patent/US4236685A/en not_active Expired - Lifetime
- 1979-02-23 CA CA000322214A patent/CA1118516A/fr not_active Expired
- 1979-02-23 GB GB7906399A patent/GB2014917B/en not_active Expired
- 1979-02-23 IT IT20458/79A patent/IT1110227B/it active
- 1979-02-23 FR FR7904695A patent/FR2418152A1/fr active Granted
- 1979-02-24 JP JP2024079A patent/JPS54122598A/ja active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
US3450375A (en) * | 1967-02-02 | 1969-06-17 | Bertea Corp | Load feel computer |
FR1562705A (fr) * | 1967-05-19 | 1969-04-04 | ||
US3659173A (en) * | 1970-06-19 | 1972-04-25 | Bendix Corp | Aircraft control system including limiting means |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2604001A1 (fr) * | 1986-09-15 | 1988-03-18 | Aerospatiale | Systeme de commande de vol electrique avec protection en incidence pour aeronef |
EP0261015A1 (fr) * | 1986-09-15 | 1988-03-23 | AEROSPATIALE Société Nationale Industrielle | Système de commande de vol électrique avec protection en incidence pour aéronef |
WO1995012152A1 (fr) * | 1992-10-06 | 1995-05-04 | Honeywell Inc. | Boucle d'asservissement de dispositif de commande manuel actif |
Also Published As
Publication number | Publication date |
---|---|
FR2418152B1 (fr) | 1983-06-17 |
JPS54122598A (en) | 1979-09-22 |
GB2014917A (en) | 1979-09-05 |
US4236685A (en) | 1980-12-02 |
IT1110227B (it) | 1985-12-23 |
CA1118516A (fr) | 1982-02-16 |
DE2807902B1 (de) | 1979-08-23 |
GB2014917B (en) | 1982-05-06 |
DE2807902C2 (de) | 1980-04-30 |
IT7920458A0 (it) | 1979-02-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |