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
Links
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
-
- 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
- G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
- G01S3/02—Direction-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
- G01S3/14—Systems for determining direction or deviation from predetermined direction
- G01S3/46—Systems 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
-
- 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
- G01S13/76—Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems wherein pulse-type signals are transmitted
- G01S13/762—Systems 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.
-
- 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
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.
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) |
Families Citing this family (61)
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EP2515260A4 (en) * | 2009-12-15 | 2018-01-10 | Nec Corporation | Information processing device, information processing method, and storage medium |
FR2956907B1 (fr) * | 2010-02-26 | 2012-09-21 | Thales Sa | Systeme radar multistatique pour la mesure precise de l'altitude |
CN101826880A (zh) * | 2010-03-23 | 2010-09-08 | 成都九洲迪飞科技有限责任公司 | 空中交通告警与防撞系统接收机信号源模块 |
GB2478954B (en) * | 2010-03-25 | 2012-02-08 | Guidance Ip Ltd | Active target |
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GB2478960B (en) * | 2010-03-25 | 2012-08-22 | Guidance Ip Ltd | An apparatus for measuring the relative direction of a radio signal |
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EP2604009A2 (en) * | 2010-08-09 | 2013-06-19 | Aviation Communication & Surveillance Systems, LLC | Systems and methods for providing surface multipath mitigation |
DE102010052475B4 (de) | 2010-11-26 | 2014-05-08 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Ortungssystem |
DE102010052474B4 (de) | 2010-11-26 | 2017-07-27 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Flugführungssystem |
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CN102435982B (zh) * | 2011-09-09 | 2014-01-15 | 陕西长岭电子科技有限责任公司 | 一种三模式空管应答机及对三种模式询问信号的检测和识别方法 |
FR2979995B1 (fr) * | 2011-09-09 | 2013-10-11 | Thales Sa | Systeme de localisation d'un engin volant |
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EP2747204A1 (en) * | 2012-12-18 | 2014-06-25 | BAE SYSTEMS plc | Improvements in and relating to radar |
AU2013366159B2 (en) * | 2012-12-18 | 2016-12-22 | Bae Systems Plc | Improvements in and relating to radar |
US9766322B2 (en) | 2013-03-14 | 2017-09-19 | Ensco, Inc. | Geolocation with radio-frequency ranging |
US9995824B2 (en) | 2014-04-09 | 2018-06-12 | Thomas Danaher Harvey | Methods and system to assist search for lost and submerged objects |
US10871566B2 (en) * | 2014-04-09 | 2020-12-22 | Thomas Danaher Harvey | Methods and system to assist search and interception of lost objects |
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CN105066986B (zh) * | 2015-07-28 | 2018-06-26 | 四川九洲空管科技有限责任公司 | 一种多模式上传体制的航空地面着陆系统及其控制方法 |
EP3165944B1 (en) * | 2015-11-04 | 2022-04-20 | Nxp B.V. | Embedded communication authentication |
RU2608183C1 (ru) * | 2015-11-17 | 2017-01-17 | Федеральное государственное образовательное бюджетное учреждение высшего профессионального образования "Санкт-Петербургский государственный университет телекоммуникаций им. проф. М.А. Бонч-Бруевича" | Многопозиционная система посадки воздушных судов |
US10281586B2 (en) * | 2016-04-07 | 2019-05-07 | Thales USA, Inc. | Transmission data for flight check |
TWI593941B (zh) * | 2016-07-26 | 2017-08-01 | 明泰科技股份有限公司 | 車載導航方法及系統 |
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DE102017117498A1 (de) | 2017-08-02 | 2019-02-07 | Airbus Defence and Space GmbH | System und Verfahren zum Kalibrieren einer Sendeeinheit sowie Wasserfahrzeug mit einem System zum Kalibrieren einer Sendeeinheit |
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CN108520640B (zh) * | 2018-03-23 | 2022-07-01 | 清研讯科(北京)科技有限公司 | 基于超宽带的无人机导航方法、导航设备、无人机 |
JP7144801B2 (ja) * | 2018-06-01 | 2022-09-30 | 国立大学法人京都大学 | 計測装置、受電装置、送電装置、および飛行システム |
DE102018120198A1 (de) | 2018-08-20 | 2020-02-20 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Luftfahrzeug |
CN112654890A (zh) * | 2018-09-20 | 2021-04-13 | 京瓷株式会社 | 电子设备、电子设备的控制方法以及电子设备的控制程序 |
KR102209074B1 (ko) * | 2019-04-22 | 2021-01-27 | 최옥재 | 신호 이동시간을 이용한 고정익 항공기의 착륙유도방법 및 이를 이용한 시스템 |
CN110597297A (zh) * | 2019-10-21 | 2019-12-20 | 深圳市道通智能航空技术有限公司 | 一种飞行器返航控制方法、装置、飞行器和存储介质 |
CN113554900B (zh) * | 2021-09-22 | 2021-12-17 | 山东世纪矿山机电有限公司 | 一种基于定位系统的交通控制系统 |
CN115145157B (zh) * | 2022-09-07 | 2022-12-13 | 北京航天自动控制研究所 | 一种基于截止频率映射的姿态控制增益整定方法 |
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-
2000
- 2000-10-24 US US09/695,359 patent/US6469654B1/en not_active Expired - Lifetime
-
2001
- 2001-05-09 NZ NZ523021A patent/NZ523021A/en unknown
- 2001-05-09 CN CN01812543A patent/CN1441909A/zh active Pending
- 2001-05-09 CA CA002409547A patent/CA2409547A1/en not_active Abandoned
- 2001-05-09 AU AU2001274822A patent/AU2001274822A1/en not_active Abandoned
- 2001-05-09 IL IL15270901A patent/IL152709A0/xx unknown
- 2001-05-09 EP EP01941470A patent/EP1297307B1/en not_active Expired - Lifetime
- 2001-05-09 WO PCT/US2001/014881 patent/WO2001086229A2/en active IP Right Grant
- 2001-05-09 ES ES01941470T patent/ES2232631T3/es not_active Expired - Lifetime
- 2001-05-09 KR KR1020027015072A patent/KR20030016257A/ko not_active Application Discontinuation
- 2001-05-09 AT AT01941470T patent/ATE279735T1/de not_active IP Right Cessation
- 2001-05-09 MX MXPA02011010A patent/MXPA02011010A/es unknown
- 2001-05-09 DE DE60106446T patent/DE60106446T2/de not_active Expired - Fee Related
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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