MXPA02011010A - Sistema de aterrizaje de transpondedor. - Google Patents

Sistema de aterrizaje de transpondedor.

Info

Publication number
MXPA02011010A
MXPA02011010A MXPA02011010A MXPA02011010A MXPA02011010A MX PA02011010 A MXPA02011010 A MX PA02011010A MX PA02011010 A MXPA02011010 A MX PA02011010A MX PA02011010 A MXPA02011010 A MX PA02011010A MX PA02011010 A MXPA02011010 A MX PA02011010A
Authority
MX
Mexico
Prior art keywords
aircraft
elevation
arrival
measurement
transponder
Prior art date
Application number
MXPA02011010A
Other languages
English (en)
Inventor
Benjamin R Kuehn
Original Assignee
Advanced Navigation & Position
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 Advanced Navigation & Position filed Critical Advanced Navigation & Position
Publication of MXPA02011010A publication Critical patent/MXPA02011010A/es

Links

Classifications

    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • 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
    • G01S3/00Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
    • G01S3/02Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using radio waves
    • G01S3/14Systems for determining direction or deviation from predetermined direction
    • G01S3/46Systems for determining direction or deviation from predetermined direction using antennas spaced apart and measuring phase or time difference between signals therefrom, i.e. path-difference systems
    • 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
    • G01S13/00Systems 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
    • G01S13/74Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems
    • G01S13/76Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems wherein pulse-type signals are transmitted
    • G01S13/762Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems wherein pulse-type signals are transmitted with special measures concerning the radiation pattern, e.g. S.L.S.
    • 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
    • G01S13/00Systems 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
    • G01S13/88Radar or analogous systems specially adapted for specific applications
    • G01S13/91Radar or analogous systems specially adapted for specific applications for traffic control
    • G01S13/913Radar or analogous systems specially adapted for specific applications for traffic control for landing purposes

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Electromagnetism (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Radio Transmission System (AREA)
  • Radio Relay Systems (AREA)
  • Casting Devices For Molds (AREA)
  • Traffic Control Systems (AREA)

Abstract

Un sistema de aterrizaje de precision de una aeronave, basado en tierra, proporciona un metodo de precision CAT I y guia para el aterrizaje. La posicion de elevacion de la aeronave es determinada midiendo la fase diferencial del transmisor y la hora de llegada de la respuesta del transpondedor ATCRBS de la aeronave. La respuesta del transpondedor es recibida en una pluralidad de ubicaciones de antenas perceptoras en donde es transmitida a un sensor, desmodulada y digitalizada. Los datos son transmitidos a un procesador central en donde se aplican la calibracion y las correcciones de trayectoria multiple. La conmutacion de la antena de diversidad del transpondedor de la aeronave esta aislada del ruido de fluctuaciones y distorsionado de la trayectoria multiple de la respuesta del transpondedor, correlacionando los saltos de fase diferencial medidos entre las antenas perceptoras separadas. Se mantiene un estimado de la separacion de la antena de diversidad mediante el procesamiento del filtro Kalman; la separacion estimada es usada para corregir los datos de la medicion de fase diferencial de la elevacion de la aeronave. La medicion de fase corregida y la medicion de la hora de llegada son procesadas utilizando otro filtro Kalman para lograr la exactitud de colocacion de elevacion deseada de la aeronave. Se aplica un subsistema de fase diferencial del transmisor y hora de llegada para lograr una medicion azimut de la posicion de la aeronave. El azimut y la elevacion de la aeronave combinados son comparados con la trayectoria de la aproximacion deseada, y el error de posicion de la aeronave en relacion con la aproximacion deseada, es comunicado a la aeronave.
MXPA02011010A 2000-05-09 2001-05-09 Sistema de aterrizaje de transpondedor. MXPA02011010A (es)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US20303900P 2000-05-09 2000-05-09
US09/695,359 US6469654B1 (en) 2000-05-09 2000-10-24 Transponder landing system
PCT/US2001/014881 WO2001086229A2 (en) 2000-05-09 2001-05-09 Transponder landing system

Publications (1)

Publication Number Publication Date
MXPA02011010A true MXPA02011010A (es) 2004-08-19

Family

ID=26898256

Family Applications (1)

Application Number Title Priority Date Filing Date
MXPA02011010A MXPA02011010A (es) 2000-05-09 2001-05-09 Sistema de aterrizaje de transpondedor.

Country Status (13)

Country Link
US (1) US6469654B1 (es)
EP (1) EP1297307B1 (es)
KR (1) KR20030016257A (es)
CN (1) CN1441909A (es)
AT (1) ATE279735T1 (es)
AU (1) AU2001274822A1 (es)
CA (1) CA2409547A1 (es)
DE (1) DE60106446T2 (es)
ES (1) ES2232631T3 (es)
IL (1) IL152709A0 (es)
MX (1) MXPA02011010A (es)
NZ (1) NZ523021A (es)
WO (1) WO2001086229A2 (es)

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Also Published As

Publication number Publication date
EP1297307B1 (en) 2004-10-13
CA2409547A1 (en) 2001-11-15
DE60106446T2 (de) 2006-02-02
US6469654B1 (en) 2002-10-22
AU2001274822A1 (en) 2001-11-20
DE60106446D1 (de) 2004-11-18
IL152709A0 (en) 2003-06-24
ATE279735T1 (de) 2004-10-15
ES2232631T3 (es) 2005-06-01
CN1441909A (zh) 2003-09-10
NZ523021A (en) 2004-06-25
KR20030016257A (ko) 2003-02-26
WO2001086229A2 (en) 2001-11-15
WO2001086229A3 (en) 2002-05-02
EP1297307A2 (en) 2003-04-02

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