DE60132896D1 - Detektion eines flugzeugstarts mit geringer leistung zum verwenden in einem bodennäherungswarnsystem - Google Patents

Detektion eines flugzeugstarts mit geringer leistung zum verwenden in einem bodennäherungswarnsystem

Info

Publication number
DE60132896D1
DE60132896D1 DE60132896T DE60132896T DE60132896D1 DE 60132896 D1 DE60132896 D1 DE 60132896D1 DE 60132896 T DE60132896 T DE 60132896T DE 60132896 T DE60132896 T DE 60132896T DE 60132896 D1 DE60132896 D1 DE 60132896D1
Authority
DE
Germany
Prior art keywords
climb rate
component
low performance
potential
aircraft
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
DE60132896T
Other languages
English (en)
Other versions
DE60132896T2 (de
Inventor
Steven Johnson
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 International Inc
Original Assignee
Honeywell International 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 International Inc filed Critical Honeywell International Inc
Publication of DE60132896D1 publication Critical patent/DE60132896D1/de
Application granted granted Critical
Publication of DE60132896T2 publication Critical patent/DE60132896T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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
    • G05D1/04—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
    • G05D1/0661—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
    • G08G5/0021—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located in the aircraft
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0047—Navigation or guidance aids for a single aircraft
    • G08G5/0065—Navigation or guidance aids for a single aircraft for taking-off
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0073—Surveillance aids
    • G08G5/0086—Surveillance aids for monitoring terrain
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/04—Anti-collision systems
    • G08G5/045—Navigation or guidance aids, e.g. determination of anti-collision manoeuvers

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Emergency Alarm Devices (AREA)
  • Other Investigation Or Analysis Of Materials By Electrical Means (AREA)
  • Developing Agents For Electrophotography (AREA)
  • Underground Structures, Protecting, Testing And Restoring Foundations (AREA)
  • Traffic Control Systems (AREA)
DE60132896T 2000-07-24 2001-07-23 Detektion eines flugzeugstarts mit geringer leistung zum verwenden in einem bodennäherungswarnsystem Expired - Lifetime DE60132896T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US22025700P 2000-07-24 2000-07-24
US220257P 2000-07-24
PCT/US2001/023387 WO2002039060A2 (en) 2000-07-24 2001-07-23 Detecting a low performance takeoff condition for aircraft for use with ground proximity warning systems

Publications (2)

Publication Number Publication Date
DE60132896D1 true DE60132896D1 (de) 2008-04-03
DE60132896T2 DE60132896T2 (de) 2009-02-12

Family

ID=22822782

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60132896T Expired - Lifetime DE60132896T2 (de) 2000-07-24 2001-07-23 Detektion eines flugzeugstarts mit geringer leistung zum verwenden in einem bodennäherungswarnsystem

Country Status (6)

Country Link
US (1) US6437707B1 (de)
EP (1) EP1303737B1 (de)
JP (1) JP2004513025A (de)
AT (1) ATE386922T1 (de)
DE (1) DE60132896T2 (de)
WO (1) WO2002039060A2 (de)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4328660B2 (ja) * 2004-04-15 2009-09-09 富士重工業株式会社 航空機の自動離陸装置、自動着陸装置及び自動離着陸装置並びに航空機の自動離陸方法、自動着陸方法及び自動離着陸方法
FR2870607B1 (fr) * 2004-05-18 2006-08-11 Airbus France Sas Procede et dispositif pour construire une trajectoire de vol a basse altitude destinee a etre suivie par un aeronef
FR2870517B1 (fr) * 2004-05-18 2006-07-28 Airbus France Sas Procede et dispositif de securisation d'un vol a basse altitude d'un aeronef
FR2870604B1 (fr) * 2004-05-18 2006-08-11 Airbus France Sas Procede et dispositif de securisation d'un vol a basse altitude d'un aeronef
FR2879562B1 (fr) * 2004-12-20 2008-05-16 Airbus France Sas Dispositif pour emettre une autorisation d'agir sur le fonctionnement d'un moteur d'aeronef et systeme de controle de moteur comportant un tel dispositif
US7626514B2 (en) * 2006-06-23 2009-12-01 Honeywell International Inc. Systems and methods for reducing nuisance alerts for helicopter enhanced ground proximity warning systems
US8615335B2 (en) * 2008-09-17 2013-12-24 The Boeing Company Progressive takeoff thrust ramp for an aircraft
US10340034B2 (en) 2011-12-30 2019-07-02 Elwha Llc Evidence-based healthcare information management protocols
US10475142B2 (en) 2011-12-30 2019-11-12 Elwha Llc Evidence-based healthcare information management protocols
US20130173294A1 (en) 2011-12-30 2013-07-04 Elwha LLC, a limited liability company of the State of Delaware Evidence-based healthcare information management protocols
US10528913B2 (en) 2011-12-30 2020-01-07 Elwha Llc Evidence-based healthcare information management protocols
US10679309B2 (en) 2011-12-30 2020-06-09 Elwha Llc Evidence-based healthcare information management protocols
US10559380B2 (en) 2011-12-30 2020-02-11 Elwha Llc Evidence-based healthcare information management protocols
US10552581B2 (en) 2011-12-30 2020-02-04 Elwha Llc Evidence-based healthcare information management protocols
US9164505B1 (en) * 2012-05-22 2015-10-20 The Boeing Company Automatic rejected takeoff system
US10228692B2 (en) 2017-03-27 2019-03-12 Gulfstream Aerospace Corporation Aircraft flight envelope protection and recovery autopilot
CN109979247A (zh) * 2019-04-18 2019-07-05 西安希德雷达科技有限公司 一种基于飞机飞行性能的近地告警方法
US11822352B2 (en) 2020-10-26 2023-11-21 Rockwell Collins, Inc. Engine out go around vertical clearance system and method

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3681580A (en) * 1969-08-01 1972-08-01 Teledyne Inc Rotation,climbout,and go-around control system
US3614728A (en) * 1970-03-06 1971-10-19 Mc Donnell Douglas Corp Indicator means for collision avoidance systems
US3934222A (en) * 1975-04-02 1976-01-20 Sundstrand Data Control, Inc. Terrain closure warning system with climb inhibit and altitude gain measurement
US5220322A (en) * 1984-07-18 1993-06-15 Sundstrand Corporation Ground proximity warning system for use with aircraft having egraded performance
GB9111086D0 (en) * 1991-05-22 1991-10-16 Marconi Gec Ltd Aircraft terrain and obstacle avoidance system
FR2689668B1 (fr) * 1992-04-07 1994-05-20 Dassault Electronique Procede et dispositif d'anti-collisions terrain pour aeronef.
DE69606804T2 (de) * 1995-06-20 2000-06-15 Honeywell Inc Integriertes System zur Grundkollisionsvermeidung
US6092009A (en) * 1995-07-31 2000-07-18 Alliedsignal Aircraft terrain information system

Also Published As

Publication number Publication date
WO2002039060A3 (en) 2003-01-09
EP1303737B1 (de) 2008-02-20
US20020021230A1 (en) 2002-02-21
EP1303737A2 (de) 2003-04-23
JP2004513025A (ja) 2004-04-30
US6437707B1 (en) 2002-08-20
ATE386922T1 (de) 2008-03-15
WO2002039060A2 (en) 2002-05-16
DE60132896T2 (de) 2009-02-12

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