Patent Application
20050049762
The present invention generally relates to aircraft flight management system displays and, more particularly, to a flight management system display that integrates graphical flight planning with textual air traffic control clearance messages.
Presently, most air traffic control systems around the world utilize voice communications to transmit various messages between air traffic controllers and pilots. The messages that are transmitted between air traffic controllers and pilots include, among other things, air traffic control clearances, various advisories, and aviation weather services, which help ensure coordination of aircraft movement, and appropriate aircraft separation. As air travel has increased over the years, controller-pilot communication has concomitantly increased to the point that the voice communication channels have, at many locations, become saturated during peak aircraft traffic periods. Moreover, at the frequencies generally used for air traffic control voice communications, the communications are limited to line-of-sight. Thus, once an aircraft is no longer within a line-of-sight path with an air traffic control center, voice communication is no longer available.
To reduce the amount of controller-pilot voice communication that presently occurs, and to alleviate the reliance on the concomitant line-of-sight communications, a new data communication system has been developed that relies on data communication of certain controller-pilot communications. With this new communication system, some routine controller-pilot communications that are presently transmitted over a voice communications channel can be transmitted over a data communications channel, thus freeing up the voice communications channel for the less routine messages. For example, the data communication system allows various textual aircraft take-off and approach clearance messages to be transmitted and received, to and from, an aircraft over a data channel. These textual messages are presently processed and displayed via a separate, dedicated message display system.
Although the present controller-pilot data communication system implementation is generally reliable, safe, and reduces the communication load over the voice communication channels, it does suffer certain drawbacks. For example, the textual messages that are transmitted to and from an aircraft are standardized, thus pilot initiated textual messages are presently created using a “cut-and-paste” implementation, in which the pilot selects one or more standard portions of text from a list and places it in the message. This operation can be cumbersome, time-consuming, and can distract from the pilot's main tasks. Moreover, because the system is implemented separate from the aircraft flight management system, if a clearance message transmitted to the aircraft instructs the pilot to modify the aircraft's current flight plan, once the pilot acknowledges the message, he or she may then need to update the flight plan in the aircraft flight management system. Again, this added operation can be cumbersome, time-consuming, and a distraction to the pilot. Moreover, because the messages are displayed on a separate display, the pilot's attention may be diverted away from the main flight deck display(s).
Hence, there is a need for a system and method that addresses one or more of the above-noted drawbacks. Namely, a system and method for transmitting, receiving, initiating, and displaying textual air traffic control clearance messages that is less cumbersome, less time-consuming, and less distractive to a pilot, and/or alleviates the need for a pilot to separately update the aircraft flight plan using the flight management system when the textual clearance message requests such a modification, and/or does not divert the pilot's attention away from the aircraft's main flight deck display(s). The present invention addresses one or more of these needs. Furthermore, other desirable features and characteristics of the present invention will become apparent from the subsequent detailed description and the appended claims, taken in conjunction with the accompanying drawings and the foregoing technical field and background.
A display system and method is provided for transmitting, receiving, initiating, and displaying textual air traffic control clearance messages simultaneously with a graphic representation of an aircraft flight plan. The system and method alleviates the need for a pilot to separately update the aircraft flight plan if the textual clearance message requests such a modification.
In one embodiment, and by way of example only, an aircraft flight management display system for displaying air traffic control clearance messages transmitted to an aircraft includes a processor and a display. The processor is adapted to receive data representative of a current aircraft flight plan, and one or more textual clearance message signals representative of the air traffic control clearance messages and is operable, in response thereto, to supply one or more flight plan display commands and one or more clearance message display commands. The display is coupled to receive the flight plan display commands and the clearance message display commands and is operable, in response thereto, to substantially simultaneously display one or more images representative of the current aircraft flight plan, and the textual air traffic clearance messages.
In another exemplary embodiment, a method of displaying an air traffic control clearance message transmitted to an aircraft in a display area of a flight deck display includes the steps of processing data representative of a current aircraft flight plan, and processing one or more textual clearance message signals representative of the air traffic control clearance message. One or more images representative of the current aircraft flight plan, and the textual air traffic clearance messages are each substantially simultaneously displayed in the display area.
The present invention will hereinafter be described in conjunction with the following drawing figures, wherein like numerals denote like elements, and wherein:
The following detailed description is merely exemplary in nature and is not intended to limit the invention or the application and uses of the invention. Furthermore, there is no intention to be bound by any expressed or implied theory presented in the preceding technical field, background, brief summary or the following detailed description.
