DE602004015180D1 - System zur Steuerung eines Flugzeuges, zumindest zur Steuerung des Flugzeuges bei ungenauem Landeanflug und der darauf folgenden Landung - Google Patents

System zur Steuerung eines Flugzeuges, zumindest zur Steuerung des Flugzeuges bei ungenauem Landeanflug und der darauf folgenden Landung

Info

Publication number
DE602004015180D1
DE602004015180D1 DE602004015180T DE602004015180T DE602004015180D1 DE 602004015180 D1 DE602004015180 D1 DE 602004015180D1 DE 602004015180 T DE602004015180 T DE 602004015180T DE 602004015180 T DE602004015180 T DE 602004015180T DE 602004015180 D1 DE602004015180 D1 DE 602004015180D1
Authority
DE
Germany
Prior art keywords
aircraft
controlling
landing
approach
imprecise
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
DE602004015180T
Other languages
English (en)
Inventor
Gilles Tatham
Eric Peyrucain
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 DE602004015180D1 publication Critical patent/DE602004015180D1/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
    • G05D1/04—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

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)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Traffic Control Systems (AREA)
  • Radar Systems Or Details Thereof (AREA)
DE602004015180T 2003-03-19 2004-02-26 System zur Steuerung eines Flugzeuges, zumindest zur Steuerung des Flugzeuges bei ungenauem Landeanflug und der darauf folgenden Landung Expired - Lifetime DE602004015180D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0303336A FR2852686B1 (fr) 2003-03-19 2003-03-19 Systeme de pilotage d'un aeronef, au moins pour piloter l'aeronef lors d'une approche de non precision en vue d'un atterrissage.

Publications (1)

Publication Number Publication Date
DE602004015180D1 true DE602004015180D1 (de) 2008-09-04

Family

ID=32799686

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004015180T Expired - Lifetime DE602004015180D1 (de) 2003-03-19 2004-02-26 System zur Steuerung eines Flugzeuges, zumindest zur Steuerung des Flugzeuges bei ungenauem Landeanflug und der darauf folgenden Landung

Country Status (6)

Country Link
US (1) US7715955B2 (de)
EP (1) EP1460504B1 (de)
AT (1) ATE402432T1 (de)
CA (1) CA2458965C (de)
DE (1) DE602004015180D1 (de)
FR (1) FR2852686B1 (de)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2852683B1 (fr) * 2003-03-19 2005-05-20 Airbus France Procede et dispositif d'aide au pilotage d'un aeronef lors d'une approche de non precision pendant une phase d'atterrissage.
FR2878953B1 (fr) 2004-12-03 2007-01-26 Thales Sa Architecture d'un systeme embarque d'aide au pilotage d'un aeronef
FR2888636B1 (fr) * 2005-07-13 2007-09-28 Airbus France Sas Dispositif d'aide a une approche avec guidage vertical pour aeronef
FR2896073B1 (fr) * 2006-01-11 2008-02-08 Airbus France Sas Systeme de pilotage d'un aeronef, au moins pour piloter l'aeronef lors d'une approche autonome en vue d'un atterrissage.
FR2897712B1 (fr) 2006-02-20 2008-04-04 Airbus France Sas Dispositif d'aide au pilotage d'un aeronef lors d'une phase d'approche en vue d'un atterrissage.
FR2899325B1 (fr) * 2006-03-29 2009-06-05 Airbus France Sas Systeme de guidage d'un aeronef.
FR2908904B1 (fr) * 2006-11-21 2009-02-06 Airbus France Sa Systeme de pilotage d'un aeronef comportant une base de donnees aeronautique.
FR2927455B1 (fr) * 2008-02-08 2014-03-21 Thales Sa Procedes d'optimisation de la localisation d'un aeronef au sol et en phases de decollage et d'atterrissage
DE102008033235A1 (de) * 2008-07-15 2010-03-11 Astrium Gmbh Verfahren zum automatischen Ermitteln einer Landebahn
US8615337B1 (en) * 2008-09-25 2013-12-24 Rockwell Collins, Inc. System supporting flight operations under instrument meteorological conditions using precision course guidance
US8121747B2 (en) * 2009-08-05 2012-02-21 Honeywell International Inc. Flight management system, process, and program product enabling dynamic switching between non-precision approach modes
FR2989174B1 (fr) * 2012-04-06 2016-12-09 Thales Sa Dispositif pour la determination d'informations de localisation et de references primaires inertielles pour un aeronef
FR2990527B1 (fr) 2012-05-09 2014-05-23 Airbus Operations Sas Procede et dispositif d'aide a la gestion du vol d'un aeronef lors d'une phase d'atterrissage.
US8712609B2 (en) 2012-05-14 2014-04-29 Honeywell International Inc. Methods and systems for representing missed approach information in perspective view on a cockpit display
KR101715336B1 (ko) * 2014-10-31 2017-03-10 한국항공우주연구원 항공기 착륙을 위한 통합 착륙 수신 장치 및 그 제어 방법
FR3044810A1 (fr) * 2015-12-04 2017-06-09 Airbus Operations Sas Systeme d’aide a la gestion du vol d’un aeronef lors d’une phase d’atterrissage.
US12020583B2 (en) 2020-03-10 2024-06-25 Honeywell International Inc. Systems and methods providing assist-to-land and emergency land functions
FR3128298B1 (fr) 2021-10-20 2024-05-03 Thales Sa Système d'aide à l'atterrissage sur une zone d'atterrissage pour un aéronef à voilure tournante

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4534000A (en) * 1975-08-29 1985-08-06 Bliss John H Inertial flight director system
US5931889A (en) * 1995-01-24 1999-08-03 Massachusetts Institute Of Technology Clock-aided satellite navigation receiver system for monitoring the integrity of satellite signals
US5820080A (en) * 1996-03-14 1998-10-13 Trimble Navigation Limited Precision equivalent landing system using gps and an altimeter
US5945943A (en) * 1997-09-17 1999-08-31 Trimble Navigation System for using differential GPS receivers with autopilot systems for category III precision approaches
US6178379B1 (en) * 1997-10-31 2001-01-23 Honeywell International Inc. Method and apparatus of monitoring a navigation system using deviation signals from navigation sensors
US6239745B1 (en) * 1999-07-30 2001-05-29 Rockwell Collins, Inc. Satellite landing system having instrument landing system look alike guidance
US6263263B1 (en) * 2000-01-12 2001-07-17 Honeywell International Inc. Altitude correction for aircraft under non-ISA temperature conditions
US6570531B1 (en) * 2000-04-27 2003-05-27 Rockwell Collins, Inc. Satellite navigation receiver designed for compatibility with aircraft automatic landing systems
US7216069B2 (en) * 2001-01-19 2007-05-08 Honeywell International, Inc. Simulated visual glideslope indicator on aircraft display
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
US6711479B1 (en) * 2001-08-30 2004-03-23 Honeywell International, Inc. Avionics system for determining terminal flightpath
US7164383B2 (en) * 2002-09-25 2007-01-16 The Board Of Regents Of The University Of Oklahoma Navigation system using locally augmented GPS

Also Published As

Publication number Publication date
FR2852686B1 (fr) 2005-08-05
EP1460504B1 (de) 2008-07-23
US7715955B2 (en) 2010-05-11
CA2458965C (fr) 2011-11-29
US20040199304A1 (en) 2004-10-07
EP1460504A1 (de) 2004-09-22
CA2458965A1 (fr) 2004-09-19
ATE402432T1 (de) 2008-08-15
FR2852686A1 (fr) 2004-09-24

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