The purpose of the present invention is to provide a flight control mechanism for controlling flight of an unmanned aerial vehicle by controlling collision between the vehicle and a boundary surface, an unmanned aerial vehicle equipped with the mechanism, and a method for using the mechanism and the vehicle. Provided is a flight control mechanism for an unmanned aerial vehicle including: a first initial collision member; a second initial collision member; and a holding member that holds the first and second initial collision members with a space therebetween above the body of the unmanned aerial vehicle, is tiltable with respect to the vehicle body by rotating about a predetermined position inside or above the vehicle body toward the side of the vehicle body, and rotates in response to collision between the first or second initial collision member and a boundary surface.
Unmanned Aerial Vehicle, Flight Control Mechanism for Unmanned Aerial Vehicle, and Method for Using Unmanned Aerial Vehicle and Mechanism for Unmanned Aerial Vehicle
2021-05-20
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2019
|European Patent Office | 2021
|European Patent Office | 2024
|European Patent Office | 2023
|Unmanned aerial vehicle arm mechanism and unmanned aerial vehicle
European Patent Office | 2024
|