The application provides a ganged servo flight control system for an unmanned aerial vehicle. 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.
本申请提供了一种用于无人飞行器的联动伺服飞行控制系统。飞行控制系统可包括具有第一连接部分、第二连接部分和第三连接部分的斜盘;连接到斜盘的第一连接部分的第一控制组件;连接到斜盘的第二连接部分的第二控制组件;以及连接到斜盘的第三连接部分的第三控制组件。第一控制组件可包括被连接以彼此配合操作的两个或更多个伺服致动器。
Ganged servo flight control system for unmanned aerial vehicle
用于无人飞行器的联动伺服飞行控制系统
2022-02-18
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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 | 2021
|Ganged servo flight control system for an unmanned aerial vehicle
European Patent Office | 2020
|Ganged servo flight control system for an unmanned aerial vehicle
European Patent Office | 2020
|Ganged servo flight control system for an unmanned aerial vehicle
European Patent Office | 2024
|