A multirotor aircraft is provided. The multirotor aircraft comprises a body comprising a main body and a camera assembly with a camera coupled to the main body; a frame connected to the body, comprising a multirotor propulsion system; and a drive system coupled with the body and the frame, for driving the body to rotate against the frame. With the multirotor aircraft, full unobstructed 360° yaw field of view of the camera in the upper or lower hemisphere can be obtained and the camera is in a safe position at takeoff and landing.
MULTIROTOR AIRCRAFT
MULTIROTORFLUGZEUG
AÉRONEF À ROTORS MULTIPLES
2021-03-31
Patent
Elektronische Ressource
Englisch