According to one embodiment, a rotorcraft includes rotors (3), a fuselage (2), at least three rods (4), at least one load sensor (5) and a control device (6). The rotors (3) obtain lift. The fuselage (2) is coupled to the rotors (3). The at least three rods (4) support the fuselage (2). The at least one load sensor (5) detects loads (F1, F2, F3, F4) applied on the at least three rods (4). The control device (6) automatically controls the rotors (3) so that measured values of the loads (F1, F2, F3, F4) detected by the at least one load sensor (5) are brought to targeted values of the loads (F1, F2, F3, F4).
ROTORCRAFT AND METHOD OF CONTROLLING ROTORCRAFT
DREHFLÜGLER UND VERFAHREN ZUR STEUERUNG DES DREHFLÜGLERS
GIRAVION ET PROCÉDÉ DE COMMANDE D'UN GIRAVION
2023-06-07
Patent
Elektronische Ressource
Englisch