Unmanned aerial vehicle, flight control mechanism of unmanned aerial vehicle, and method using the same

摘要

To provide a flight control mechanism for controlling the flight of an unmanned aerial vehicle by controlling a collision with a boundary surface, an unmanned aerial vehicle equipped with the mechanism, and a method using these. The first preceding collision member, the second preceding collision member, and the first and second preceding collision members are separated and held above the fuselage of the unmanned aerial vehicle, and the aircraft is centered on the inside of the aircraft or a predetermined position on the aircraft. A holding member that can be tilted with respect to the airframe by rotating to the side of the above, and a holding member that rotates in response to one of the first and second preceding collision members colliding with the boundary surface. Provided a flight control mechanism for unmanned aerial vehicles.