A control method for controlling a yaw angle γz and a roll angle γx of a vertical take-off aircraft comprising at least two drive groups arranged in opposite side regions of the aircraft so as to be spaced apart from a fuselage of the aircraft is presented. Each drive group comprises at least one first drive unit. The first drive unit is arranged so as to be spaced apart from the fuselage to pivot about a pivot angle α into a horizontal flight position and a vertical flight position.
STEUERUNGSVERFAHREN ZUR STEUERUNG EINES GIER- UND EINES ROLLWINKELS EINES SENKRECHT STARTENDEN FLUGZEUGS
CONTROL METHOD FOR CONTROLLING A YAW ANGLE AND A ROLL ANGLE OF AN AIRCRAFT THAT TAKES OFF VERTICALLY
PROCÉDÉ DE COMMANDE POUR LA COMMANDE D'UN ANGLE DE LACET ET DE ROULIS D'UN AVION À DÉMARRAGE VERTICAL
2021-11-03
Patent
Electronic Resource
German
European Patent Office | 2018
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