[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

DE69421489D1 - Verbesserungen an Flugzeuglandesystemen - Google Patents

Verbesserungen an Flugzeuglandesystemen

Info

Publication number
DE69421489D1
DE69421489D1 DE69421489T DE69421489T DE69421489D1 DE 69421489 D1 DE69421489 D1 DE 69421489D1 DE 69421489 T DE69421489 T DE 69421489T DE 69421489 T DE69421489 T DE 69421489T DE 69421489 D1 DE69421489 D1 DE 69421489D1
Authority
DE
Germany
Prior art keywords
landing system
airplane landing
system improvements
airplane
landing
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
DE69421489T
Other languages
English (en)
Other versions
DE69421489T2 (de
Inventor
David Parkin
John David Sole
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.)
Thales ATM Ltd
Original Assignee
Thales ATM 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 Thales ATM Ltd filed Critical Thales ATM Ltd
Application granted granted Critical
Publication of DE69421489D1 publication Critical patent/DE69421489D1/de
Publication of DE69421489T2 publication Critical patent/DE69421489T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S1/00Beacons 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
    • G01S1/02Beacons 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
    • G01S1/022Means for monitoring or calibrating
    • G01S1/024Means for monitoring or calibrating of beacon transmitters
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S1/00Beacons 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
    • G01S1/02Beacons 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
    • G01S1/08Systems for determining direction or position line
    • G01S1/44Rotating or oscillating beam beacons defining directions in the plane of rotation or oscillation
    • G01S1/54Narrow-beam systems producing at a receiver a pulse-type envelope signal of the carrier wave of the beam, the timing of which is dependent upon the angle between the direction of the receiver from the beacon and a reference direction from the beacon; Overlapping broad beam systems defining a narrow zone and producing at a receiver a pulse-type envelope signal of the carrier wave of the beam, the timing of which is dependent upon the angle between the direction of the receiver from the beacon and a reference direction from the beacon
    • G01S1/56Timing the pulse-type envelope signals derived by reception of the beam

Landscapes

  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Details Of Aerials (AREA)
DE69421489T 1993-09-28 1994-08-12 Verbesserungen an Flugzeuglandesystemen Expired - Lifetime DE69421489T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9319993A GB2282292B (en) 1993-09-28 1993-09-28 Improvements in or relating to aircraft landing systems

Publications (2)

Publication Number Publication Date
DE69421489D1 true DE69421489D1 (de) 1999-12-09
DE69421489T2 DE69421489T2 (de) 2000-04-06

Family

ID=10742653

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69421489T Expired - Lifetime DE69421489T2 (de) 1993-09-28 1994-08-12 Verbesserungen an Flugzeuglandesystemen

Country Status (7)

Country Link
US (1) US5512900A (de)
EP (1) EP0645642B1 (de)
JP (1) JP3479125B2 (de)
AU (1) AU672521B2 (de)
CA (1) CA2129944C (de)
DE (1) DE69421489T2 (de)
GB (1) GB2282292B (de)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5629692A (en) * 1995-07-20 1997-05-13 Honeywell Inc. Method and apparatus for alerting pilot to transponder antenna failure in a traffic alert and collision avoidance system
DE19757044A1 (de) * 1997-12-20 1999-06-24 Cit Alcatel Überwachungseinrichtung für den Landekurssender eines Instrumentenlandesystems
DE19953271A1 (de) * 1999-11-06 2001-05-10 Airsys Navigation Systems Gmbh Sendeantenne
US6597312B1 (en) * 2002-01-30 2003-07-22 Northrop Grumman Corporation Phased array antenna system generating multiple beams having a common phase center
US8049661B1 (en) 2007-11-15 2011-11-01 Lockheed Martin Corporation Antenna array with robust failed-element processor
JP5104938B2 (ja) * 2010-12-09 2012-12-19 株式会社デンソー フェーズドアレイアンテナの位相校正方法及びフェーズドアレイアンテナ
JP5810746B2 (ja) * 2011-08-24 2015-11-11 日本電気株式会社 アンテナ装置及びビーム指向特性改善方法
CN109782791A (zh) * 2017-11-14 2019-05-21 长城汽车股份有限公司 一种无人机的降落方法和装置