Turning now to the description, and with reference to
The processor 104, as was just noted, is in operable communication with, and receives user input commands from, the user interface 102. The processor 104 is additionally in operable communication with the navigation databases 106, and with the display 108, and is coupled to receive various types of avionics data 114 from various remote systems and/or sensors (not illustrated), and to receive signals 116 representative of air traffic control clearance messages. The processor 104 receives the user input commands supplied from the user interface 102 and is configured, in response to these user input commands, to selectively retrieve data from one or more of the navigation databases 106 and supply appropriate display commands to the display 108, so that the retrieved data is appropriately displayed on the display 108. The processor 104 is additionally configured to supply appropriate display commands to the display 108 so that the avionics data 114 may be selectively displayed on the display 108.
The processor 104 may be any one of numerous known general purpose microprocessors or an application specific processor that operates in response to program instructions. In the depicted embodiment, the processor 104 includes on-board RAM (random access memory) 118, and on-board ROM (read only memory) 120. The program instructions that control the processor 104 may be stored in either or both the RAM 118 and the ROM 120. For example, the operating system software may be stored in the ROM 120, whereas various operating mode software routines and various operational parameters may be stored in the RAM 118. It will be appreciated that this is merely exemplary of one scheme for storing operating system software and software routines, and that various other storage schemes may be implemented. It will also be appreciated that the processor 104 may be implemented using various other circuits, not just a programmable processor. For example, digital logic circuits and analog signal processing circuits could also be used.
The navigation databases 106 include various types of navigation-related data. Such navigation-related data includes various flight plan related data such as, for example, waypoints, distances between waypoints, headings between waypoints, data related to different airports, navigational aids, obstructions, special use airspace, political boundaries, communication frequencies, and aircraft approach information. It will be appreciated that, although the navigation database 106 is, for clarity and convenience, shown as being stored separate from the processor 104, the database 106 could be loaded into the on-board RAM 118, or the database 106 could be integrally formed as part of the processor 104, and/or RAM 118, and/or ROM 120. The navigation database 106 could also be part of a device or system that is physically separate from the display system 100. The avionics data 114 that is supplied from remote systems and/or sensors includes data representative of the state of an aircraft such as, for example, aircraft speed, altitude, and heading.
The air traffic control signals 116 are transmitted to an aircraft via, for example, modulated radio frequency (RF) signals. The air traffic control signals 116 are received and demodulated by a transceiver 122, and are then supplied to the processor 104. The air traffic control signals 116 each include data representative of one or more air traffic control clearance messages. Thus, the processor 104 further processes the signals 116 and supplies one or more display commands to the display 108, such that the clearance messages are displayed in both a textual format and a graphical format. As will be described more fully below, the processor 104 also supplies air traffic control response signals 124 to the transceiver 122, which in turn modulates the response signals 124 and transmits the modulated response signals 126 to an air traffic control station (not shown). In the depicted embodiment, the transceiver 122 is separate from the processor 104. However, it will be appreciated that the transceiver 122 could be implemented as part of the processor 104.
The display 108 is used to display various images and data, in both a graphical and a textual format, and to supply visual feedback to the user 109 in response to the user input commands supplied by the user 109 to the user interface 102. It will be appreciated that the display 108 may be any one of numerous known displays suitable for rendering image and/or text data in a format viewable by the user 109. Non-limiting examples of such displays include various cathode ray tube (CRT) displays, and various flat panel displays such as, various types of LCD (liquid crystal display) and TFT (thin film transistor) displays. To provide a more complete description of the method that is implemented by the flight management system 100, a general description of the display 108 and its layout will now be provided.
With reference to
The vertical profile 206 includes a side-view aircraft symbol 214, one or more waypoint symbols 216, line segments 218 that interconnect the waypoint symbols 216, a vertical axis 220, and a horizontal axis 222. The aircraft symbol 214 is preferably displayed with an orientation substantially equivalent to the actual orientation of the aircraft. The waypoint symbols 216 and interconnecting line segments 218 correspond to the current flight path and flight plan of the aircraft. The vertical axis 220 represents aircraft altitude and is suitably graduated with altitude values (not shown), and the horizontal axis 222 represents aircraft lateral position and is suitably graduated with lateral distance values (not shown). It will be appreciated that the horizontal axis 222 could alternatively be graduated with time values in addition to, or instead of, lateral distance values.
