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
VERFAHREN UND STEUERUNG ZUR STEUERUNG EINES FLUGZEUGS DURCH VERBESSERTE DIREKTAUFTRIEBSSTEUERUNG
PROCÉDÉ ET DISPOSITIF DE COMMANDE POUR COMMANDER UN AÉRONEF PAR UNE COMMANDE DE PORTANCE DIRECTE AMÉLIORÉE
2024-05-01
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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