EP1946285A1 - Procédé, agencement et dispositif de commande de navigation de véhicules aériens et terrestres en utilisant une détermination de position basée sur des satellites - Google Patents
Procédé, agencement et dispositif de commande de navigation de véhicules aériens et terrestres en utilisant une détermination de position basée sur des satellitesInfo
- Publication number
- EP1946285A1 EP1946285A1 EP06793982A EP06793982A EP1946285A1 EP 1946285 A1 EP1946285 A1 EP 1946285A1 EP 06793982 A EP06793982 A EP 06793982A EP 06793982 A EP06793982 A EP 06793982A EP 1946285 A1 EP1946285 A1 EP 1946285A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- aircraft
- information
- ground
- control device
- display device
- 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
Links
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0004—Transmission of traffic-related information to or from an aircraft
- G08G5/0013—Transmission of traffic-related information to or from an aircraft with a ground station
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/02—Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
- G08G5/025—Navigation or guidance aids
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/06—Traffic control systems for aircraft, e.g. air-traffic control [ATC] for control when on the ground
- G08G5/065—Navigation or guidance aids, e.g. for taxiing or rolling
Definitions
- the invention relates to the satellite-aided navigation ⁇ tion of ground vehicles and landed aircraft in the airport area.
- the pilot task After the landing of an aircraft, the pilot task has to move the aircraft quickly and safely to the parking position assigned to it by a control device (eg an operations center in the airport tower).
- a control device eg an operations center in the airport tower.
- the landing position and parking position can be several kilometers apart.
- the pilot After landing, the pilot often has the problem that he can not immediately orient himself clearly. This may be due, for example, the size of the airport, the sudden change of the reference environment from the sprawling air space for comparatively ⁇ as narrow floor space to be an airport or difficult vision ⁇ relationships. In many cases, especially when flying to the airport for the first time, the pilot has no indication of where his intended parking position is. Add to this that the radio frequencies of Bodenkon ⁇ trolls that could give clues are often overloaded. Also the signs of the airports, eg on the Rolling and apron railways (so-called taxiways), is neither optimal nor standardized.
- the pilot of the apron control directs the air ⁇ vehicle driver over radio to the intended position. It should be noted that the radio frequencies are congested on the ground and in the air in such a way that there are European programs which aim to radio communications uplifting ⁇ Lich reduce.
- the speed of the pilots 'speech is so high or their intelligibility on the radio is so low that the pilots require the utmost concentration in order to understand the pilots' instructions and to be able to follow them.
- the radio communication is always general and thus listened to by all - and thus also by those who are not affected by a specific instruction that is given by radio. This increases to satisfy the requirements ⁇ gen to the concentration of the pilots to reach a standing position on, because they must constantly pay attention to whether just them an arrival instructions are issued at a given moment.
- the aim of the invention is to make the ground navigation of aircraft and ground vehicles at airports safer and more effective. Stalten. This object is achieved on the basis of the descriptive part of claims 1, 23 and 24 by the characterizing part of these claims.
- Advantages of the invention are more effective and safer design of the aircraft ⁇ the transmission of highly topical, topographic maps information and target position information movements on the ground to the aircraft for ground navigation at the airport,
- Relief of pilots and ground controllers in land navigation include the transmission of the traffic-directing information vehicle from a control device on the air, in particular stop instructions, speed limits, indications of danger spots, the integrated imaging of the entire Bodenge ⁇ schehens of air and ground vehicles in a control device, eg the tower or a dispatch center in its entirety or in functional or topographical excerpts, the drastic reduction of radiotelephone traffic, complex ground installations such as antennas or sensors are not and when using GSM, GPRS or UMTS Wi-Fi or WiMAX only to a reasonable extent, which also makes use of regional airports possible,
- Soil life for billing or controlling Zwe ⁇ CKEN available, the whereabouts and current location of Bodeneinrichtun ⁇ gene can be determined via a monitor in a control center, it can be used inexpensive, commercially available terminals are set, for example, PDA with GPRS and GPS.
- FIG. 1 the schematic sequence of the method
- FIG. 3 a schematic representation of the trajectory of an aircraft before landing and its taxiway after landing
- Fig. 4 is a schematic representation of the taxiway in a plan view.
- Fig. 5 a schematic representation of the display device of a navigation system.
- a first embodiment relates to an aircraft F landing on an airport (Fig. 3).
- the aircraft F has a navigation system N (FIG. 2) on board, which determines its geographical position at cyclic intervals via satellite-supported position determination (GPS).
- the navigation system N is connected to a communications network KN via a transmitting and receiving device SEV-F (FIG. 2).
- control device KE Also connected to this communication network KN are a control device KE and a memory S, which also have transmission and reception systems SEV-KE, SEV-S (FIG. 2).
- the control device KE In order to ensure a safe and orderly clearance of the aircraft F on the ground, is the control device KE before or during the approach of the aircraft F a the Aircraft F assigned final target position ZP formed on Bo ⁇ the and transmitted to a memory S (Fig. 1).
