An aircraft includes a vehicle body, a main wing fixedly connected to the vehicle body and configured to provide lift thrust for the aircraft, a canard arranged at the vehicle body near a nose and configured to provide lift thrust for the aircraft, and a multi-rotor assembly including a first rotor assembly mechanically coupled with the main wing and a second rotor assembly rotatably connected to the canard and configured with an adjustable tilting angle relative to the canard to provide at least one of lift thrust or forward pulling thrust for the aircraft.
AIRCRAFT, AIRCRAFT CONTROL METHOD AND DEVICE, AND COMPUTER-READABLE STORAGE MEDIUM
06.03.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Aircraft control method, aircraft and computer readable storage medium
Europäisches Patentamt | 2023
|AIRCRAFT, AIRCRAFT CONTROL METHOD AND DEVICE, AND COMPUTER-READABLE STORAGE MEDIUM
Europäisches Patentamt | 2025
|AIRCRAFT, AIRCRAFT CONTROL METHOD AND DEVICE, AND COMPUTER-READABLE STORAGE MEDIUM
Europäisches Patentamt | 2023
|Aircraft, aircraft control method and device, and computer readable storage medium
Europäisches Patentamt | 2024
|Aircraft, control method, apparatus and computer readable storage medium for aircraft
Europäisches Patentamt | 2023
|