FR2099479A1 - - Google Patents

Info

Publication number
FR2099479A1
FR2099479A1 FR7126519A FR7126519A FR2099479A1 FR 2099479 A1 FR2099479 A1 FR 2099479A1 FR 7126519 A FR7126519 A FR 7126519A FR 7126519 A FR7126519 A FR 7126519A FR 2099479 A1 FR2099479 A1 FR 2099479A1
Authority
FR
France
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
Application number
FR7126519A
Other languages
French (fr)
Other versions
FR2099479B1 (en
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.)
Ltv Electrosystems Inc
Original Assignee
Ltv Electrosystems Inc
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 Ltv Electrosystems Inc filed Critical Ltv Electrosystems Inc
Publication of FR2099479A1 publication Critical patent/FR2099479A1/fr
Application granted granted Critical
Publication of FR2099479B1 publication Critical patent/FR2099479B1/fr
Expired 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
    • G05D1/0055—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
    • G05D1/0077—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements using redundant signals or controls
FR7126519A 1970-07-20 1971-07-20 Expired FR2099479B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US5655170A 1970-07-20 1970-07-20

Publications (2)

Publication Number Publication Date
FR2099479A1 true FR2099479A1 (en) 1972-03-17
FR2099479B1 FR2099479B1 (en) 1975-02-21

Family

ID=22005144

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7126519A Expired FR2099479B1 (en) 1970-07-20 1971-07-20

Country Status (4)

Country Link
US (1) US3679156A (en)
DE (1) DE2135366C2 (en)
FR (1) FR2099479B1 (en)
GB (1) GB1328592A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2683502A1 (en) * 1991-11-12 1993-05-14 Aerospatiale System for controlling the movement of a movable mechanical element, and a flight control system for aircraft including it

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1488667A (en) * 1973-12-07 1977-10-12 Lucas Industries Ltd Actuating arrangement for aircraft control surfaces
US4270809A (en) * 1978-05-12 1981-06-02 Honda Giken Kogyo Kabushiki Kaisha Device for diagnosing trouble in a control circuit for electromagnetic actuators
GB2054173B (en) * 1978-07-21 1982-09-08 Honda Motor Co Ltd Trouble diagnosing device of a control system
WO1982000862A1 (en) * 1980-09-02 1982-03-18 Rockwell International Corp Actuator system for a control surface of an aircraft
US4466597A (en) * 1981-12-02 1984-08-21 Pneumo Corporation Electro-mechanical direct drive valve servo system with rotary to linear valve drive mechanism
FR2557854B1 (en) * 1984-01-09 1987-01-23 Aerospatiale FLIGHT CONTROL SYSTEM FOR AIRCRAFT
DE3462866D1 (en) * 1984-01-09 1987-05-07 Aerospatiale Aircraft flight control system
FR2557853B1 (en) * 1984-01-09 1986-04-25 Aerospatiale FLIGHT CONTROL SYSTEM FOR AIRCRAFT
US5074495A (en) * 1987-12-29 1991-12-24 The Boeing Company Load-adaptive hybrid actuator system and method for actuating control surfaces
US5033694A (en) * 1989-09-08 1991-07-23 Daiichi Electric Kabushiki Kaisha Attitude control device for air or sea transportation craft
US5082208A (en) * 1989-09-29 1992-01-21 The Boeing Company System and method for controlling an aircraft flight control member
US5182505A (en) * 1991-06-19 1993-01-26 Honeywell Inc. Aircraft control surface position transducer
US5493497A (en) * 1992-06-03 1996-02-20 The Boeing Company Multiaxis redundant fly-by-wire primary flight control system
US5670856A (en) * 1994-11-07 1997-09-23 Alliedsignal Inc. Fault tolerant controller arrangement for electric motor driven apparatus
US5678786A (en) * 1995-12-06 1997-10-21 Mcdonnell Douglas Helicopter Co. Reconfigurable helicopter flight control system
DE19628395C2 (en) * 1996-07-13 1998-06-04 Daimler Benz Aerospace Airbus System for controlling the exhaust air volume flows of an aircraft
US5806805A (en) * 1996-08-07 1998-09-15 The Boeing Company Fault tolerant actuation system for flight control actuators
US6209825B1 (en) 1998-02-27 2001-04-03 Lockheed Martin Corporation Low power loss electro hydraulic actuator
US6481203B1 (en) 1999-06-10 2002-11-19 Tecumseh Products Company Electric shifting of a variable speed transmission
US6443399B1 (en) * 2000-07-14 2002-09-03 Honeywell International Inc. Flight control module merged into the integrated modular avionics
US6439512B1 (en) * 2000-08-24 2002-08-27 Hr Textron, Inc. All-hydraulic powered horizontal stabilizer trim control surface position control system
US6923405B2 (en) * 2003-11-17 2005-08-02 The Boeing Company Enhanced rudder control system
US7786684B2 (en) * 2007-10-22 2010-08-31 Honeywell International Inc. Electromechanical flight control system and method for rotorcraft
US8172174B2 (en) * 2008-11-13 2012-05-08 Honeywell International Inc. Hybrid electromechanical/hydromechanical actuator and actuation control system
GB2503397B (en) * 2011-03-29 2017-10-18 Bae Systems Plc A control system for an un-manned vehicle

