NO941141L - Funksjonssikkert digital-buss/analog-protopkoll omformer system - Google Patents

Funksjonssikkert digital-buss/analog-protopkoll omformer system

Info

Publication number
NO941141L
NO941141L NO941141A NO941141A NO941141L NO 941141 L NO941141 L NO 941141L NO 941141 A NO941141 A NO 941141A NO 941141 A NO941141 A NO 941141A NO 941141 L NO941141 L NO 941141L
Authority
NO
Norway
Prior art keywords
digital
analog
interface
control
bus
Prior art date
Application number
NO941141A
Other languages
English (en)
Other versions
NO941141D0 (no
Inventor
John Arthur Baker
Otto Hubert Boe
Wayne Erlin Burklund
Robert William Edmeads
Melvin Gerard Oster
Original Assignee
Lear Astronics 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 Lear Astronics Corp filed Critical Lear Astronics Corp
Publication of NO941141D0 publication Critical patent/NO941141D0/no
Publication of NO941141L publication Critical patent/NO941141L/no

Links

Classifications

    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; 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
    • G06F11/20—Error detection or correction of the data by redundancy in hardware using active fault-masking, e.g. by switching out faulty elements or by switching in spare elements
    • G06F11/2002—Error detection or correction of the data by redundancy in hardware using active fault-masking, e.g. by switching out faulty elements or by switching in spare elements where interconnections or communication control functionality are redundant
    • G06F11/2007—Error detection or correction of the data by redundancy in hardware using active fault-masking, e.g. by switching out faulty elements or by switching in spare elements where interconnections or communication control functionality are redundant using redundant communication media
    • 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
    • G05B9/00—Safety arrangements
    • G05B9/02—Safety arrangements electric
    • G05B9/03—Safety arrangements electric with multiple-channel loop, i.e. redundant control systems
    • 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
    • G06—COMPUTING OR CALCULATING; 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
    • G06F11/0796—Safety measures, i.e. ensuring safe condition in the event of error, e.g. for controlling element
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06J—HYBRID COMPUTING ARRANGEMENTS
    • G06J1/00—Hybrid computing arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Quality & Reliability (AREA)
  • General Engineering & Computer Science (AREA)
  • Computer Hardware Design (AREA)
  • Software Systems (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mathematical Physics (AREA)
  • Evolutionary Computation (AREA)
  • Fuzzy Systems (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Safety Devices In Control Systems (AREA)
  • Control By Computers (AREA)
  • Communication Control (AREA)
  • Selective Calling Equipment (AREA)
  • Arrangements For Transmission Of Measured Signals (AREA)
  • Feedback Control In General (AREA)
  • Debugging And Monitoring (AREA)

Abstract

Feilsikker flyelektronisk grensesnittenhet (10) som, tjener som et protokollomformersystem for oversettelse av data for styreformål fra en digital kommunikasjons-buss (65) til en analog styrekanal som en oppgradering eller et grensesnitt til et eksisterende analogt styresystem. Den flyelektroniske grensesnittenheten (10) innbefatter en digital grensesnittbusslogikk. (101), en digital dataprosessormodul (102), et analogt grensesnitt og en modusvalgkrets (104). Data kommuni-sert over den digitale grensesnittbussen (65) blir periodisk oversatt til ekvivalente og analoge styre-signaler. For sikkerhetens skyld sikrer den flyelektroniske grensesnittenheten (10) integriteten til systemet ved gjentagende å gå tilbake i sløyfe eller foreta en rundhopping av digitale ekvivalenter til de analoge utgangssignalene og sammenligne dem med kommanderte digitale styreverdier. Protokoll-omformersystemet overvåker dessuten kommunikasjonene over den digitale databussen med hensyn til datakon-tinuitet. Dersom forskjellen mellom en rundhopp-digitalekvivalent til et analogt utgangssignal og en forventet verdi overskrider tolererbare grenser eller dersom kommunikasjonen feiler, frakobler systemet dennes grensesnitt fra styringen ved anvendelse av redundant programvare og hardvare og returnerer styringen til det analoge styresystemet (51).
NO941141A 1992-07-31 1994-03-28 Funksjonssikkert digital-buss/analog-protopkoll omformer system NO941141L (no)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/923,146 US5377109A (en) 1992-07-31 1992-07-31 Failsafe digital bus to analog protocol converter system
PCT/US1993/007298 WO1994003854A1 (en) 1992-07-31 1993-07-29 Failsafe digital bus to analog protocol converter system

Publications (2)

Publication Number Publication Date
NO941141D0 NO941141D0 (no) 1994-03-28
NO941141L true NO941141L (no) 1994-05-20

Family

ID=25448198

Family Applications (1)

Application Number Title Priority Date Filing Date
NO941141A NO941141L (no) 1992-07-31 1994-03-28 Funksjonssikkert digital-buss/analog-protopkoll omformer system

Country Status (13)

Country Link
US (1) US5377109A (no)
EP (1) EP0606469B1 (no)
JP (1) JPH07503090A (no)
AT (1) ATE198105T1 (no)
AU (1) AU4996693A (no)
CA (1) CA2120347A1 (no)
DE (1) DE69329751T2 (no)
DK (1) DK0606469T3 (no)
GR (1) GR3035461T3 (no)
IL (1) IL106511A (no)
NO (1) NO941141L (no)
PT (1) PT606469E (no)
WO (1) WO1994003854A1 (no)

