The present invention discloses a method and flight controller for controlling an aircraft, comprising the following step: —determining the pitch control input δE for at least one pitch moment generator element, based on the lift control input δF for at least one lift generator element; wherein the step of determining the pitch control input δE based on the lift control input δF includes the step of determining a feed forward filter output Fq,δE,δF(q).
METHOD AND CONTROLLER FOR CONTROLLING AN AIRCRAFT BY IMPROVED DIRECT LIFT CONTROL
14.05.2020
Patent
Elektronische Ressource
Englisch
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