An unmanned aerial vehicle (UAV) with omnidirectional thrust vectoring includes a central unit, a connective structure, and a plurality of propulsion units with omnidirectional thrust vectoring allowing a full six degrees of freedom. A vectored propulsion unit comprises thruster vectored by an omnidirectional mechanism and may include an autonomous sub-vehicle housed within a rotational frame, or an actuator-thruster assembly with directional control. A UAV with omnidirectional thrust vectoring includes a control system with a ground station unit, a central flight control unit, and a propulsion control unit. A plurality of vectored propulsion units working in coordination allows an unmanned aerial vehicle to maneuver with any stance or body orientation.
Unmanned Aerial Vehicle With Omnidirectional Thrust Vectoring
2018-05-31
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Unmanned aerial vehicle with omnidirectional thrust vectoring
European Patent Office | 2020
|UNMANNED AERIAL VEHICLE WITH OMNIDIRECTIONAL THRUST VECTORING
European Patent Office | 2018
|Optimal Control for Thrust Vectoring Unmanned Aerial Vehicle
Trans Tech Publications | 2010
|Thrust vectoring system and process for use with unmanned aerial vehicles
European Patent Office | 2023
|THRUST VECTORING SYSTEM AND PROCESS FOR USE WITH UNMANNED AERIAL VEHICLES
European Patent Office | 2024
|