1. Field of the Invention
The present invention relates to methods and systems for reducing runway incursions at airports, including such methods and systems which utilize the local airfield communications channel and the flat panel display system on board the aircraft to provide visibility of active aircraft within an airport to other aircraft within the airport on the display system.
2. Description of the Related Art
Runway safety is a vital component of aviation safety as a whole and of vital concern to both the Federal Aviation Administration, pilots, and the flying public. Although considerable work has been done on the development of sophisticated collision avoidance systems to prevent mid-air collisions, such has not been the case with respect to systems to avoid collisions once the aircraft is safely on the ground, or to reduce or prevent runway incursions at crowded airports. Instead, considerable reliance has been placed on visual sightings by the control tower or a pilot of a taxiing aircraft to provide a verbal warning of a potential runway incursion so that evasive action can then be taken. Although this has proven satisfactory under certain conditions, it has not always worked and has resulted in catastrophic situations, such as the air disaster which occurred in Majorcca when two large commercial jets collided on the ground resulting in several deaths, as well as resulting in many near misses. This situation becomes even more critical at airports with multiple runways and taxiways where several aircraft are in motion on the ground simultaneously. In addition, the predicted growth over the next several years in air traffic will only add to the problem and implies that the number of such actual incidents may rise if improvements are not made in methods and systems for preventing or reducing runway incursions
Existing flat panel display systems, such as the systems described in the aforementioned commonly owned U.S. Pat. No. 6,693,558, and two copending patent applications, all of which have been incorporated by reference in their entirety herein, include global positioning systems or GPS; however, to the applicant's knowledge, such GPS systems have not been utilized to avoid or prevent runway incursions. Moreover, commercial graphics processors, or CGPs, from the gaming industry have been used in the past by avionics suppliers for other applications with little to no mandated safety guidelines. In fact, it is known that there are potential failures which can occur within such commercial graphic processors which can result in a display of misleading information to a pilot, which is the last thing one would want in a system which would be intended to avoid or prevent runway incursions where misleading information could result in a potential disaster. Although complex and costly systems might be developed which could solve the problem, because of the need to then retrofit existing aircraft with such a system, there exists a need for a simple and low cost method and system capable of providing a geo-referenced display of all active aircraft within an airport to all aircraft within that airport, such as on an electronic airport map viewable to both the pilots on the ground as well as to the ground controller in the tower.
An improved method and system for reducing runway incursion periodically transmits a data packet on the normal airfield voice communication channel from an aircraft dispersed on the ground at the airport when the aircraft is utilizing the voice communication channel, with the data packet comprising a current ground position for the aircraft along with a unique identifier for the aircraft; provides a geo-referenced map display of the airport; and receives the transmitted data packet at another location at the airport and displays the ground location of the data packet transmitting aircraft on the geo-referenced map display for indicating the position of the aircraft on the ground at the airport. Each of the aircraft dispersed on the ground at the airport would have a different unique identifier to distinguish the various aircraft on the geo-referenced map display. In addition, each of the dispersed aircraft is polled in order to update the geo-referenced map display with updated ground position information on the location of the various dispersed aircraft. When the microphone is keyed to talk by the pilot, a short burst, such as a 3 microsecond burst or one which could be transmitted for up to 20 microseconds, of data containing theuniques aircraft identifier, such as the tail number, for example, and the ground position of the aircraft is transmitted to the control tower and all other aircraft on the same frequency, such as the airport ground frequency of 121.6 or 121.9 MHz Since all aircraft at a given airport must communicate with the tower over a common frequency, this transmitted data packet of GPS information which takes place over that communication channel, together with the geo-referenced map display, enables both the control tower and the pilots on the ground, all tuned to that same communication channel, to receive an accurate display of the exact location and identification of each of the aircraft dispersed on the ground at the airport on their geo-referenced map display, such as part of the flat panel display system in the aircraft and is believed to provide a simple, cost effective solution to the problem of minimizing, if not preventing runway incursions.
Referring now to the drawings in detail, and initially to
In this regard, when the pilot keys the microphone to talk for up to 20 microseconds, for example, the latitudinal and longitudinal position of the aircraft along with its unique identifier, such as the tail number, would be transmitted in the data packet to all other aircraft on that frequency as well as to the ground controller on that frequency. Preferably, this could be accomplished in a 3 microsecond burst. In addition, in order to update this information periodically so as to provide an updated geo-referenced map display containing the latest ground position information for the various aircraft dispersed on the ground, the tower preferably polls the aircraft by transmitting a signal to the various interface boxes via the communication channel which respond with data packets containing the updated information for updating the displays.
Consequently, by utilizing the system and method of the present invention, the problem of runway incursion can be overcome by utilizing the existing aircraft radio and airport frequency in an efficient and economical manner so that an aircraft equipped with a display system capable of displaying a geo-referenced map of the airport can superimpose positions of all other aircraft on the map for pilot information as well as the ground track that the aircraft needs to follow based on its ultimate destination within the airport, to enable safe and efficient movement of the aircraft on the ground.
It should be recognized that structures and/or elements and/or method steps shown and/or described in connection with any disclosed form or embodiment of the invention may be incorporated in any other disclosed or described or suggested form or embodiment as a matter of design choice. Moreover, while there have shown and described and pointed out fundamental novel features of the invention as applied to preferred embodiments thereof, it will be understood that various omissions and substitutions and changes in the form and details of the system and method illustrated may be made by those skilled in the art without departing from the spirit and scope of the present invention.
This application is a continuation of U.S. patent application No. 12/317,425, filed Dec. 23, 2008, now U.S. Pat. No. 8,046,158, and is related to commonly owned U.S. Pat. No. 6,693,558, filed Dec. 14, 2001, issued Feb. 17, 2004, naming Geoffrey S. M. Hedrick as the sole inventor; copending U.S. patent application Ser. No. 11/212059, filed Aug. 24, 2005, entitled “Aircraft Flat Panel Display System With Graphical Image Integrity”, naming Geoffrey S. M. Hedrick, Shahram Askarpour, Markus Knopf, and Jeff Collins as joint inventors; and copending U.S. patent application Ser. No. 11/223,168, filed Sep. 8, 2005, entitled “Aircraft Flat Panel Display System With Improved Information Availability”, naming Geoffrey S. M. Hedrick and Shahram Askarpour as joint inventors, and is an improvement thereon. The contents of each of the foregoing are hereby specifically incorporated by reference in their entirety.
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Number | Date | Country | |
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Parent | 12317425 | Dec 2008 | US |
Child | 13280038 | US |