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3198082A (en) * 1962-11-09 1965-08-03 Lockheed Aircraft Corp Electrical primary flight control system utilizing redundant channels
US3469162A (en) * 1965-04-13 1969-09-23 Hawker Siddeley Dynamics Ltd Multiplex-type control apparatus

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2898889A (en) * 1958-10-03 1959-08-11 John V Foster Mechanically-limited, electrically operated hydraulic valve system for aircraft controls
US3027878A (en) * 1959-06-10 1962-04-03 Honeywell Regulator Co Fluid motor control apparatus
US3426650A (en) * 1965-12-23 1969-02-11 Bell Aerospace Corp Triple channel redundant hydraeric control system
US3401600A (en) * 1965-12-23 1968-09-17 Bell Aerospace Corp Control system having a plurality of control chains each of which may be disabled in event of failure thereof
US3422767A (en) * 1966-12-05 1969-01-21 Webster Electric Co Inc Variable displacement swashplate pumps
US3554084A (en) * 1967-11-17 1971-01-12 Honeywell Inc Redundant force summing servo unit
US3505929A (en) * 1968-04-16 1970-04-14 Gen Electric Redundant flight control servoactuator

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3198082A (en) * 1962-11-09 1965-08-03 Lockheed Aircraft Corp Electrical primary flight control system utilizing redundant channels
US3469162A (en) * 1965-04-13 1969-09-23 Hawker Siddeley Dynamics Ltd Multiplex-type control apparatus

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
(REVUE GB AIRCRAFT ENGINEERING,VOLUME 38,DECEMBRE 1966,NO 4,PAGES 19,20 ET 25 A 28,P.J.MALTBY" A NEW DEVELOPMENT IN MULTIPLEX ELECTRO-HYDRAULIC ACTUATORS".) *
A NEW DEVELOPMENT IN MULTIPLEX ELECTRO-HYDRAULIC ACTUATORS".) *
REVUE GB AIRCRAFT ENGINEERING,VOLUME 38,DECEMBRE 1966,NO 4,PAGES 19,20 ET 25 A 28,P.J.MALTBY" *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2683502A1 (en) * 1991-11-12 1993-05-14 Aerospatiale System for controlling the movement of a movable mechanical element, and a flight control system for aircraft including it

Also Published As

Publication number Publication date
US3679156A (en) 1972-07-25
DE2135366A1 (en) 1972-02-03
FR2099479B1 (en) 1975-02-21
GB1328592A (en) 1973-08-30
DE2135366C2 (en) 1982-04-01

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