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2924847A1 (de) * 1979-06-20 1981-01-22 Standard Elektrik Lorenz Ag Mikrowellenlandesystem, das nach dem strahlschwenkverfahren arbeitet
US4647926A (en) * 1984-07-27 1987-03-03 Allied Corporation Warning system for microwave landing system airborne receiver
FR2582127B1 (fr) * 1985-03-29 1994-05-20 Thomson Csf Procede et dispositif de surveillance d'une station d'un systeme d'aide a l'atterissage du type mls
DE3618628A1 (de) * 1986-06-03 1987-12-10 Standard Elektrik Lorenz Ag Nach dem strahlschwenkverfahren arbeitendes mikrowellenlandesystem
GB2194407B (en) * 1986-08-27 1990-05-30 Marconi Co Ltd Antenna pattern monitor
JPS63144274A (ja) * 1986-12-08 1988-06-16 Nec Corp マイクロ波着陸誘導装置のモニタ確認回路
GB2203915B (en) * 1987-04-20 1991-05-22 Hazeltine Corp Automatic, real-time fault monitor verifying network in a microwave landing system
US4823127A (en) * 1987-04-20 1989-04-18 Hazeltine Corporation Automatic, real-time fault monitor verifying network in a microwave landing system
DE3885092T2 (de) * 1988-04-21 1994-05-19 Hazeltine Corp Automatische Überprüfungsschaltung in Echtzeit für einen Fehlermonitor in einem Mikrowellenlandesystem.
US5134416A (en) * 1990-01-08 1992-07-28 Cafarelli Nicholas J Scanning antenna having multipath resistance

Also Published As

Publication number Publication date
EP0645642B1 (de) 1999-11-03
GB2282292A (en) 1995-03-29
DE69421489T2 (de) 2000-04-06
AU7287494A (en) 1995-04-13
AU672521B2 (en) 1996-10-03
US5512900A (en) 1996-04-30
EP0645642A1 (de) 1995-03-29
CA2129944A1 (en) 1995-03-29
CA2129944C (en) 2005-11-29
GB9319993D0 (en) 1993-11-17
GB2282292B (en) 1997-12-17
JPH07159503A (ja) 1995-06-23
JP3479125B2 (ja) 2003-12-15

Similar Documents

Publication Publication Date Title
DE69302242D1 (de) Hubschrauberrumpf-Struktur
NO951788D0 (no) Kombinert flymaskin
DE68906415D1 (de) Flugzeugbremsanlage.
DE69310214D1 (de) Dialogsystem
DE69430198D1 (de) Grossraumflugzeug
DE69121112D1 (de) Flugsimulator
DE68919811D1 (de) Flugzeuginstrumentensysteme.
DE59010174D1 (de) Autonomes Landesystem
DE69818927D1 (de) Flugzeugbugfahrwerk
FI925957A0 (fi) Styranordning foer en eller flera arbetspunkter
DE69421489D1 (de) Verbesserungen an Flugzeuglandesystemen
DE69315955D1 (de) Flugobjekt
BR9207063A (pt) Aeronave híbrida
DE69301793D1 (de) Triebwerkaufhängung an Luftfahrzeugstruktur
DE69409729D1 (de) Hubschrauber
FI933431A0 (fi) Kosmetisk eller dermatologisk anti-ureaseblandning
ATA162993A (de) Flugzeughangar
SE9303994D0 (sv) Nytt flygsystem
KR970006116A (ko) 동체구조
SE9202692D0 (sv) En flygmaskin
ATA258393A (de) Flugzeughangar
KR970061694A (ko) 비행기 동체
KR950007323U (ko) 소프트 랜딩 시스템
BR9504322A (pt) Aerodisco - veículo aeronáutico atmosférico
GB2251997B (en) Aircraft landing system

Legal Events

Date Code Title Description
8364 No opposition during term of opposition