DE3688265D1 - Digitales automatisches flugsteuersystem mit ueberwachung ungleichartiger funktionen. - Google Patents

Digitales automatisches flugsteuersystem mit ueberwachung ungleichartiger funktionen.

Info

Publication number
DE3688265D1
DE3688265D1 DE8686303800T DE3688265T DE3688265D1 DE 3688265 D1 DE3688265 D1 DE 3688265D1 DE 8686303800 T DE8686303800 T DE 8686303800T DE 3688265 T DE3688265 T DE 3688265T DE 3688265 D1 DE3688265 D1 DE 3688265D1
Authority
DE
Germany
Prior art keywords
monitoring
control system
flight control
automatic flight
unique functions
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.)
Expired - Fee Related
Application number
DE8686303800T
Other languages
English (en)
Other versions
DE3688265T2 (de
Inventor
Dale Dean Davidson
Douglas Gene Endrud
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.)
Honeywell Inc
Original Assignee
Honeywell 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 Honeywell Inc filed Critical Honeywell Inc
Publication of DE3688265D1 publication Critical patent/DE3688265D1/de
Application granted granted Critical
Publication of DE3688265T2 publication Critical patent/DE3688265T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/07—Responding to the occurrence of a fault, e.g. fault tolerance
    • G06F11/16—Error detection or correction of the data by redundancy in hardware
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Quality & Reliability (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Feedback Control In General (AREA)
  • Safety Devices In Control Systems (AREA)
  • Ceramic Products (AREA)
  • Hardware Redundancy (AREA)
DE8686303800T 1985-05-30 1986-05-19 Digitales automatisches flugsteuersystem mit ueberwachung ungleichartiger funktionen. Expired - Fee Related DE3688265T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/739,583 US4799159A (en) 1985-05-30 1985-05-30 Digital automatic flight control system with disparate function monitoring

Publications (2)

Publication Number Publication Date
DE3688265D1 true DE3688265D1 (de) 1993-05-19
DE3688265T2 DE3688265T2 (de) 1993-09-09

Family

ID=24972957

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8686303800T Expired - Fee Related DE3688265T2 (de) 1985-05-30 1986-05-19 Digitales automatisches flugsteuersystem mit ueberwachung ungleichartiger funktionen.

Country Status (7)