- a communication connection is set up in the landing approach via the communication network between the aircraft F and the memory S. If the aircraft F arrives in this predefined area by a predetermined geographical position VP (FIG. 3) during landing, this is reported to the memory S and recognized therein.
- VP geographical position
- an existing mobile communication technology is partially adhesive and the protocols before ⁇ - such as GSM, GPRS, UMTS or WiMAX - is used.
- the topographical information TI which contain at least the destination position ZP and the route information RI, are transmitted from the memory S to the navigation system N (FIGS. 1, 2 ).
- This information TI, ZP and RI can then be displayed in the aircraft F in the form of an electronic map display on a display device (FIG. 5). Due to the representation of the route information RI, the pilot can move the aircraft F directly to the target position ZP without first having to orientate himself at the airport. Even complex radio-controlled contact with the control device KE is no longer required for ground navigation. The pilot may simply follow the presentation on the display device, which may even further traffic information, in particular Garge ⁇ messenger or limitations of Rollgeschwindgkeit, may indicate danger provide (Fig. 5).
- a further exemplary embodiment relates to the coordinated use of ground vehicles BF, here by way of example the refueling of the aircraft F by a tanker vehicle.
- control device KE decides which of the tank vehicles undertakes this refueling task. So far, this information is transmitted to the vehicle floor by means of BF especially egg ⁇ nes written order and voice WOR the.
- the tanker has a GPS system for locational ⁇ atmospheric. In addition to the pure position determination, it is also a standard function of GPS systems to provide speed information due to time measurement and determination of the distance traveled.
- the monitoring device KE mandated a specific ground vehicle with the refueling of the aircraft F at a certain gate, the entspre ⁇ promising campaign information AI and the bottom BZI destination information is transmitted to the ground vehicle.
- the invention is not limited to the embodiment be ⁇ , but can be set for the control of other aircraft and ground vehicles such as luggage or catering trucks is ⁇ . These vehicles are to be designed according to the invention.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Traffic Control Systems (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Radio Relay Systems (AREA)
- Navigation (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102005053499A DE102005053499A1 (de) | 2005-11-09 | 2005-11-09 | Verfahren, Anordnung und Kontrolleinrichtung zum Navigieren von Luft- und Bodenfahrzeugen unter Einsatz Satelliten-gestützter Positionsbestimmung |
PCT/EP2006/067108 WO2007054410A1 (fr) | 2005-11-09 | 2006-10-05 | Procédé, agencement et dispositif de commande de navigation de véhicules aériens et terrestres en utilisant une détermination de position basée sur des satellites |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1946285A1 true EP1946285A1 (fr) | 2008-07-23 |
EP1946285B1 EP1946285B1 (fr) | 2010-06-23 |
Family
ID=37440827
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP06793982A Not-in-force EP1946285B1 (fr) | 2005-11-09 | 2006-10-05 | Procédé, agencement et dispositif de commande de navigation de véhicules aériens et terrestres en utilisant une détermination de position basée sur des satellites |
Country Status (5)
Country | Link |
---|---|
US (1) | US20080270020A1 (fr) |
EP (1) | EP1946285B1 (fr) |
AT (1) | ATE472149T1 (fr) |
DE (2) | DE102005053499A1 (fr) |
WO (1) | WO2007054410A1 (fr) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8145367B2 (en) * | 2001-03-06 | 2012-03-27 | Honeywell International Inc. | Closed airport surface alerting system |
US8509140B2 (en) | 2006-11-21 | 2013-08-13 | Honeywell International Inc. | System and method for transmitting information using aircraft as transmission relays |
US7729263B2 (en) | 2007-08-08 | 2010-06-01 | Honeywell International Inc. | Aircraft data link network routing |
US9264126B2 (en) | 2007-10-19 | 2016-02-16 | Honeywell International Inc. | Method to establish and maintain an aircraft ad-hoc communication network |
US8811265B2 (en) | 2007-10-19 | 2014-08-19 | Honeywell International Inc. | Ad-hoc secure communication networking based on formation flight technology |
US8570990B2 (en) | 2007-12-04 | 2013-10-29 | Honeywell International Inc. | Travel characteristics-based ad-hoc communication network algorithm selection |
