AIRCRAFT AUTORECOVERY SYSTEMS AND METHODS

Methods and systems for performing auto-recovery for an aircraft (20). An example system includes position and information systems (26, 30), an automatic flight control system (36), a database (32), and a processor (22). The database includes terrain data, airport data, obstacle data, and protected...

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Bibliographic Details
Main Authors JOHNSON Steven, C, GLOVER, John, H, BATEMAN, Charles, D
Format Patent
LanguageEnglish
French
German
Published 24.01.2018
Subjects
CONTROLLING
PHYSICS
REGULATING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
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Summary:Methods and systems for performing auto-recovery for an aircraft (20). An example system includes position and information systems (26, 30), an automatic flight control system (36), a database (32), and a processor (22). The database includes terrain data, airport data, obstacle data, and protected airspace data. The processor determines if one of a caution alert exists based on data stored in the database and information received from the position and information systems. Auto­recovery instructions are generated and sent to the automatic flight control system if no positive flight control input has been performed at time of expiration of a waiting period. Auto-recovery instructions are generated based on an analysis of two or more auto-recovery routes. The system does not perform auto-recovery if components of the system fail to meet a predefined validity or integrity level.
Bibliography:Application Number: EP20040750394