IT8124118A0 - Apparecchiatura di controllo per un servosistema doppio. - Google Patents

Apparecchiatura di controllo per un servosistema doppio.

Info

Publication number
IT8124118A0
IT8124118A0 IT8124118A IT2411881A IT8124118A0 IT 8124118 A0 IT8124118 A0 IT 8124118A0 IT 8124118 A IT8124118 A IT 8124118A IT 2411881 A IT2411881 A IT 2411881A IT 8124118 A0 IT8124118 A0 IT 8124118A0
Authority
IT
Italy
Prior art keywords
control equipment
servo system
dual servo
dual
equipment
Prior art date
Application number
IT8124118A
Other languages
English (en)
Other versions
IT1138241B (it
Inventor
Jerry Doniger
Albert T Kirchhein
Gibson Reynolds
Original Assignee
Bendix Corp
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 Bendix Corp filed Critical Bendix Corp
Publication of IT8124118A0 publication Critical patent/IT8124118A0/it
Application granted granted Critical
Publication of IT1138241B publication Critical patent/IT1138241B/it

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B23/00—Testing or monitoring of control systems or parts thereof
    • G05B23/02—Electric testing or monitoring
    • G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
    • G05B23/0218—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterised by the fault detection method dealing with either existing or incipient faults
    • G05B23/0243—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterised by the fault detection method dealing with either existing or incipient faults model based detection method, e.g. first-principles knowledge model
    • G05B23/0245—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterised by the fault detection method dealing with either existing or incipient faults model based detection method, e.g. first-principles knowledge model based on a qualitative model, e.g. rule based; if-then decisions
    • 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
    • G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00—Program-control systems
    • G05B2219/30—Nc systems
    • G05B2219/41—Servomotor, servo controller till figures
    • G05B2219/41264—Driven by two motors

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Safety Devices In Control Systems (AREA)
IT24118/81A 1980-09-26 1981-09-24 Apparecchiatura di controllo per un servosistema doppio IT1138241B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/191,231 US4370706A (en) 1980-09-26 1980-09-26 Controller for a dual servo system

Publications (2)

Publication Number Publication Date
IT8124118A0 true IT8124118A0 (it) 1981-09-24
IT1138241B IT1138241B (it) 1986-09-17

Family

ID=22704650

Family Applications (1)

Application Number Title Priority Date Filing Date
IT24118/81A IT1138241B (it) 1980-09-26 1981-09-24 Apparecchiatura di controllo per un servosistema doppio

Country Status (6)

Country Link
US (1) US4370706A (it)
JP (1) JPS5786901A (it)
CA (1) CA1160327A (it)
DE (1) DE3137157A1 (it)
GB (1) GB2084349B (it)
IT (1) IT1138241B (it)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4472780A (en) * 1981-09-28 1984-09-18 The Boeing Company Fly-by-wire lateral control system
DE3200839C1 (de) * 1982-01-14 1983-08-25 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Vorrichtung zum Trimmen von Flugzeugen
EP0093276B1 (en) * 1982-04-15 1988-10-26 General Electric Company Turbine control system
EP0096510B1 (en) * 1982-06-03 1988-07-27 LUCAS INDUSTRIES public limited company Control system primarily responsive to signals from digital computers
GB8426486D0 (en) * 1984-10-19 1984-11-28 Lucas Ind Plc Electro-hydraulic actuator systems
US4622667A (en) * 1984-11-27 1986-11-11 Sperry Corporation Digital fail operational automatic flight control system utilizing redundant dissimilar data processing
US4799159A (en) * 1985-05-30 1989-01-17 Honeywell Inc. Digital automatic flight control system with disparate function monitoring
GB2196445A (en) * 1986-10-17 1988-04-27 John James Sylvester Derry Condition monitoring equipment for power output devices
US4807516A (en) * 1987-04-23 1989-02-28 The Boeing Company Flight control system employing three controllers operating a dual actuator
US5442544A (en) * 1990-01-26 1995-08-15 Honeywell Inc. Single input single output rate optimal controller
US5287045A (en) * 1990-02-20 1994-02-15 Kabushiki Kaisha Toshiba Fully digital apparatus for controlling operation of electric motor
US5274554A (en) * 1991-02-01 1993-12-28 The Boeing Company Multiple-voting fault detection system for flight critical actuation control systems
GB9121540D0 (en) * 1991-10-10 1991-11-27 Smiths Industries Plc Computing systems and methods
US5593109A (en) * 1995-01-10 1997-01-14 Lucas Western, Inc. Actuator system and method
JP2002160701A (ja) * 2000-11-22 2002-06-04 Ishida Co Ltd 包装装置
US7854737B2 (en) * 2002-12-20 2010-12-21 Depuy Products, Inc. Instrument and associated method of trailing for modular hip stems
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
GB2410341A (en) * 2004-01-23 2005-07-27 Biacore Ab Method and apparatus for the development of a control process for an instrument
US7433741B2 (en) * 2005-09-30 2008-10-07 Rockwell Automation Technologies, Inc. Hybrid user interface having base presentation information with variably prominent supplemental information
US7878461B2 (en) * 2006-01-17 2011-02-01 Gulfstream Aerospace Corporation System and method for an integrated backup control system
CA2637226A1 (en) 2006-01-17 2007-07-26 Gulfstream Aerospace Corporation Apparatus and method for backup control in a distributed flight control system
GB0611525D0 (en) * 2006-06-10 2006-07-19 Goodrich Actuation Systems Sas Actuator arrangement
US8172174B2 (en) * 2008-11-13 2012-05-08 Honeywell International Inc. Hybrid electromechanical/hydromechanical actuator and actuation control system
US8365024B2 (en) * 2010-02-26 2013-01-29 Honeywell International Inc. High integrity data bus fault detection using multiple signal components
GB201004026D0 (en) * 2010-03-10 2010-04-28 Airbus Operations Ltd Slat monitoring system
US8054208B2 (en) 2010-03-30 2011-11-08 Honeywell International Inc. Re-configurable multipurpose analog interface
US8782299B2 (en) 2010-04-27 2014-07-15 Honeywell International Inc. Re-configurable multi-purpose digital interface
US8390324B2 (en) 2010-09-20 2013-03-05 Honeywell International Inc. Universal functionality module
CN102426432B (zh) * 2011-12-30 2013-07-03 北京华航无线电测量研究所 一种三维成像安检门伺服控制装置
CN102419560B (zh) * 2011-12-30 2013-07-03 北京华航无线电测量研究所 一种三维成像安检门伺服控制装置的伺服控制器
JP6196097B2 (ja) * 2013-08-12 2017-09-13 日本信号株式会社 遮断装置
SG11202106268PA (en) * 2018-12-19 2021-07-29 Safran Electronics & Defense System for configuring an aircraft in a single-pilot mode or a two-pilot mode

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3688099A (en) * 1971-04-28 1972-08-29 Lear Siegler Inc Automatic control system with a digital computer
CA1026850A (en) * 1973-09-24 1978-02-21 Smiths Industries Limited Dual, simultaneously operating control system with fault detection
US4035705A (en) * 1975-03-17 1977-07-12 Sperry Rand Corporation Fail-safe dual channel automatic pilot with maneuver limiting
FR2344063A1 (fr) * 1976-03-10 1977-10-07 Smiths Industries Ltd Circuit numerique de commande a deux voies au moins
CA1118101A (en) * 1977-06-02 1982-02-09 Jerry Doniger Digital flight guidance system
US4159444A (en) * 1978-03-21 1979-06-26 Sperry Rand Corporation Fail operational dual electromechanical servo actuator for aircraft with model monitoring
US4209734A (en) * 1978-03-27 1980-06-24 Sperry Corporation Dynamic equalization system for dual channel automatic pilot
US4313201A (en) * 1980-03-05 1982-01-26 United Technologies Corporation Tested, dissimilar helicopter stability augmentation

Also Published As

Publication number Publication date
US4370706A (en) 1983-01-25
GB2084349A (en) 1982-04-07
JPS5786901A (en) 1982-05-31
CA1160327A (en) 1984-01-10
IT1138241B (it) 1986-09-17
DE3137157A1 (de) 1982-05-13
GB2084349B (en) 1984-03-07

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