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DE4336207A1 (de) * 1993-10-23 1995-04-27 Bodenseewerk Geraetetech Schnittstellenanordnung für die Datenübertragung zwischen Trägerflugzeug und Flugkörper
US5555498A (en) * 1994-03-18 1996-09-10 Chrysler Corporation Circuit and method for interfacing vehicle controller and diagnostic test instrument
US5548510A (en) * 1994-10-28 1996-08-20 Mcdonnell Douglas Corporation Method and apparatus for providing a universal electrical interface between an aircraft and an associated store
US5809220A (en) * 1995-07-20 1998-09-15 Raytheon Company Fault tolerant distributed control system
US6133846A (en) * 1996-10-01 2000-10-17 Honeywell Inc. Low cost redundant communications system
US5992290A (en) * 1997-04-09 1999-11-30 Cubic Defense Systems, Inc. Aircraft interface device and crossover cable kit
US6131065A (en) * 1998-02-25 2000-10-10 Cardinal Communications, Inc. Electronic flight data strips and method for air traffic control
US6275503B1 (en) 1998-07-24 2001-08-14 Honeywell International Inc. Method for transmitting large information packets over networks
US6360290B1 (en) 1999-06-23 2002-03-19 United Technologies Corporation Commercial standard digital bus interface circuit
US20020032006A1 (en) * 2000-05-05 2002-03-14 K. Prasad Nair Efficient network routing method for air/ground data services
US7017861B1 (en) * 2000-05-22 2006-03-28 Saab Ab Control system for actuators in an aircraft
US6459228B1 (en) 2001-03-22 2002-10-01 Mpc Products Corporation Dual input servo coupled control sticks
US6718409B2 (en) * 2001-04-06 2004-04-06 The United States Of America As Represented By The Secretary Of The Navy National marine electronics association protocol converter
US7313474B2 (en) * 2002-03-07 2007-12-25 Bg Soflex Llc Simple engine fuel controller
US7353090B2 (en) * 2004-10-04 2008-04-01 The Boeing Company System, bus monitor assembly and method of monitoring at least one data bus of an aircraft
US7487403B2 (en) * 2004-11-12 2009-02-03 International Business Machines Corporation Method for handling a device failure
US7676558B2 (en) * 2004-11-12 2010-03-09 International Business Machines Corporation Configuring shared devices over a fabric
JP5281396B2 (ja) * 2005-06-07 2013-09-04 コーニンクレッカ フィリップス エレクトロニクス エヌ ヴィ フェイルセーフ遠隔制御
US7487015B1 (en) * 2006-07-31 2009-02-03 The United States Of America As Represented By The Secretary Of The Navy Emulator for an inertial navigation unit protocol converter
US7487014B1 (en) * 2006-07-31 2009-02-03 The United States Of America As Represented By The Secretary Of The Navy Inertial navigation unit protocol converter
US7684904B2 (en) * 2007-06-27 2010-03-23 Arinc Incorporated Systems and methods for communication, navigation, surveillance and sensor system integration in a vehicle
US7868276B2 (en) * 2007-10-24 2011-01-11 Lockheed Martin Corporation Airborne vehicle emulation system and method
US7869385B2 (en) * 2007-10-31 2011-01-11 The Boeing Company Interactivity with a bus interface card
FR2992122B1 (fr) * 2012-06-15 2014-06-27 Thales Sa Dispositif de conversion securise de commandes numeriques en signaux analogiques de puissance pour aeronef
CN103676640B (zh) * 2012-09-03 2016-12-28 上海航天测控通信研究所 应用于交会对接的数据通信装置
US10095646B2 (en) 2014-04-29 2018-10-09 Harold Ray Bettencourt Device and method for allowing integration of incompatible devices into a vehicle bus network
US10001776B2 (en) * 2016-03-21 2018-06-19 The Boeing Company Unmanned aerial vehicle flight control system
US10318904B2 (en) 2016-05-06 2019-06-11 General Electric Company Computing system to control the use of physical state attainment of assets to meet temporal performance criteria
US10304559B2 (en) * 2016-12-30 2019-05-28 Western Digital Technologies, Inc. Memory write verification using temperature compensation
DE102018005149A1 (de) * 2018-06-29 2020-01-02 Interroll Holding Ag Analog gesteuerte Fördervorrichtung mit Datenauslesung
US20200023955A1 (en) * 2018-07-23 2020-01-23 Textron Innovations Inc. System and Method for Rotorcraft Flight Control
US11014689B2 (en) 2018-08-13 2021-05-25 Applied Avionics, Inc. Command interpreter or command parser based control architecture for aircraft control, interface units and/or illuminated pushbutton switches
EP4586039A3 (en) * 2020-05-04 2025-11-05 Auterion AG System and method for software-defined drones
US11353890B1 (en) 2021-06-16 2022-06-07 Beta Air, Llc Electrical vertical take-off and landing aircraft having reversionary flight control and method of use

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DE3374723D1 (en) * 1982-02-17 1988-01-07 British Aerospace Aircraft data instrumentation and acquisition system
US4604711A (en) * 1982-07-23 1986-08-05 Sundstrand Data Control, Inc. Aircraft flight data display system
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Also Published As

Publication number Publication date
GR3035461T3 (en) 2001-05-31
JPH07503090A (ja) 1995-03-30
IL106511A (en) 1996-10-31
DE69329751D1 (de) 2001-01-18
EP0606469B1 (en) 2000-12-13
IL106511A0 (en) 1993-12-28
NO941141D0 (no) 1994-03-28
EP0606469A4 (en) 1997-05-14
AU4996693A (en) 1994-03-03
US5377109A (en) 1994-12-27
WO1994003854A1 (en) 1994-02-17
DE69329751T2 (de) 2001-04-12
CA2120347A1 (en) 1994-02-17
PT606469E (pt) 2001-04-30
DK0606469T3 (da) 2001-04-17
EP0606469A1 (en) 1994-07-20
ATE198105T1 (de) 2000-12-15

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