The present disclosure provides an aircraft. The aircraft includes: a vehicle body; main wings, fixedly connected to the vehicle body and used to provide lift thrust for the aircraft; canards, arranged at the vehicle body near a nose and used to provide the lift thrust for the aircraft; and a multi-rotor assembly including first rotor assemblies and second rotor assemblies. The first rotor assemblies are mechanically coupled with the main wings; and the second rotor assemblies and the canards are rotatably connected to each other. The second rotor assemblies are configured to be able to adjust their tilting angle relative to the canards to provide lift thrust and/or forward pulling thrust for the aircraft.
AIRCRAFT, AIRCRAFT CONTROL METHOD AND DEVICE, AND COMPUTER-READABLE STORAGE MEDIUM
FLUGZEUG, FLUGZEUGSTEUERUNGSVERFAHREN UND -VORRICHTUNG UND COMPUTERLESBARES SPEICHERMEDIUM
AÉRONEF, PROCÉDÉ ET DISPOSITIF DE COMMANDE D'AÉRONEF ET SUPPORT DE STOCKAGE LISIBLE PAR ORDINATEUR
02.04.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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