An aircraft attitude controller configured to obtain information representative of an attitude of an aircraft is disclosed. On the basis of the information, the attitude controller is configured to control the attitude of the aircraft by actively controlling a position of a winglet at a distal end of a wing portion of a wing of the aircraft, relative to the wing portion, thereby to control an angle of incidence of the winglet.
AIRCRAFT ATTITUDE CONTROLLER AND WING SYSTEM
2024-02-29
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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