US9467221B2 (en) | 2008-02-04 | 2016-10-11 | Honeywell International Inc. | Use of alternate communication networks to complement an ad-hoc mobile node to mobile node communication network |
US8190147B2 (en) | 2008-06-20 | 2012-05-29 | Honeywell International Inc. | Internetworking air-to-air network and wireless network |
US8386167B2 (en) * | 2008-11-14 | 2013-02-26 | The Boeing Company | Display of taxi route control point information |
US9718557B2 (en) * | 2014-01-17 | 2017-08-01 | The Research Foundation For The State University Of New York | Flight data tracker |
CN103914076B (zh) * | 2014-03-28 | 2017-02-15 | 浙江吉利控股集团有限公司 | 一种基于无人机的货物传送系统和方法 |
US20170032687A1 (en) * | 2015-07-31 | 2017-02-02 | Honeywell International Inc. | Automatic in/out aircraft taxiing, terminal gate locator and aircraft positioning |
EP3444791A3 (fr) | 2017-08-13 | 2019-04-24 | IATAS Automatic Air Traffic Control Ltd | Système et procédés de services automatisés de contrôle du trafic aérien d'aéroports |
US10535276B2 (en) | 2017-12-04 | 2020-01-14 | Ge Aviation Systems Llc | Route planning and movement of an aircraft on the ground based on a navigation model trained to increase aircraft operational efficiency |
US20220309935A1 (en) * | 2021-03-29 | 2022-09-29 | Rockwell Collins, Inc. | System and method to display airport moving map and taxi routing guidance content for commonly used taxi route |
US20230123419A1 (en) * | 2021-10-14 | 2023-04-20 | Honeywell International Inc. | Systems and methods for suggesting context-relevant communication frequencies for an aircraft |
DE102023004236A1 (de) | 2023-10-21 | 2024-01-11 | Mercedes-Benz Group AG | Verfahren zur Navigation eines Fahrzeuges |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6195609B1 (en) * | 1993-09-07 | 2001-02-27 | Harold Robert Pilley | Method and system for the control and management of an airport |
US6006158A (en) * | 1993-09-07 | 1999-12-21 | H. R. Pilley | Airport guidance and safety system incorporating lighting control using GNSS compatible methods |
DE4303562A1 (de) * | 1993-02-08 | 1994-08-18 | Hoechst Ag | Härtungsmittel für wäßrige Epoxidharz-Dispersionen |
US6542086B2 (en) * | 1997-09-22 | 2003-04-01 | Siemens Aktiengesellschaft | Docking system for airport terminals |
US20030045994A1 (en) * | 2000-06-27 | 2003-03-06 | Stratton Richard L. | Airport ground-control system and method |
US7117089B2 (en) * | 2001-03-06 | 2006-10-03 | Honeywell International Inc. | Ground runway awareness and advisory system |
WO2002095709A2 (fr) * | 2001-05-18 | 2002-11-28 | Technology Planning Incorporated | Procede et systeme de gestion des mouvements de trafic de surface |
US7333887B2 (en) * | 2003-08-08 | 2008-02-19 | Baiada R Michael | Method and system for tactical gate management by aviation entities |
US20030074128A1 (en) * | 2001-10-16 | 2003-04-17 | Aris Mardirossian | Airport traffic control system |
US6748325B1 (en) * | 2001-12-07 | 2004-06-08 | Iwao Fujisaki | Navigation system |
ATE487925T1 (de) * | 2002-02-19 | 2010-11-15 | Boeing Co | Flughafenrollweg-navigationssystem |
RS20050149A (en) * | 2002-08-16 | 2007-02-05 | Togewa Holding Ag., | Method and system for gsm authentication wlan roaming |
US7271740B2 (en) * | 2003-12-19 | 2007-09-18 | Fischer Mark R | System and process for providing improved aircraft operational safety |
US7109889B2 (en) * | 2004-03-01 | 2006-09-19 | Honeywell International Inc. | Methods and apparatus for surface movement situation awareness |
US7222017B2 (en) * | 2004-06-17 | 2007-05-22 | The Boeing Company | Method and system for entering and displaying ground taxi instructions |
US7343229B1 (en) * | 2004-07-28 | 2008-03-11 | Rockwell Collins, Inc. | Method and apparatus for dynamic taxi path selection |
US7512714B2 (en) * | 2004-08-31 | 2009-03-31 | Honeywell International Inc. | System and method for transmitting ACARS messages over a TCP/IP data communication link |
-
2005
- 2005-11-09 DE DE102005053499A patent/DE102005053499A1/de not_active Withdrawn
-
2006
- 2006-10-05 EP EP06793982A patent/EP1946285B1/fr not_active Not-in-force
- 2006-10-05 US US12/092,493 patent/US20080270020A1/en not_active Abandoned
- 2006-10-05 DE DE502006007285T patent/DE502006007285D1/de active Active
- 2006-10-05 AT AT06793982T patent/ATE472149T1/de active
- 2006-10-05 WO PCT/EP2006/067108 patent/WO2007054410A1/fr active Application Filing
Non-Patent Citations (1)
Title |
---|
See references of WO2007054410A1 * |
Also Published As
Publication number | Publication date |
---|---|
DE502006007285D1 (de) | 2010-08-05 |
US20080270020A1 (en) | 2008-10-30 |
DE102005053499A1 (de) | 2007-05-24 |
ATE472149T1 (de) | 2010-07-15 |
WO2007054410A1 (fr) | 2007-05-18 |
EP1946285B1 (fr) | 2010-06-23 |
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