ES2107306T3 - Dispositivo para guia del piloto de un avion que se aproxima a su posicion de estacionamiento. - Google Patents

Dispositivo para guia del piloto de un avion que se aproxima a su posicion de estacionamiento.

Info

Publication number
ES2107306T3
ES2107306T3 ES95909774T ES95909774T ES2107306T3 ES 2107306 T3 ES2107306 T3 ES 2107306T3 ES 95909774 T ES95909774 T ES 95909774T ES 95909774 T ES95909774 T ES 95909774T ES 2107306 T3 ES2107306 T3 ES 2107306T3
Authority
ES
Spain
Prior art keywords
aircraft
sub
plane
horizontal
distance
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
ES95909774T
Other languages
English (en)
Inventor
Ernst Otto Tabel
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Application granted granted Critical
Publication of ES2107306T3 publication Critical patent/ES2107306T3/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
    • G08G5/20—Arrangements for acquiring, generating, sharing or displaying traffic information
    • G08G5/22—Arrangements for acquiring, generating, sharing or displaying traffic information located on the ground
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/002—Taxiing aids
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C15/00—Surveying instruments or accessories not provided for in groups G01C1/00 - G01C13/00
    • G01C15/002—Active optical surveying means
    • 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
    • G01S17/00—Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
    • G01S17/02—Systems using the reflection of electromagnetic waves other than radio waves
    • G01S17/06—Systems determining position data of a target
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/50—Navigation or guidance aids
    • G08G5/51—Navigation or guidance aids for control when on the ground, e.g. taxiing or rolling
    • 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
    • G01S17/00—Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
    • G01S17/88—Lidar systems specially adapted for specific applications
    • 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
    • G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/48—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S17/00
    • G01S7/51—Display arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Electromagnetism (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Mechanical Engineering (AREA)
  • Optical Radar Systems And Details Thereof (AREA)
  • Traffic Control Systems (AREA)
  • Length Measuring Devices By Optical Means (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

LA INVENCION SE REFIERE A UN DISPOSITIVO PARA GUIA DE PILOTOS EN UN AVION QUE SE ACERCA A SU POSICION DE APARCADO ESPECIFICA CUANDO CIRCULA DE FORMA RECTA. EL DISPOSITIVO COMPRENDE UNA DISPOSICION DE MEDICION DE DISTANCIA, QUE SE DISPONE DE MANERA ENFRENTADA EN LA DIRECCION DE DESPLAZAMIENTO A PARTIR DE LA PARTE FRONTAL DEL AVION Y DETERMINA LA POSICION ACTUAL DEL AVION. EL DISPOSITIVO COMPRENDE ADEMAS UNA DISPOSICION DE INDICACION MOSTRANDO AL PILOTO LA DISTANCIA QUE PERMANECE ENTRE LA POSICION ACTUAL Y LA POSICION DE APARCADO. LA INVENCION SE CARACTERIZA DE TAL MODO, PROVISTA COMO DISPOSICION DE MEDICION DE DISTANCIA, QUE SE DISPONE AL MENOS DE UN SENSOR (15) LASER 2D QUE MIDE LA PARTE FRONTAL DE UN AVION (10) PUNTO POR PUNTO EN UN PLANO (NO HORIZONTAL) CON UN ANGULO PREDETERMINADO DE OBSERVACION (16) Y EN CICLOS DE MEDICION SUCESIVOS, INTERRUMPE CADA PUNTO MEDIDO (P1-P4) DENTRO DE SUS COORDENADAS HORIZONTALES Y VERTICALES, FORMANDO LOS VALORES MEDIOS COMO UNA POSICION ACTUAL DEL AVION CON RESPECTO A LAS COORDENADAS (X{SUB,P}2 -X{SUB,P}3) HORIZONTALES, DETERMINADAS EN UN CICLO DE MEDICION. LOS PUNTOS MEDIDOS CUYAS COORDINADAS (Y{SUB,P} - Y {SUB,P}3) VERTICALES CAEN DENTRO AL MENOS DE UNA ZONA (23) DE ALTURA, QUE PUEDE SER DEFINIDA DE MANERA SEPARADA PARA CADA TIPO DE AVION ENTRE VALORES (YU - YO) DE LIMITACION, SE COMPARAN CON LA POSICION DE APARCADO, QUE ES DEFINIDA A ELECCION COMO COORDINADAS HORIZONTALES, Y GENERA UNA SEÑAL PARA LA DISPOSICION (17) DE INDICACION COMO UNA FUNCION DE LA DISTANCIA ENTRE LA POSICION ACTUAL Y LA POSICION DE APARCADO.
ES95909774T 1994-03-02 1995-02-23 Dispositivo para guia del piloto de un avion que se aproxima a su posicion de estacionamiento. Expired - Lifetime ES2107306T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4406821A DE4406821A1 (de) 1994-03-02 1994-03-02 Vorrichtung zur Führung des Piloten eines sich seiner Parkposition nähernden Flugzeuges

Publications (1)

Publication Number Publication Date
ES2107306T3 true ES2107306T3 (es) 1997-11-16

Family

ID=6511621

Family Applications (1)

Application Number Title Priority Date Filing Date
ES95909774T Expired - Lifetime ES2107306T3 (es) 1994-03-02 1995-02-23 Dispositivo para guia del piloto de un avion que se aproxima a su posicion de estacionamiento.

