Abstract: Systems and methods for changing the orientation of information displayed on a display device mounted on a control pedestal at a position between two seats. One method involves changing the orientation of information displayed on a display device located on a control pedestal of an aircraft so that, instead of sub-optimal joint viewing of the displayed information by two pilots, an individual pilot may be able to read the displayed information more easily. The system enables either pilot to select a respective more optimal orientation for the displayed information for individual viewing. Each pilot may separately then quickly switch the display mode back to the “up is forward” orientation for joint viewing. Returning to the “up is forward” orientation may also be set to occur as a function of time.

Abstract: Systems and methods for changing the orientation of information displayed on a display device mounted on a control pedestal at a position between two seats. One method involves changing the orientation of information displayed on a display device located on a control pedestal of an aircraft so that, instead of sub-optimal joint viewing of the displayed information by two pilots, an individual pilot may be able to read the displayed information more easily. The system enables either pilot to select a respective more optimal orientation for the displayed information for individual viewing. Each pilot may separately then quickly switch the display mode back to the “up is forward” orientation for joint viewing. Returning to the “up is forward” orientation may also be set to occur as a function of time.

Abstract: A method, avionics apparatus and computer program for determining a terminal flight path, including access to aircraft position information provided by a Global Positioning System (GPS) receiver. The method apparatus and computer program determine an Intended Touchdown Point (ITP), which is the desired landing location on an intended runway; determine a Current Touchdown Point (CTP), which is where the aircraft will land given its current glidepath and is a function of the current trajectory, configuration and engine thrust; determine a correspondence of the CTP and ITP and generate an output signal as a function of the correspondence, which is displayed on a cockpit display device, annunciated on a cockpit speaker, or both.

Abstract: A signal processing device references a database of communication/navigation facilities and determines if communications are available with that facility given a current position of the user.

Abstract: A method, avionics apparatus and computer program for determining a terminal flight path, including access to aircraft position information provided by a Global Positioning System (GPS) receiver. The method apparatus and computer program determine an Intended Touchdown Point (ITP), which is the desired landing location on an intended runway; determine a Current Touchdown Point (CTP), which is where the aircraft will land given its current glidepath and is a function of the current trajectory, configuration and engine thrust; determine a correspondence of the CTP and ITP and generate an output signal as a function of the correspondence, which is displayed on a cockpit display device, annunciated on a cockpit speaker, or both.

Abstract: A method and device for deriving and displaying advanced TCAS information.

Abstract: A circuit and method for displaying a vertical profile view of situational awareness information.

Abstract: A method and device for deriving and displaying advanced TCAS information.

Abstract: A signal processing device references a database of communication/navigation facilities and determines if communications are available with that facility given a current position of the user.