DE602005001801D1 - Steuerungsanzeige mit Ermittlung der maximalen Steigung zum Steuern eines Flugzeuges im Bodenfolgeflug - Google Patents

Steuerungsanzeige mit Ermittlung der maximalen Steigung zum Steuern eines Flugzeuges im Bodenfolgeflug

Info

Publication number
DE602005001801D1
DE602005001801D1 DE602005001801T DE602005001801T DE602005001801D1 DE 602005001801 D1 DE602005001801 D1 DE 602005001801D1 DE 602005001801 T DE602005001801 T DE 602005001801T DE 602005001801 T DE602005001801 T DE 602005001801T DE 602005001801 D1 DE602005001801 D1 DE 602005001801D1
Authority
DE
Germany
Prior art keywords
aircraft
determination
controlling
maximum gradient
control display
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
DE602005001801T
Other languages
English (en)
Other versions
DE602005001801T2 (de
Inventor
Franck Artini
Jean-Pierre Demortier
Christophe Bouchet
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of DE602005001801D1 publication Critical patent/DE602005001801D1/de
Application granted granted Critical
Publication of DE602005001801T2 publication Critical patent/DE602005001801T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • G05D1/04—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
    • G05D1/0646—Rate of change of altitude or depth specially adapted for aircraft to follow the profile of undulating ground
    • 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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D7/00—Indicating measured values
    • G01D7/02—Indicating value of two or more variables simultaneously
    • G01D7/08—Indicating value of two or more variables simultaneously using a common indicating element for two or more variables
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D2207/00—Indexing scheme relating to details of indicating measuring values
    • G01D2207/10—Displays which are primarily used in aircraft or display aircraft-specific information
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D2207/00—Indexing scheme relating to details of indicating measuring values
    • G01D2207/20—Displays for vehicles in which information is superimposed on an external view, e.g. heads-up displays or enhanced reality displays

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
DE602005001801T 2004-05-18 2005-04-04 Steuerungsanzeige mit Ermittlung der maximalen Steigung zum Steuern eines Flugzeuges im Bodenfolgeflug Active DE602005001801T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0405375 2004-05-18
FR0405375A FR2870514B1 (fr) 2004-05-18 2004-05-18 Indicateur de pilotage determinant la pente maximale pour le pilotage d'un aeronef en suivi de terrain

Publications (2)

Publication Number Publication Date
DE602005001801D1 true DE602005001801D1 (de) 2007-09-13
DE602005001801T2 DE602005001801T2 (de) 2008-04-17

Family

ID=34942063

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005001801T Active DE602005001801T2 (de) 2004-05-18 2005-04-04 Steuerungsanzeige mit Ermittlung der maximalen Steigung zum Steuern eines Flugzeuges im Bodenfolgeflug

Country Status (6)

Country Link
US (1) US7089090B2 (de)
EP (1) EP1598720B1 (de)
AT (1) ATE368881T1 (de)
CA (1) CA2503036C (de)
DE (1) DE602005001801T2 (de)
FR (1) FR2870514B1 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2878060B1 (fr) * 2004-11-15 2010-11-05 Airbus France Procede et dispositif d'alerte et d'evitement de terrain pour un aeronef
FR2887065B1 (fr) * 2005-06-14 2007-07-20 Airbus France Sas Procede et systeme d'aide au pilotage d'un aeronef volant a basse altitude
FR2889342B1 (fr) * 2005-07-26 2010-11-19 Airbus France Procede et dispositif de detection d'un risque de collision d'un aeronef avec le terrain environnant
FR2958050B1 (fr) 2010-03-24 2012-12-28 Dassault Aviat Procede et systeme de gestion de la variation d'energie d'un aeronef
FR2958033B1 (fr) 2010-03-24 2012-05-25 Dassault Aviat Dispositif d'affichage de la variation d'energie d'un aeronef, procede et systeme d'affichage de la variation d'energie correspondants
FR2978586B1 (fr) 2011-07-27 2013-07-26 Eurocopter France Procede d'aide au pilotage, dispositif d'aide au pilotage, et aeronef
FR3020478B1 (fr) * 2014-04-28 2016-05-20 Airbus Operations Sas Procede et ensemble de guidage d'un aeronef lors d'un vol a basse hauteur.
US9296490B2 (en) 2014-08-25 2016-03-29 Honeywell International Inc. Aircraft operating and position information display system and method
FR3033886B1 (fr) 2015-03-18 2017-04-21 Dassault Aviat Dispositif d' affichage d'une variation d'energie et d'une borne de variation d'energie d'un aeronef

