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
2025-03-06
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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