Disclosed is a control apparatus (300) for controlling a steering system (301) of an aircraft landing gear, the aircraft landing gear being configurable in a stowed configuration and a deployed configuration. The steering system (301) comprises a wheel arrangement (202) including one or more wheels. The control apparatus (300) is arranged to perform a control process comprising: receiving one or more signals from one or more sensors (302a, 302b) indicating a position of the wheel arrangement (202) when the landing gear is in the stowed configuration; determining whether a predetermined condition is satisfied in relation to the position of the wheel arrangement (202); and, in response to determining that the predetermined condition is satisfied, performing an adjustment process to control the steering system (301) to adjust the position of the wheel arrangement (202).
AIRCRAFT STEERING
FLUGZEUGLENKUNG
SYSTÈME DE DIRECTION D'UN AÉRONEF
02.01.2019
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Aircraft steering system, aircraft, and aircraft steering method
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