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5353022A (en) * 1987-08-06 1994-10-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Airplane takeoff and landing performance monitoring system
US5796612A (en) * 1992-11-18 1998-08-18 Aers/Midwest, Inc. Method for flight parameter monitoring and control
FR2733061B1 (fr) * 1995-04-13 1997-05-23 Sextant Avionique Dispositif optoelectronique d'aide au pilotage d'un aeronef par mauvaise visibilite
US6691004B2 (en) * 1995-07-31 2004-02-10 Honeywell International, Inc. Method for determining a currently obtainable climb gradient of an aircraft
GB2310184B (en) * 1996-02-19 2000-10-11 Marconi Gec Ltd Aircraft terrain advisory system
CA2202409C (en) * 1997-04-11 1998-04-07 Carl W. Millard Howgozit airspeed indicator system
US6486799B1 (en) * 1999-07-19 2002-11-26 The University Of West Florida Computer based human-centered display system
US6675328B1 (en) * 1999-10-08 2004-01-06 Vigilant Networks, Llc System and method to determine data throughput in a communication network
US6262674B1 (en) * 2000-08-10 2001-07-17 Honeywell International Inc. Aircraft display with potential thrust indicator
FR2831871B1 (fr) * 2001-11-08 2004-08-13 Airbus France Procede et dispositif d'aide au pilotage d'un aeronef

Also Published As

Publication number Publication date
CA2503036C (fr) 2013-02-12
EP1598720B1 (de) 2007-08-01
US7089090B2 (en) 2006-08-08
CA2503036A1 (fr) 2005-11-18
DE602005001801T2 (de) 2008-04-17
FR2870514A1 (fr) 2005-11-25
US20050273221A1 (en) 2005-12-08
EP1598720A1 (de) 2005-11-23
ATE368881T1 (de) 2007-08-15
FR2870514B1 (fr) 2006-07-28

Similar Documents

Publication Publication Date Title
DE602005001801D1 (de) Steuerungsanzeige mit Ermittlung der maximalen Steigung zum Steuern eines Flugzeuges im Bodenfolgeflug
EP2128842A3 (de) Anwenderhilfsverfahren und Systeme
ATE353136T1 (de) Verfahren und vorrichtung zum abändern eines flugplanes eines flugzeuges
CA2557405C (fr) Dispositif optoelectronique securise d'aide au roulage pour aeronef
ATE372925T1 (de) Steuerungsanzeige zum anzeigen von schubinformationen eines luftfahrzeuges
DE602007001136D1 (de) Vorrichtung zur unterstützung der flugzeuglenkung in der landeanflugsphase zum landen
ATE445873T1 (de) Verfahren und einrichtung zum sichern eines automatischen fluges eines flugzeugs auf niedriger höhe
CN105894855A (zh) 危险驾驶的提示方法及装置
TR201906392T4 (tr) Bir döner kanatlı uçağın karaya indirilmesine yönelik aparat ve yöntem.
EP2568257B1 (de) System und Verfahren zum Anzeigen der Fluggeschwindigkeit für ein Flugzeug
FR2935179B1 (fr) Procede et dispositif d'aide au controle des systemes embarques dans un aeronef
ATE408876T1 (de) Vermeidung von geländekollisionen von flugzeugen sowie alarmverfahren und -vorrichtung
WO2006134256A3 (fr) Procede et systeme d’aide au pilotage d’un aeronef volant a basse altitude
WO2008060260A3 (en) System and method for increasing visibility of critical flight information on aircraft displays
WO2005013204A3 (en) Flight situation presentation system and method
ATE393421T1 (de) Hilfssystem zur verzögerungssteuerung eines flugzeuges im rollvorgang
DE602007010255D1 (de) Flugzeuglenkwinkelwarnsystem
GB201112569D0 (en) Tractor control/display systems
ATE400864T1 (de) System zum unterstützen der bodennavigation eines flugzeugs auf einem flughafen
US9895941B2 (en) Aircraft tire pressure monitoring system
KR20070011660A (ko) 항공기 훈련용 시뮬레이터 및 항공기용 블랙박스 분석용영상정보 표시장치 및 그 운용방법
FR2919066B1 (fr) Instrument de secours pour aeronef
CA2457772A1 (fr) Indicateur d'attitude pour aeronef
ATE555938T1 (de) Flugzeugsteuerungsanzeige zum anzeigen der schuberzeugung von mindestens einem flugzeugmotor
DE60307928D1 (de) Vorrichtung zur Unterstützung der visuellen Postionsbestimmung eines Flugzeuges während des Fluges

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
R082 Change of representative

Ref document number: 1598720

Country of ref document: EP

Representative=s name: MEISSNER & MEISSNER, 14199 BERLIN, DE