Country Status (7)

Country Link
US (1) US5889479A (es)
EP (1) EP0746497B1 (es)
AT (1) ATE154913T1 (es)
AU (1) AU1811895A (es)
DE (2) DE4406821A1 (es)
ES (1) ES2107306T3 (es)
WO (1) WO1995023734A1 (es)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2169965A1 (es) * 1999-08-02 2002-07-16 Team Tecnologia Europ Aplic Al Procedimiento y aparato para el guiado de aeronaves en maniobra de atraque.

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US7541944B2 (en) * 2004-07-12 2009-06-02 The Boeing Company Systems and methods for collision avoidance
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DK1619342T3 (da) * 2004-07-22 2009-07-27 Bea Sa Varmefölsom array-indretning til tilstedeværelsesdetektering ved automatiske döre
US8862379B2 (en) * 2004-09-20 2014-10-14 The Boeing Company Vehicle collision shield
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US8085410B1 (en) * 2009-04-16 2011-12-27 Patrick Allen Hargabus Projected scanning laser device and method for locating small objects
CN104443423B (zh) * 2013-09-18 2016-08-17 爱乐基股份有限公司 航空器进场引导系统的校正定位方法
CN104443434B (zh) * 2013-09-18 2016-08-10 业群资讯股份有限公司 航空器停靠过程的引导方法
TWM484091U (zh) * 2014-03-31 2014-08-11 Unibase Information Corp 具有稽核及影像同步功能的航空器導引系統、及其稽核與影像同步裝置
US10627490B2 (en) 2016-01-31 2020-04-21 Velodyne Lidar, Inc. Multiple pulse, LIDAR based 3-D imaging
CN109154661A (zh) 2016-03-19 2019-01-04 威力登激光雷达有限公司 用于基于lidar的3-d成像的集成照射和检测
US10393877B2 (en) 2016-06-01 2019-08-27 Velodyne Lidar, Inc. Multiple pixel scanning LIDAR
US11383963B2 (en) 2017-03-03 2022-07-12 Jlg Industries, Inc. Obstacle detection system for an aerial work platform
WO2018183843A1 (en) 2017-03-31 2018-10-04 Velodyne Lidar, Inc. Integrated lidar illumination power control
CN110809704B (zh) 2017-05-08 2022-11-01 威力登激光雷达美国有限公司 Lidar数据获取与控制
US11294041B2 (en) 2017-12-08 2022-04-05 Velodyne Lidar Usa, Inc. Systems and methods for improving detection of a return signal in a light ranging and detection system
US10410530B1 (en) 2018-02-27 2019-09-10 Honeywell International Inc. Systems and methods for detecting potential surface collisions and providing warnings onboard an aircraft or airport vehicle
US10234303B1 (en) 2018-02-28 2019-03-19 Honeywell International Inc. Methods and systems for providing visually automated in-cockpit aircraft docking guidance with use of airport moving map applications
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US10712434B2 (en) 2018-09-18 2020-07-14 Velodyne Lidar, Inc. Multi-channel LIDAR illumination driver
US11082010B2 (en) 2018-11-06 2021-08-03 Velodyne Lidar Usa, Inc. Systems and methods for TIA base current detection and compensation
US12061263B2 (en) 2019-01-07 2024-08-13 Velodyne Lidar Usa, Inc. Systems and methods for a configurable sensor system
US11885958B2 (en) 2019-01-07 2024-01-30 Velodyne Lidar Usa, Inc. Systems and methods for a dual axis resonant scanning mirror
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CN112863252B (zh) * 2021-01-18 2022-12-02 北京京东乾石科技有限公司 飞行器降落控制方法、装置、系统、设备及存储介质

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2169965A1 (es) * 1999-08-02 2002-07-16 Team Tecnologia Europ Aplic Al Procedimiento y aparato para el guiado de aeronaves en maniobra de atraque.

Also Published As

Publication number Publication date
WO1995023734A1 (de) 1995-09-08
EP0746497B1 (de) 1997-07-02
EP0746497A1 (de) 1996-12-11
AU1811895A (en) 1995-09-18
US5889479A (en) 1999-03-30
ATE154913T1 (de) 1997-07-15
DE4406821A1 (de) 1995-09-07
DE59500347D1 (de) 1997-08-07

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