FR2410828A1 - Dispositif de guidage d'aeronefs a l'atterrissage - Google Patents

Dispositif de guidage d'aeronefs a l'atterrissage

Info

Publication number
FR2410828A1
FR2410828A1 FR7834252A FR7834252A FR2410828A1 FR 2410828 A1 FR2410828 A1 FR 2410828A1 FR 7834252 A FR7834252 A FR 7834252A FR 7834252 A FR7834252 A FR 7834252A FR 2410828 A1 FR2410828 A1 FR 2410828A1
Authority
FR
France
Prior art keywords
track
landing
guidance device
aircraft guidance
network
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.)
Granted
Application number
FR7834252A
Other languages
English (en)
Other versions
FR2410828B1 (fr
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.)
Toshiba Corp
Original Assignee
Tokyo Shibaura Electric Co Ltd
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 Tokyo Shibaura Electric Co Ltd filed Critical Tokyo Shibaura Electric Co Ltd
Publication of FR2410828A1 publication Critical patent/FR2410828A1/fr
Application granted granted Critical
Publication of FR2410828B1 publication Critical patent/FR2410828B1/fr
Granted legal-status Critical Current

Links

Classifications

    • 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
    • G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
    • G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves
    • G01S1/08—Systems for determining direction or position line
    • G01S1/14—Systems for determining direction or position line using amplitude comparison of signals transmitted simultaneously from antennas or antenna systems having differently oriented overlapping directivity-characteristics
    • G01S1/16—Azimuthal guidance systems, e.g. system for defining aircraft approach path, localiser system

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Traffic Control Systems (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

L'INVENTION CONCERNE UN DISPOSITIF DE GUIDAGE D'AERONEFS A L'ATTERRISSAGE. CE DISPOSITIF COMPREND UN RESEAU 13 D'ANTENNES ELEMENTAIRES DISPOSEES SUIVANT UNE LIGNE QUI COUPE LA DIRECTION D'UNE PISTE 12 SENSIBLEMENT A ANGLE DROIT EN SON MILIEU. LES SIGNAUX DE BANDES LATERALES ET LES SIGNAUX D'ONDE PORTEUSE SONT DEPHASES A DES TAUX PRESENTANT ENTRE EUX DES RELATIONS TELLES QUE LES DIAGRAMMES DE RAYONNEMENT CORRESPONDANTS SONT EMIS PAR LE RESEAU D'ANTENNES 13 SUIVANT DES ANGLES HORIZONTAUX PRESCRITS TH PAR RAPPORT A LA COURSE DE LA PISTE. CE DISPOSITIF DE GUIDAGE EST PARTICULIEREMENT DESTINE AUX AERODROMES PLACES DANS DES SITES ENCAISSES, OU LA PLACE MANQUE EN LONGUEUR.
FR7834252A 1977-12-05 1978-12-05 Dispositif de guidage d'aeronefs a l'atterrissage Granted FR2410828A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP52145808A JPS602628B2 (ja) 1977-12-05 1977-12-05 航空機着陸誘導装置

Publications (2)

Publication Number Publication Date
FR2410828A1 true FR2410828A1 (fr) 1979-06-29
FR2410828B1 FR2410828B1 (fr) 1984-04-13

Family

ID=15393610

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7834252A Granted FR2410828A1 (fr) 1977-12-05 1978-12-05 Dispositif de guidage d'aeronefs a l'atterrissage

Country Status (5)

Country Link
US (1) US4232316A (fr)
JP (1) JPS602628B2 (fr)
CA (1) CA1112743A (fr)
FR (1) FR2410828A1 (fr)
GB (1) GB2009556B (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2519430A1 (fr) * 1981-12-31 1983-07-08 Thomson Csf Systeme d'atterrissage hyperfrequence a protection contre le brouillage
JPS6027867A (ja) * 1983-07-25 1985-02-12 Nec Corp 空中線装置
JP5591738B2 (ja) * 2011-02-28 2014-09-17 株式会社東芝 Ｉｌｓのローカライザ空中線装置用電力分配器およびこれを用いたローカライザ空中線装置
SE536546C2 (sv) * 2012-04-30 2014-02-11 Fmt Int Trade Ab Förfarande jämte anordning för att identifiera ett flygplani samband med parkering av flygplanet vid ett stand

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2419562A (en) * 1942-03-10 1947-04-29 Standard Telephones Cables Ltd Antenna array
US2501668A (en) * 1943-11-22 1950-03-28 Sperry Corp Aircraft landing system
US3508267A (en) * 1967-12-28 1970-04-21 Anvar Airport runway distance meter
US3893119A (en) * 1972-09-20 1975-07-01 Anvar Distance measuring apparatus integrated in an aircraft landing system of the ILS type
US4032920A (en) * 1975-09-02 1977-06-28 Wilcox Electric, Inc. Two-frequency instrument landing system with integral monitor

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NO124503B (fr) * 1967-06-08 1972-04-24 Sintef
NL7601477A (nl) * 1975-02-27 1976-08-31 Int Standard Electric Corp Landingskoerszendinstallatie of glijpadzend- installatie voor een instrumentlandingsstelsel.

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2419562A (en) * 1942-03-10 1947-04-29 Standard Telephones Cables Ltd Antenna array
US2501668A (en) * 1943-11-22 1950-03-28 Sperry Corp Aircraft landing system
US3508267A (en) * 1967-12-28 1970-04-21 Anvar Airport runway distance meter
US3893119A (en) * 1972-09-20 1975-07-01 Anvar Distance measuring apparatus integrated in an aircraft landing system of the ILS type
US4032920A (en) * 1975-09-02 1977-06-28 Wilcox Electric, Inc. Two-frequency instrument landing system with integral monitor

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
EXBK/59 *

Also Published As

Publication number Publication date
JPS5478696A (en) 1979-06-22
CA1112743A (fr) 1981-11-17
GB2009556A (en) 1979-06-13
US4232316A (en) 1980-11-04
GB2009556B (en) 1982-06-09
JPS602628B2 (ja) 1985-01-23
FR2410828B1 (fr) 1984-04-13

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