A ganged servo flight control system for an unmanned aerial vehicle is provided. The flight control system may include a swashplate having first, second, and third connection portions; a first control assembly connected to the first connection portion of the swashplate; a second control assembly connected to the second connection portion of the swashplate; and a third control assembly connected to the third connection portion of the swashplate. The first control assembly may include two or more servo-actuators connected to operate in cooperation with each other. 16217 168 164 184B 0198C 182C C> C 0 0 184C 1 188B 0 8A184A 1831B 198A 186A 182A
GANGED SERVO FLIGHT CONTROL SYSTEM FOR AN UNMANNED AERIAL VEHICLE
2021-09-23
Patent
Electronic Resource
English
Ganged servo flight control system for unmanned aerial vehicle
European Patent Office | 2022
|GANGED SERVO FLIGHT CONTROL SYSTEM FOR AN UNMANNED AERIAL VEHICLE
European Patent Office | 2024
|GANGED SERVO FLIGHT CONTROL SYSTEM FOR AN UNMANNED AERIAL VEHICLE
European Patent Office | 2023
|GANGED SERVO FLIGHT CONTROL SYSTEM FOR AN UNMANNED AERIAL VEHICLE
European Patent Office | 2022
|Ganged servo flight control system for an unmanned aerial vehicle
European Patent Office | 2020
|