The lateral map 208 includes a top-view aircraft symbol 224, one or more waypoint symbols 226, line segments 228 that interconnect the waypoint symbols, and one or more range rings 230. The lateral map 208 also preferably includes various map features including, but not limited to, terrain, political boundaries, and navigation aids, which, for clarity, are not shown in
The textual air traffic control messages 210 that are displayed in the display area 202 correspond to the above-mentioned air traffic control signals 116 that are received and demodulated by the transceiver 122, and processed by the processor 104. The user interface field 212, as will be described more fully below, is displayed whenever a textual air traffic control signal 116 is received and processed by the processor 104, and the corresponding textual air traffic control message 210 is displayed. Preferably, the textual messages 210 and user interface field 212 are automatically displayed each time a textual air traffic control signal 116 is received and processed by the processor 104. Moreover, the message 210 and user interface field 212 both preferably remain displayed until the processor 104 receives an appropriate response via the user interface field 212, preferably in the form of a user command signal supplied from the user interface 102. Once an appropriate response to the displayed message 210 is received, the message 210 and user interface field 212 are preferably no longer displayed in the display area 202. In a particular preferred embodiment, the message 210 and user interface field 212 are both simultaneously displayed on the lateral map 208. It will be appreciated that this is merely exemplary of a particular preferred embodiment, and that either, or both, could be displayed with the other graphical and textual images described above.
Having described a particular embodiment of the system 100, and the general layout of the display area 202, from a structural standpoint, and having generally described the overall functionality of the system 100, a more detailed description of a process implemented by the system 100 to simultaneously display flight management data and textual air clearance messages on the same display 108 will be provided. In doing so, reference should be made, as appropriate, to
Turning first to
The processor 104 also determines whether the received air traffic clearance message signal 116 indicates a modification to the current flight plan (308). If the message signal 116 does indicate such a modification, then the modification is graphically displayed on the lateral map 208 with the current flight plan (310). For example, as shown in
The processor 104 will continue supplying display commands to the display 108, such that the current and modified flight plans, the textual clearance message 210, and the user interface field 212 are simultaneously displayed, until the user 109 appropriately responds to the textual clearance message 210 (312). Once the appropriate response is provided, the processor 104 supplies an air traffic control response signal 124 to the transceiver 122, which in turn modulates the response signal 124 and transmits the signal to the air traffic control station that sent the originating message (314). The processor 104 also updates the flight plan, if necessary, consistent with the user response (316). For example, in the depicted embodiment, and as shown in
In addition to responding to textual clearance messages transmitted to the aircraft, it will be appreciated that the system 100 may be configured to allow the pilot 109 to transmit textual messages from the aircraft to, for example, an air traffic control center. In one embodiment, the pilot 109 may compose a message using the user interface keyboard 112. The message, while it is being composed, is displayed as a textual clearance message 210 in the display area 202. Then, when the pilot 109 is ready to send the message, he or she may transmit the message 210 by selecting the “Accept” button in the user interface field 212. Alternatively, when the pilot 109 is composing a textual message 210, the system 100 could be configured such that the user interface field 212 displays a “Transmit” button, rather than the “Accept” button. In either case, when the message 210 is transmitted, the processor 104 transmits the textual message data to the transceiver 122, which modulates the textual message data for transmission to the air traffic control center.
It will be appreciated that the use of the keyboard 112 to compose a pilot-initiated textual message 210 is merely exemplary of one particular embodiment, and that the system 100 could be configured to allow the pilot 109 to compose messages using other means of implementation. For example, the system 100 could be configured to allow the pilot 109 to select predetermined phrases or words from, for example, a static or drop-down menu, using the CCD 110. The words or phrases are preferably consistent with air traffic control syntax such, and may be, for example, cockpit control language such as disclosed in U.S. Pat. No. 5,844,503, entitled “Method and Apparatus for Avionics Management,” which is assigned to the assignee of the present application, the entirety of which is hereby incorporated by reference.
In addition to automatically updating a current flight plan in response to a clearance message, the system 100 is also preferably configured to generate and transmit a textual message in response to the pilot 109 graphically updating the flight plan. For example, with reference once again to
While at least one exemplary embodiment has been presented in the foregoing detailed description, it should be appreciated that a vast number of variations exist. It should also be appreciated that the exemplary embodiment or exemplary embodiments are only examples, and are not intended to limit the scope, applicability, or configuration of the invention in any way. Rather, the foregoing detailed description will provide those skilled in the art with a convenient road map for implementing the exemplary embodiment or exemplary embodiments. It should be understood that various changes can be made in the function and arrangement of elements without departing from the scope of the invention as set forth in the appended claims and the legal equivalents thereof.
