The present disclosure provides methods and system for managing gust loading in an aircraft. A deflection angle of one or more spoilers of the aircraft is monitored. When the spoiler deflection angle is above a first threshold value, one or more aileron control signals are sent to the ailerons. The aileron control signals cause the ailerons to deflect based on the spoiler deflection angle.
Gust loading management
2020-12-29
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Gust loading and response of flexible aircraft
Engineering Index Backfile | 1967
|Engineering Index Backfile | 1966
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