ATE338296T1 - Verfahren zum leiten eines flugzeuges während der endphase der landung und dazugehörige vorrichtung - Google Patents

Verfahren zum leiten eines flugzeuges während der endphase der landung und dazugehörige vorrichtung

Info

Publication number
ATE338296T1
ATE338296T1 AT03352001T AT03352001T ATE338296T1 AT E338296 T1 ATE338296 T1 AT E338296T1 AT 03352001 T AT03352001 T AT 03352001T AT 03352001 T AT03352001 T AT 03352001T AT E338296 T1 ATE338296 T1 AT E338296T1
Authority
AT
Austria
Prior art keywords
aircraft
landing
guiding
ground
final stage
Prior art date
Application number
AT03352001T
Other languages
English (en)
Inventor
Paul Henry Robert
Guy Juanole
Michel Devy
Original Assignee
Airbus France
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 France filed Critical Airbus France
Application granted granted Critical
Publication of ATE338296T1 publication Critical patent/ATE338296T1/de

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)
  • Traffic Control Systems (AREA)
  • Closed-Circuit Television Systems (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Image Processing (AREA)
  • Radio Relay Systems (AREA)
AT03352001T 2002-01-25 2003-01-21 Verfahren zum leiten eines flugzeuges während der endphase der landung und dazugehörige vorrichtung ATE338296T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0200928A FR2835314B1 (fr) 2002-01-25 2002-01-25 Procede de guidage d'un aeronef en phase finale d'atterrissage et dispositif correspondant

Publications (1)

Publication Number Publication Date
ATE338296T1 true ATE338296T1 (de) 2006-09-15

Family

ID=27589582

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03352001T ATE338296T1 (de) 2002-01-25 2003-01-21 Verfahren zum leiten eines flugzeuges während der endphase der landung und dazugehörige vorrichtung

Country Status (7)

Country Link
US (1) US6952632B2 (de)
EP (1) EP1335258B1 (de)
AT (1) ATE338296T1 (de)
CA (1) CA2418243C (de)
DE (1) DE60307911T2 (de)
ES (1) ES2271508T3 (de)
FR (1) FR2835314B1 (de)

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US8284997B2 (en) * 2009-03-11 2012-10-09 Honeywell International Inc. Vision-based vehicle navigation system and method
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KR101050730B1 (ko) * 2010-07-30 2011-07-20 엘아이지넥스원 주식회사 활주로 보조선 기반의 무인 항공기 위치 제어장치 및 그 제어방법
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Also Published As

Publication number Publication date
CA2418243A1 (fr) 2003-07-25
CA2418243C (fr) 2011-03-15
DE60307911D1 (de) 2006-10-12
EP1335258A1 (de) 2003-08-13
EP1335258B1 (de) 2006-08-30
FR2835314B1 (fr) 2004-04-30
US20030225487A1 (en) 2003-12-04
US6952632B2 (en) 2005-10-04
FR2835314A1 (fr) 2003-08-01
DE60307911T2 (de) 2007-04-12
ES2271508T3 (es) 2007-04-16

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