ES2188684T3 - Procedimiento de ayuda para el aterrizaje de un avion. - Google Patents

Procedimiento de ayuda para el aterrizaje de un avion.

Info

Publication number
ES2188684T3
ES2188684T3 ES96105760T ES96105760T ES2188684T3 ES 2188684 T3 ES2188684 T3 ES 2188684T3 ES 96105760 T ES96105760 T ES 96105760T ES 96105760 T ES96105760 T ES 96105760T ES 2188684 T3 ES2188684 T3 ES 2188684T3
Authority
ES
Spain
Prior art keywords
reflectors
landing
airplane
procedure
help procedure
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
ES96105760T
Other languages
English (en)
Inventor
Wilhelm Dr Gruner
Franz-Josef Tospann
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 Defence and Space GmbH
Original Assignee
EADS Deutschland GmbH
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 EADS Deutschland GmbH filed Critical EADS Deutschland GmbH
Application granted granted Critical
Publication of ES2188684T3 publication Critical patent/ES2188684T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88—Radar or analogous systems specially adapted for specific applications
    • G01S13/91—Radar or analogous systems specially adapted for specific applications for traffic control
    • G01S13/913—Radar or analogous systems specially adapted for specific applications for traffic control for landing purposes
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88—Radar or analogous systems specially adapted for specific applications
    • G01S13/93—Radar or analogous systems specially adapted for specific applications for anti-collision purposes
    • G01S13/933—Radar or analogous systems specially adapted for specific applications for anti-collision purposes of aircraft or spacecraft
    • G01S13/935—Radar or analogous systems specially adapted for specific applications for anti-collision purposes of aircraft or spacecraft for terrain-avoidance
    • 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
    • G08G5/0026—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located on the ground
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/02—Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
    • G08G5/025—Navigation or guidance aids
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q15/00—Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
    • H01Q15/14—Reflecting surfaces; Equivalent structures
    • H01Q15/18—Reflecting surfaces; Equivalent structures comprising plurality of mutually inclined plane surfaces, e.g. corner reflector
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
    • G01S13/06—Systems determining position data of a target
    • G01S13/08—Systems for measuring distance only
    • G01S13/32—Systems for measuring distance only using transmission of continuous waves, whether amplitude-, frequency-, or phase-modulated, or unmodulated
    • G01S13/34—Systems for measuring distance only using transmission of continuous waves, whether amplitude-, frequency-, or phase-modulated, or unmodulated using transmission of continuous, frequency-modulated waves while heterodyning the received signal, or a signal derived therefrom, with a locally-generated signal related to the contemporaneously transmitted signal
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/74—Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems
    • G01S13/75—Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems using transponders powered from received waves, e.g. using passive transponders, or using passive reflectors

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Electromagnetism (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Traffic Control Systems (AREA)

Abstract

LA INVENCION SE REFIERE A UN PROCEDIMIENTO PARA AYUDA DE TOMA DE TIERRA DE UN AVION. CON ELLO SE UTILIZA UN RADAR DE A BORDO FM-CW CON ALCANCE CORTO, POR EJEMPLO 5 KM, Y ALTA RESOLUCION DE ANGULO Y DE CAMPO. EN LA ZONA DE LA BANDA DE TIERRA SE APLICAN DE FORMA DEFINIDA MULTIPLES REFLECTORES DE RADAR PASIVOS, CON PREFERENCIA REFLECTORES CORNER. CON ESTOS REFLECTORES ES POSIBLE UNA NAVEGACION CON TOMA DE TIERRA, QUE CUMPLEN LAS CONDICIONES B DE CAT III.
ES96105760T 1995-04-13 1996-04-12 Procedimiento de ayuda para el aterrizaje de un avion. Expired - Lifetime ES2188684T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19513440A DE19513440A1 (de) 1995-04-13 1995-04-13 Verfahren zur Landehilfe für ein Flugzeug

Publications (1)

Publication Number Publication Date
ES2188684T3 true ES2188684T3 (es) 2003-07-01

Family

ID=7759300

Family Applications (1)

Application Number Title Priority Date Filing Date
ES96105760T Expired - Lifetime ES2188684T3 (es) 1995-04-13 1996-04-12 Procedimiento de ayuda para el aterrizaje de un avion.

Country Status (3)

Country Link
EP (1) EP0738900B1 (es)
DE (2) DE19513440A1 (es)
ES (1) ES2188684T3 (es)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19949737A1 (de) * 1999-10-15 2001-04-26 Apm Gmbh Airport Equipment Vorrichtung zur Führung von Luftfahrzeugen auf Landeplätzen
DE102014211522A1 (de) 2014-06-17 2015-12-17 Robert Bosch Gmbh Radaranordnung und Verfahren zum Bestimmen der Lage eines Luftfahrzeugs bezüglich einer Landeplattform
FR3103178B1 (fr) * 2019-11-20 2022-12-30 Thales Sa Procede d'aide a l'atterrissage d'un aeronef sur une piste d'atterrissage

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3243816A (en) * 1962-06-08 1966-03-29 Sierra Research Corp Final approach landing system
US3716855A (en) * 1970-07-15 1973-02-13 Texas Instruments Inc Glideslope position detection system for use with an independent aircraft landing monitor
DE3644478A1 (de) * 1986-12-24 1988-07-07 Licentia Gmbh System fuer landehilfe fuer flugzeuge mit eigenem bordradar
US5208601A (en) * 1990-07-24 1993-05-04 The United States Of America As Represented By The Secretary Of The Navy All-weather precision landing system for aircraft in remote areas
DE4243669A1 (de) * 1992-12-23 1994-06-30 Deutsche Aerospace Verfahren zur Überwachung eines Gebietes und Anordnung zur Durchführung des Verfahrens
US5483241A (en) * 1994-05-09 1996-01-09 Rockwell International Corporation Precision location of aircraft using ranging

Also Published As

Publication number Publication date
EP0738900A1 (de) 1996-10-23
EP0738900B1 (de) 2002-12-18
DE19513440A1 (de) 1996-10-17
DE59609984D1 (de) 2003-01-30

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