Embodiments are directed to generating, by a processing device, a feedback command for an aircraft based on a reference input and an output response of the aircraft, and analyzing, by the processing device, the feedback command to allocate control to a plurality of control surfaces over a plurality of separate frequency bands.
PITCH FEEDBACK CONTROL SPLITTING FOR HELICOPTERS WITH REDUNDANT ACTUATORS
2015-07-30
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Pitch feedback control splitting for helicopters with redundant actuators
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