摘要:
The present examples provide circuits, systems, processes, and the like for providing precision course guidance, typically for improved positive course guidance below published minimum descent altitude or decision altitude, including just in time calculations of obstacle free flight paths. The calculated flight path may be presented in the context of a synthetic scene of the environment surrounding the aircraft. To provide precision course guidance, exemplary avionics systems, processes and the like, as described below may be utilized.
摘要:
A system for providing a manipulatable graphical display comprising a user input device responsive to a user input, a cursor control device operably coupled to the user input device, and a menu engine operably coupled to the cursor control device. The cursor control device is further configured to process an output received from the user input device and generate a cursor image positioned on a display in response to the user output suitable for locking onto and tracing a path on the display.
摘要:
A head worn head up display (HUD) system providing an enhanced head down view in an environment including a head worn device including a vision tracking device and a dynamic head down display. The head worn HUD system includes a computational platform for receiving vision tracking device signals from a vision tracking device of a head worn device and for generating head down display signals associated with a dynamic head down display. The computational platform processes and utilizes the vision tracking device signals and the generated head down display signals to provide output signals to the head worn device for output by the head worn device as superimposed visual steering cues to the operator.
摘要:
An integrated system for providing a reporting point journey log display in an aircraft and for providing the automatic transfer and installation of a reporting point journey log in a ground retention application. The integrated system includes means for procuring and aggregating reporting point on-board aircraft data from aircraft systems. Means are provided for generating a reporting point cockpit message and readback script from the aggregated reporting point onboard aircraft data. The aggregated reporting point onboard aircraft data is automatically transmitted to a receiving ground application for assembling the data into the form of a reporting point journey log. The reporting point journey log is installed into a ground storage application.
摘要:
A system for providing crosswind component information to a pilot of an aircraft is disclosed. The system is comprised of a navigation system; datalink system; devices for manual input of data; a crosswind component module consisting of, in part, a processor and database; and an indicating system consisting of, in part, a tactical display unit system of an aircraft. A navigation system may provide flight parameters for measured and intended flight data as inputs. Other data may also be provided from manual input devices and a datalink system as inputs. The processor of the crosswind component module receives the data, retrieves runway direction data, and determines the data of the crosswind components. An indicating system receives the data of the crosswind components and displays this information.
摘要:
An integrated system for providing minimum equipment decision support for an aircraft including means for procuring onboard aircraft data and providing a cockpit message. Minimum equipment list (MEL) constraints and offboard flight plan related information are procured. The onboard aircraft flight data, minimum equipment list constraints, and offboard flight plan related information are synthesized to enable holistic flight dispatch determinations within the current fault condition of the aircraft.
摘要:
An information magnification system for providing enhanced display information for a display system for a vehicle. The display system is of a type that includes a first display and a second display. The information magnification system includes a user interface for providing the capability for a user to select a magnification zone of interest on the first display of the vehicle. An information magnification electronics subsystem is associated with the user interface and with the first and second displays to enable the selected magnification zone to be presented on the second display appearing to be behind the physical surface of the second display at a selected distance, thus providing the capability for the user to maintain a far field of focus.
摘要:
The present invention is a flight deck situational awareness system for displaying Required Time of Arrival (RTA) information for an aircraft. The system may include a memory configured for storing aircraft navigation information for the aircraft. The system may also include a processor. The processor may be configured for being communicatively coupled with the memory and may further be configured for receiving the aircraft navigation information stored in the memory. The processor may generate a depiction based upon the aircraft navigation information. The depiction may include a Required Time of Arrival (RTA) flight cue for the aircraft. The system may further include a display, which may be communicatively coupled with the processor. The display may receive the depiction from the processor and may display the depiction.
摘要:
An aircraft taxi route display system may include a user interface including a display device and a user input, a computer including a computer processor and a computer storage device, wherein the computer is in communication with the user interface, and/or a communications link capable of receiving at least one airport characteristic, wherein the communications link is in communication with the computer processor, and the computer processor is configured to present an aircraft taxi route. A method may include capturing at least one of at least one taxi turn direction or at least one taxi distance, accepting from a user input a selection of at least one of at least one taxi turn direction or at least one taxi distance, clearing an aircraft taxi route from the selection of at least one of at least one taxi turn direction or at least one taxi distance, and displaying the aircraft taxi route.
摘要:
A system for providing taxi navigation information to a pilot of an aircraft is comprised of a navigation system; a taxi navigation module consisting of, in part, a processor and database; and an indicating system consisting of, in part, a tactical display unit system (e.g., a primary flight director (“PFD”), and head-up display (“HUD”) of an aircraft. A navigation system may provide aircraft position data of the aircraft while it is on the ground. A processor receives the aircraft position data, retrieves taxi navigation symbology based upon the aircraft position data from a taxi navigation database, and provides this data to the indicating system. The indicating system generates the display of taxi navigation information on a display unit which, in turn, provides the pilot with an egocentric view of airport signage using colored aviation signage symbology.