DE69715401T2 - Strukturierte datenleitweglenkung verwendendes flugverwaltungssystem für automatische steuerungsanzeigeeinheit - Google Patents

Strukturierte datenleitweglenkung verwendendes flugverwaltungssystem für automatische steuerungsanzeigeeinheit

Info

Publication number
DE69715401T2
DE69715401T2 DE69715401T DE69715401T DE69715401T2 DE 69715401 T2 DE69715401 T2 DE 69715401T2 DE 69715401 T DE69715401 T DE 69715401T DE 69715401 T DE69715401 T DE 69715401T DE 69715401 T2 DE69715401 T2 DE 69715401T2
Authority
DE
Germany
Prior art keywords
display unit
management system
automatic control
control display
structured data
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 - Lifetime
Application number
DE69715401T
Other languages
English (en)
Other versions
DE69715401D1 (de
Inventor
D Hayes
D Gunn
A Herald
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Priority claimed from PCT/US1997/008117 external-priority patent/WO1997043704A1/en
Publication of DE69715401D1 publication Critical patent/DE69715401D1/de
Application granted granted Critical
Publication of DE69715401T2 publication Critical patent/DE69715401T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Navigation (AREA)
DE69715401T 1996-05-14 1997-05-14 Strukturierte datenleitweglenkung verwendendes flugverwaltungssystem für automatische steuerungsanzeigeeinheit Expired - Lifetime DE69715401T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US1787496P 1996-05-14 1996-05-14
US08/854,645 US6112140A (en) 1996-05-14 1997-05-12 Flight management system providing for automatic control display unit backup utilizing structured data routing
PCT/US1997/008117 WO1997043704A1 (en) 1996-05-14 1997-05-14 Flight management system providing for automatic control display unit backup utilizing structured data routing

Publications (2)

Publication Number Publication Date
DE69715401D1 DE69715401D1 (de) 2002-10-17
DE69715401T2 true DE69715401T2 (de) 2003-05-15

Family

ID=56289766

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69715401T Expired - Lifetime DE69715401T2 (de) 1996-05-14 1997-05-14 Strukturierte datenleitweglenkung verwendendes flugverwaltungssystem für automatische steuerungsanzeigeeinheit

Country Status (2)

Country Link
US (1) US6112140A (de)
DE (1) DE69715401T2 (de)

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US6799095B1 (en) * 1999-09-08 2004-09-28 Rockwell Collins Method and apparatus for interactively displaying a route window for a flight management system
US6317659B1 (en) * 1999-12-09 2001-11-13 Honeywell International Inc. Layered subsystem architecture for a flight management system
EP1299784B1 (de) * 2000-07-10 2004-05-06 Honeywell International Inc. Aus blöcken zusammengesetzte flüssigkristallanzeige
US6401013B1 (en) * 2000-07-11 2002-06-04 Rockwell Collins, Inc. Method and system for integrating a laptop PC in a cockpit
US6789007B2 (en) * 2001-06-25 2004-09-07 The Boeing Company Integrated onboard maintenance documentation with a central maintenance system
US6571155B2 (en) 2001-07-02 2003-05-27 The Boeing Company Assembly, computer program product and method for displaying navigation performance based flight path deviation information
US6853315B2 (en) * 2002-01-23 2005-02-08 Triad Sensors, Inc. Piezoelectric rate sensor system and method
US6985801B1 (en) 2002-02-28 2006-01-10 Garmin International, Inc. Cockpit instrument panel systems and methods with redundant flight data display
US6832138B1 (en) 2002-02-28 2004-12-14 Garmin International, Inc. Cockpit instrument panel systems and methods with redundant flight data display
EP1537609A2 (de) * 2002-09-04 2005-06-08 Triad Sensors Inc. Interface-elektronik für piezoelektrische bauelemente
US6922625B2 (en) 2002-12-12 2005-07-26 Honeywell International Inc. Jet engine control and protection system and method
US20040159166A1 (en) * 2003-02-13 2004-08-19 Schiller Peter J. Solid-state piezoelectric motion transducer
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US7209809B2 (en) * 2003-10-15 2007-04-24 The Boeing Company Method and apparatus for obtaining high integrity and availability in multi-channel systems
US7392426B2 (en) * 2004-06-15 2008-06-24 Honeywell International Inc. Redundant processing architecture for single fault tolerance
US20070067074A1 (en) * 2005-08-19 2007-03-22 Honeywell International Inc. Reconfigurable algorithmic networks implemented via a flight data recorder
FR2892092B1 (fr) * 2005-10-18 2009-03-13 Airbus France Sas Systeme d'affichage pour un aeronef.
US7825890B2 (en) * 2006-01-19 2010-11-02 International Business Machines Corporation Apparatus, system and method of providing auto-dimming and state transition signal functionality to telephone systems
US8947297B2 (en) * 2006-01-30 2015-02-03 The Invention Science Fund I, Llc Positional display elements
US8151024B2 (en) * 2009-05-28 2012-04-03 Honeywell International Inc. Reconfigurable virtual backplane systems and methods
US20120215384A1 (en) * 2009-10-30 2012-08-23 Emerald Sky Technologies, LLC Flight Control System with Dynamic Allocation of Functionality Between Flight Crew and Automation
FR2962561B1 (fr) * 2010-07-09 2013-03-08 Thales Sa Systeme de visualisation comportant un dispositif d'affichage de secours
FR2967274B1 (fr) * 2010-11-05 2012-12-07 Thales Sa Procede de determination d'un equipement "leader" dans un environnement asynchrone comprenant une pluralite d'equipements electroniques
US8744650B1 (en) * 2011-03-17 2014-06-03 The Boeing Company Aircraft control system
US9922651B1 (en) * 2014-08-13 2018-03-20 Rockwell Collins, Inc. Avionics text entry, cursor control, and display format selection via voice recognition
US8761971B2 (en) * 2012-01-11 2014-06-24 The Boeing Company Auto-flight system pilot interface
US9696878B2 (en) 2014-07-21 2017-07-04 Honeywell International Inc. System and method for abstracting a display
US9701398B2 (en) 2014-11-03 2017-07-11 Douglas Allen SCHULTZ Method and apparatus for augmented pilot operations of fly-by-wire vehicles
FR3037136B1 (fr) * 2015-06-08 2017-05-19 Airbus Operations Sas Systeme et procede d'affichage d'un aeronef
CN106468911B (zh) * 2015-08-20 2019-06-28 陕西千山航空电子有限责任公司 一种用于故障诊断的故障信息备份方法
US10466949B2 (en) * 2015-09-14 2019-11-05 Bell Helicopter Textron Inc. Ballistic-resistant cockpit display
US20170323239A1 (en) 2016-05-06 2017-11-09 General Electric Company Constrained time computing control system to simulate and optimize aircraft operations with dynamic thermodynamic state and asset utilization attainment
US10496351B2 (en) 2017-06-07 2019-12-03 Ge Aviation Systems Llc Automatic display unit backup during failures of one more display units through the utilization of graphic user interface objects defined for control transfer and reversion after resolution of the failures
US11232207B2 (en) * 2018-10-01 2022-01-25 Textron Innovations Inc. Decentralized trust assessment

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Also Published As

Publication number Publication date
DE69715401D1 (de) 2002-10-17
US6112140A (en) 2000-08-29

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