A flight control system and method which determines an expected power required data in response to a flight control command of the at least one model following control law and utilizes the expected power required data to perform at least one action to control an engine speed.
ENGINE ANTICIPATION FOR ROTARY WING AIRCRAFT
MOTORVORHERSAGE FÜR DREHFLÜGELFLUGZEUG
ANTICIPATION DE MOTEUR POUR UN AÉRONEF À AILES ROTATIVES
2018-07-25
Patent
Elektronische Ressource
Englisch
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