FR2992122B1 - Dispositif de conversion securise de commandes numeriques en signaux analogiques de puissance pour aeronef - Google Patents

Dispositif de conversion securise de commandes numeriques en signaux analogiques de puissance pour aeronef

Info

Publication number
FR2992122B1
FR2992122B1 FR1201713A FR1201713A FR2992122B1 FR 2992122 B1 FR2992122 B1 FR 2992122B1 FR 1201713 A FR1201713 A FR 1201713A FR 1201713 A FR1201713 A FR 1201713A FR 2992122 B1 FR2992122 B1 FR 2992122B1
Authority
FR
France
Prior art keywords
aircraft
power signals
digital controls
analogue power
secure conversion
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.)
Active
Application number
FR1201713A
Other languages
English (en)
Other versions
FR2992122A1 (fr
Inventor
Yannick Meret
Damien Brocas
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.)
Thales SA
Original Assignee
Thales SA
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 Thales SA filed Critical Thales SA
Priority to FR1201713A priority Critical patent/FR2992122B1/fr
Priority to US13/918,508 priority patent/US20130338846A1/en
Publication of FR2992122A1 publication Critical patent/FR2992122A1/fr
Application granted granted Critical
Publication of FR2992122B1 publication Critical patent/FR2992122B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F1/00—Details not covered by groups G06F3/00 - G06F13/00 and G06F21/00
    • G06F1/26—Power supply means, e.g. regulation thereof
    • 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
    • G05B19/00—Programme-control systems
    • G05B19/02—Programme-control systems electric
    • G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
    • G05B19/042—Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
    • G05B19/0428—Safety, monitoring
    • 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
    • B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
FR1201713A 2012-06-15 2012-06-15 Dispositif de conversion securise de commandes numeriques en signaux analogiques de puissance pour aeronef Active FR2992122B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1201713A FR2992122B1 (fr) 2012-06-15 2012-06-15 Dispositif de conversion securise de commandes numeriques en signaux analogiques de puissance pour aeronef
US13/918,508 US20130338846A1 (en) 2012-06-15 2013-06-14 Secure device for converting digital controls into analog power signals for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1201713A FR2992122B1 (fr) 2012-06-15 2012-06-15 Dispositif de conversion securise de commandes numeriques en signaux analogiques de puissance pour aeronef

Publications (2)

Publication Number Publication Date
FR2992122A1 FR2992122A1 (fr) 2013-12-20
FR2992122B1 true FR2992122B1 (fr) 2014-06-27

Family

ID=47827266

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1201713A Active FR2992122B1 (fr) 2012-06-15 2012-06-15 Dispositif de conversion securise de commandes numeriques en signaux analogiques de puissance pour aeronef

Country Status (2)

Country Link
US (1) US20130338846A1 (fr)
FR (1) FR2992122B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3049075B1 (fr) * 2016-03-15 2018-03-09 Sagem Defense Securite Dispositif d'actionnement et carte de commande et de surveillance associee
FR3075491B1 (fr) * 2017-12-14 2019-12-20 Safran Landing Systems Harnais electrique

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5377109A (en) * 1992-07-31 1994-12-27 Lear Astronics Corp. Failsafe digital bus to analog protocol converter system
DE19922561A1 (de) * 1999-05-17 2000-11-23 Sick Ag Verfahren und Vorrichtung zur sicheren Übertragung von Datensignalen über ein Bussystem
US7017861B1 (en) * 2000-05-22 2006-03-28 Saab Ab Control system for actuators in an aircraft
US6366837B1 (en) * 2000-07-14 2002-04-02 Honeywell International Inc. Method for providing command augmentation to a command lane within a vehicle
US7182296B2 (en) * 2002-03-28 2007-02-27 Honeywell International, Inc. Methods and apparatus for error-tolerant wrap-back ACE monitor
FR2838532B1 (fr) * 2002-04-10 2004-07-30 Airbus France Systeme et procede de controle de plusieurs actionneurs
EP1443399B1 (fr) * 2003-01-23 2009-05-20 Supercomputing Systems AG Système à tolérance de fautes contrôlé par un ordinateur
US7209809B2 (en) * 2003-10-15 2007-04-24 The Boeing Company Method and apparatus for obtaining high integrity and availability in multi-channel systems
US7021587B1 (en) * 2004-01-07 2006-04-04 Trutrak Flight Systems, Inc Dual channel fail-safe system and method for adjusting aircraft trim
US7108232B2 (en) * 2004-02-05 2006-09-19 Hoh Roger H Helicopter force-feel and stability augmentation system with parallel servo-actuator
US8099179B2 (en) * 2004-09-10 2012-01-17 GM Global Technology Operations LLC Fault tolerant control system
US7789345B2 (en) * 2005-03-03 2010-09-07 Nabtesco Corporation Actuator control apparatus
US8188860B2 (en) * 2007-10-22 2012-05-29 Infineon Technologies Ag Secure sensor/actuator systems
FR2927308B1 (fr) * 2008-02-08 2010-10-22 Airbus France Systeme distribue de commande de vol.
FR2941912B1 (fr) * 2009-02-10 2011-02-18 Airbus France Systeme de commande de vol et aeronef le comportant
US8690101B2 (en) * 2012-05-18 2014-04-08 Rockwell Collins, Inc. Triplex cockpit control data acquisition electronics

Also Published As

Publication number Publication date
FR2992122A1 (fr) 2013-12-20
US20130338846A1 (en) 2013-12-19

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