JP2016022942A5 - - Google Patents

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Publication number
JP2016022942A5
JP2016022942A5 JP2015096358A JP2015096358A JP2016022942A5 JP 2016022942 A5 JP2016022942 A5 JP 2016022942A5 JP 2015096358 A JP2015096358 A JP 2015096358A JP 2015096358 A JP2015096358 A JP 2015096358A JP 2016022942 A5 JP2016022942 A5 JP 2016022942A5
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JP
Japan
Prior art keywords
control module
flight
actuator
flight control
error
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
Application number
JP2015096358A
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English (en)
Japanese (ja)
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JP2016022942A (ja
JP6407096B2 (ja
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Publication date
Priority claimed from US14/332,514 external-priority patent/US9533752B2/en
Application filed filed Critical
Publication of JP2016022942A publication Critical patent/JP2016022942A/ja
Publication of JP2016022942A5 publication Critical patent/JP2016022942A5/ja
Application granted granted Critical
Publication of JP6407096B2 publication Critical patent/JP6407096B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2015096358A 2014-07-16 2015-05-11 飛行操縦翼面のための入力一致システム Active JP6407096B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/332,514 US9533752B2 (en) 2014-07-16 2014-07-16 Input congruence system for flight control surfaces
US14/332,514 2014-07-16

Publications (3)

Publication Number Publication Date
JP2016022942A JP2016022942A (ja) 2016-02-08
JP2016022942A5 true JP2016022942A5 (enExample) 2018-06-21
JP6407096B2 JP6407096B2 (ja) 2018-10-17

Family

ID=53541617

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015096358A Active JP6407096B2 (ja) 2014-07-16 2015-05-11 飛行操縦翼面のための入力一致システム

Country Status (6)

Country Link
US (1) US9533752B2 (enExample)
EP (2) EP3446969A1 (enExample)
JP (1) JP6407096B2 (enExample)
CN (1) CN105278539B (enExample)
BR (1) BR102015014081B1 (enExample)
CA (1) CA2891307C (enExample)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3072475B1 (fr) * 2017-10-17 2019-11-01 Thales Procede de traitement d'une erreur lors de l'execution d'une procedure avionique predeterminee, programme d'ordinateur et systeme de detection et d'alerte associe
EP3483673B1 (en) * 2017-11-14 2023-06-14 TTTech Auto AG Method and computer system to consistently control a set of actuators
US10599534B1 (en) * 2018-11-06 2020-03-24 Bae Systems Controls Inc. Three lane bit-for-bit remote electronic unit
FR3106907B1 (fr) * 2020-01-31 2022-02-11 Thales Sa Dispositif electronique de calcul de diffusion centralises d'etat(s) d'un aeronef, ensemble avionique, procede, et programme d'ordinateur associes

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5493497A (en) * 1992-06-03 1996-02-20 The Boeing Company Multiaxis redundant fly-by-wire primary flight control system
US5515282A (en) * 1994-04-25 1996-05-07 The Boeing Company Method and apparatus for implementing a databus voter to select flight command signals from one of several redundant asynchronous digital primary flight computers
US5802077A (en) 1995-05-15 1998-09-01 The Boeing Company Method and apparatus for obtaining high integrity and availability in a multi-channel system
US7209809B2 (en) 2003-10-15 2007-04-24 The Boeing Company Method and apparatus for obtaining high integrity and availability in multi-channel systems
US20100318245A1 (en) 2005-03-03 2010-12-16 Nabtesco Corporation Flight control system
US7725215B2 (en) 2005-08-05 2010-05-25 Honeywell International Inc. Distributed and recoverable digital control system
US8386093B2 (en) 2007-04-05 2013-02-26 Bombardier Inc. Multi-axis serially redundant, single channel, multi-path fly-by-wire flight control system
FR2916890B1 (fr) * 2007-05-31 2009-07-24 Airbus France Sas Procede et dispositif de surveillance de systemes avioniques relies a un media partage
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
FR2941913B1 (fr) * 2009-02-10 2012-08-31 Airbus France Systeme de commande de vol et aeronef le comportant
DE102011010679A1 (de) * 2011-02-08 2012-08-09 Eads Deutschland Gmbh Unbemanntes Luftfahrzeug mit eingebautem Kollisionswarnsystem

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