Country Link
US (1) US4799159A (de)
EP (1) EP0207611B1 (de)
JP (1) JPS61276036A (de)
BR (1) BR8602323A (de)
CA (1) CA1262178A (de)
DE (1) DE3688265T2 (de)
IL (1) IL78896A (de)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4713757A (en) 1985-06-11 1987-12-15 Honeywell Inc. Data management equipment for automatic flight control systems having plural digital processors
US5184312A (en) * 1985-10-13 1993-02-02 The Boeing Company Distributed built-in test equipment system for digital avionics
FR2628858B1 (fr) * 1988-03-15 1990-08-17 Aerospatiale Systeme de commande de vol pour aeronef
DE3816254A1 (de) * 1988-05-11 1989-11-23 Siemens Ag Steuereinheit zur lenkung der hinterraeder eines strassenfahrzeuges
US5448480A (en) * 1988-05-11 1995-09-05 Siemens Aktiengesellschaft Fail-safe operation via controller redundancy for steering the back wheels of a road vehicle
US5377109A (en) * 1992-07-31 1994-12-27 Lear Astronics Corp. Failsafe digital bus to analog protocol converter system
FR2706153B1 (fr) * 1993-06-07 1995-08-18 Sextant Avionique Dispositif de pilotage automatique pour aérodynes.
JPH07262148A (ja) * 1994-03-22 1995-10-13 Nec Corp コンピュータシステム
US5553237A (en) * 1994-12-13 1996-09-03 Base Ten Systems, Inc. Safety critical monitoring of microprocessor controlled embedded systems
JPH08235006A (ja) * 1995-02-24 1996-09-13 Fujitsu Ltd 状態監視システム
FR2760109B1 (fr) * 1997-02-25 1999-05-28 Sextant Avionique Procede et dispositif pour l'execution par un processeur unique de plusieurs fonctions de niveaux de criticite differents, avec une grande securite de fonctionnement
US6367031B1 (en) * 1998-12-17 2002-04-02 Honeywell International Inc. Critical control adaption of integrated modular architecture
US6517396B1 (en) * 2000-07-03 2003-02-11 Stephen W. Into Boat speed control
US6573672B2 (en) * 2001-06-29 2003-06-03 Honeywell International Inc. Fail passive servo controller
GB2384313A (en) * 2002-01-18 2003-07-23 Qinetiq Ltd An attitude sensor
CN100356281C (zh) * 2004-03-16 2007-12-19 清华大学 一种用于飞行器的自动驾驶仪
US7421526B2 (en) * 2005-08-24 2008-09-02 Honeywell International Inc. Reconfigurable virtual backplane architecture
US7933696B2 (en) * 2006-08-31 2011-04-26 GM Global Technology Operations LLC Distributed arithmetic logic unit security check
US8015390B1 (en) 2008-03-19 2011-09-06 Rockwell Collins, Inc. Dissimilar processor synchronization in fly-by-wire high integrity computing platforms and displays
US7852235B1 (en) 2008-04-28 2010-12-14 Rockwell Collins, Inc. High integrity computing via input synchronization systems and methods
DE102009007215A1 (de) * 2009-02-03 2010-08-05 Siemens Aktiengesellschaft Automatisierungssystem mit einem programmierbaren Matrixmodul
US8682562B2 (en) * 2009-05-08 2014-03-25 Rolls-Royce Corporation Turbine engine thrust scheduling
US8151024B2 (en) * 2009-05-28 2012-04-03 Honeywell International Inc. Reconfigurable virtual backplane systems and methods
CN104123122A (zh) * 2013-04-24 2014-10-29 成都飞机设计研究所 一种非相似三余度飞控计算机的非相似余度软件开发方法
WO2018100494A1 (en) * 2016-11-30 2018-06-07 Bombardier Inc. Aircraft control system with residual error containment
FR3075997B1 (fr) * 2017-12-26 2020-01-10 Thales Calculateur electronique de mise en oeuvre d'au moins une fonction critique, dispositif electronique, procede et programme d'ordinateur associes
WO2019217634A1 (en) 2018-05-09 2019-11-14 Abb Schweiz Ag Valve position control
DE102020107172A1 (de) * 2020-03-16 2021-09-16 Volocopter Gmbh Verfahren zur Steuerung eines Fluggeräts, Steuerungseinrichtung für ein Fluggerät und Fluggerät mit einer solchen Steuerungseinrichtung

Family Cites Families (11)

* 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
GB1502184A (en) * 1974-07-05 1978-02-22 Sperry Rand Corp Automatic flight control systems
US3994456A (en) * 1975-05-29 1976-11-30 Sperry Rand Corporation Steered lateral course transition control apparatus for aircraft area navigation systems
FR2344063A1 (fr) * 1976-03-10 1977-10-07 Smiths Industries Ltd Circuit numerique de commande a deux voies au moins
US4330826A (en) * 1980-02-05 1982-05-18 The Bendix Corporation Synchronizer and synchronization system for a multiple computer system
JPS56166562A (en) * 1980-05-23 1981-12-21 Mitsubishi Electric Corp Data processor
US4370706A (en) * 1980-09-26 1983-01-25 The Bendix Corporation Controller for a dual servo system
EP0096510B1 (de) * 1982-06-03 1988-07-27 LUCAS INDUSTRIES public limited company Steuerungssystem in erster Linie reagierend auf Signale von Digitalrechnern
WO1984000071A1 (en) * 1982-06-16 1984-01-05 Boeing Co Autopilot flight director system
US4622667A (en) * 1984-11-27 1986-11-11 Sperry Corporation Digital fail operational automatic flight control system utilizing redundant dissimilar data processing

Also Published As

Publication number Publication date
IL78896A0 (en) 1986-09-30
EP0207611A2 (de) 1987-01-07
IL78896A (en) 1990-11-29
JPS61276036A (ja) 1986-12-06
CA1262178A (en) 1989-10-03
US4799159A (en) 1989-01-17
EP0207611B1 (de) 1993-04-14
BR8602323A (pt) 1987-01-21
DE3688265T2 (de) 1993-09-09
EP0207611A3 (en) 1989-03-29

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee