DE69726595D1 - Verfahren und vorrichtung für konforme landebahnausrichtung für eine head-up-anzeige - Google Patents

Verfahren und vorrichtung für konforme landebahnausrichtung für eine head-up-anzeige

Info

Publication number
DE69726595D1
DE69726595D1 DE69726595T DE69726595T DE69726595D1 DE 69726595 D1 DE69726595 D1 DE 69726595D1 DE 69726595 T DE69726595 T DE 69726595T DE 69726595 T DE69726595 T DE 69726595T DE 69726595 D1 DE69726595 D1 DE 69726595D1
Authority
DE
Germany
Prior art keywords
compliant
head
display
runway orientation
runway
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
DE69726595T
Other languages
English (en)
Other versions
DE69726595T2 (de
Inventor
R Wilkens
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
Application granted granted Critical
Publication of DE69726595D1 publication Critical patent/DE69726595D1/de
Publication of DE69726595T2 publication Critical patent/DE69726595T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C23/00—Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
    • G01C23/005—Flight directors
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/01—Head-up displays
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/0083—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot to help an aircraft pilot in the rolling phase
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/01—Head-up displays
    • G02B27/0179—Display position adjusting means not related to the information to be displayed
    • G02B2027/0187—Display position adjusting means not related to the information to be displayed slaved to motion of at least a part of the body of the user, e.g. head, eye
DE69726595T 1996-11-18 1997-10-23 Verfahren und vorrichtung für konforme landebahnausrichtung für eine head-up-anzeige Expired - Fee Related DE69726595T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US08/751,444 US5745054A (en) 1996-11-18 1996-11-18 Method and apparatus for conformal runway alignment on a head up display
US751444 1996-11-18
PCT/US1997/018953 WO1998022780A1 (en) 1996-11-18 1997-10-23 Method and apparatus for conformal runway alignment on a head up display

Publications (2)

Publication Number Publication Date
DE69726595D1 true DE69726595D1 (de) 2004-01-15
DE69726595T2 DE69726595T2 (de) 2004-11-11

Family

ID=25022004

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69726595T Expired - Fee Related DE69726595T2 (de) 1996-11-18 1997-10-23 Verfahren und vorrichtung für konforme landebahnausrichtung für eine head-up-anzeige

Country Status (4)

Country Link
US (1) US5745054A (de)
EP (1) EP0938645B1 (de)
DE (1) DE69726595T2 (de)
WO (1) WO1998022780A1 (de)

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US6731226B2 (en) * 2001-12-04 2004-05-04 Smiths Aerospace, Inc. Airport feature display system and data interchange method for conformal display
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US7650232B1 (en) * 2005-09-22 2010-01-19 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration (Nasa) Trajectory specification for high capacity air traffic control
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US7689326B2 (en) * 2006-02-02 2010-03-30 Honeywell International Inc. Heading awareness symbology for track centered primary flight displays
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US8386167B2 (en) * 2008-11-14 2013-02-26 The Boeing Company Display of taxi route control point information
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US20100127896A1 (en) * 2008-11-21 2010-05-27 Bland Hugh Schwarting Optical path alignment landing system
KR20100070973A (ko) * 2008-12-18 2010-06-28 박호철 헤드업 디스플레이 내비게이션 장치, 시스템 및 서비스 구현방법
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US8264379B2 (en) * 2009-03-10 2012-09-11 Honeywell International Inc. Methods and systems for correlating data sources for vehicle displays
FR2948468B1 (fr) * 2009-07-23 2011-09-16 Airbus Operations Sas Procede et dispositif d'aide au controle lateral d'aeronef lors d'une phase d'approche
US8487787B2 (en) 2010-09-30 2013-07-16 Honeywell International Inc. Near-to-eye head tracking ground obstruction system and method
US9092975B2 (en) * 2011-02-23 2015-07-28 Honeywell International Inc. Aircraft systems and methods for displaying visual segment information
US9139307B2 (en) 2013-06-28 2015-09-22 Honeywell International Inc. Aircraft systems and methods for displaying runway lighting information
US9098999B2 (en) * 2013-09-13 2015-08-04 The Boeing Company Systems and methods for assuring the accuracy of a synthetic runway presentation
CN105513106B (zh) * 2015-12-05 2018-08-17 中国航空工业集团公司洛阳电光设备研究所 一种平显等角跑道符号绘制方法
US10175694B2 (en) 2016-11-01 2019-01-08 The Boeing Company Flight control system with synthetic inertial localizer deviation and method of use
US10203693B2 (en) 2016-11-01 2019-02-12 The Boeing Company Flight control system with synthetic inertial glideslope deviation and method of use
US10089892B2 (en) 2016-11-01 2018-10-02 The Boeing Company Flight control system with low-frequency instrument landing system localizer anomaly detection and method of use
FR3061794B1 (fr) * 2017-01-06 2019-05-24 Thales Dispositif electronique de surveillance d'au moins un signal de radionavigation en phase d'approche d'une piste d'atterrissage, procede de surveillance et programme d'ordinateur associes
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CN111596680A (zh) * 2020-06-03 2020-08-28 中国商用飞机有限责任公司 飞行器自动飞行控制方法和系统

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Also Published As

Publication number Publication date
EP0938645A1 (de) 1999-09-01
WO1998022780A1 (en) 1998-05-28
US5745054A (en) 1998-04-28
DE69726595T2 (de) 2004-11-11
EP0938645B1 (de) 2003-12-03

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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