Abstract: A method and device for displaying radio frequency information, including a database of stored radio frequency identifiers and radio frequency information corresponding thereto, and a processor coupled to the database and operating one or more algorithms for generating a display signal as a function of a correspondence between a decoded radio frequency identifier and one of the stored radio frequency identifiers.

Abstract: An apparatus, method and computer program product useful for supplying the pilot of an aircraft with aircraft attitude information. During bank angles exceeding a predefined limit, the roll gyro is slaved to a roll angle estimator for improved system accuracy.

Abstract: An apparatus, method and computer program product useful for supplying the pilot of an aircraft with aircraft attitude information. During bank angles exceeding a predefined limit, the roll gyro is slaved to a roll angle estimator for improved system accuracy.

Abstract: An aviation facility nominating device for an aircraft includes a position receiving component that receives position data indicating a position of the aircraft, an aviation data receiving component that receives aviation data associated with a plurality of aviation facilities, a facility selecting component for selecting aviation data for a selected plurality of the aviation facilities based on a position of the aircraft and a nominating component that nominates at least one but not all of the selected plurality of aviation facilities as a nominated aviation facility likely to be of interest to a pilot based on the position of the aircraft.

Abstract: An apparatus, method and computer program product useful for supplying the pilot of an aircraft with aircraft attitude information in the event of full or partial failure of the gyroscopic system normally used to supply such data. The pitch angle, roll angle and heading angle estimates provided by the apparatus, method and computer program product can be displayed to the pilot thereby alleviating the requirement that the pilot mentally integrate such data from the remaining aircraft instruments.

Abstract: An apparatus, method and computer program product useful for supplying the pilot of an aircraft with aircraft attitude information. During bank angles exceeding a predefined limit, the roll gyro is slaved to a roll angle estimator for improved system accuracy.

Abstract: An aviation facility nominating device for an aircraft includes a position receiving component that receives position data indicating a position of the aircraft, an aviation data receiving component that receives aviation data associated with a plurality of aviation facilities, a facility selecting component for selecting aviation data for a selected plurality of the aviation facilities based on a position of the aircraft and a nominating component that nominates at least one but not all of the selected plurality of aviation facilities as a nominated aviation facility likely to be of interest to a pilot based on the position of the aircraft.

Abstract: A method and device for displaying radio frequency information, including a database of stored radio frequency identifiers and radio frequency information corresponding thereto, and a processor coupled to the database and operating one or more algorithms for generating a display signal as a function of a correspondence between a decoded radio frequency identifier and one of the stored radio frequency identifiers.

Abstract: A method and device for displaying radio frequency information, including a circuit or processor for retrieving various radio frequency information that are correlated to each of the various communication and navigational frequencies, including such information as the name of the facility transmitting, the frequency station type, the station identifier, the runway number, and the final approach course. The method and device include means for displaying the retrieved radio frequency information.

Abstract: An apparatus, method and computer program product useful for supplying the pilot of an aircraft with aircraft attitude information. During bank angles exceeding a predefined limit, the roll gyro is slaved to a roll angle estimator for improved system accuracy.

Abstract: An apparatus, method and computer program product useful for supplying the pilot of an aircraft with aircraft attitude information in the event of full or partial failure of the gyroscopic system normally used to supply such data. The pitch angle, roll angle and heading angle estimates provided by the apparatus, method and computer program product can be displayed to the pilot thereby alleviating the requirement that the pilot mentally integrate such data from the remaining aircraft instruments.