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
2016-04-19
Patent
Elektronische Ressource
Englisch
PITCH FEEDBACK CONTROL SPLITTING FOR HELICOPTERS WITH REDUNDANT ACTUATORS
Europäisches Patentamt | 2015
|ADJUSTABLE PITCH PROPELLER OR GTE FAN WITH REDUNDANT ACTUATORS.
Europäisches Patentamt | 2020
|REDUNDANT HYDRAULIC CONTROL SYSTEM FOR ACTUATORS
NTIS | 1971
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